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2006 FREEMAN SCHOLAR LECTURE

Swimming and Flying in Nature—The Route Toward Applications: The Freeman Scholar Lecture OPEN ACCESS

[+] Author and Article Information
Promode R. Bandyopadhyay

Department of Autonomous and Defensive Systems, Naval Undersea Warfare Center, Newport, RI 02841promode.bandyopadhya@navy.mil

J. Fluids Eng 131(3), 031801 (Feb 09, 2009) (29 pages) doi:10.1115/1.3063687 History: Received October 14, 2008; Revised October 15, 2008; Published February 09, 2009

Evolution is a slow but sure process of perfecting design to give a life-form a natural advantage in a competitive environment. The resulting complexity and performance are so sophisticated that, by and large, they are yet to be matched by man-made devices. They offer a vast array of design inspirations. The lessons from swimming and flying animals that are useful to fluids engineering devices are considered. The science and engineering of this subject—termed “biorobotics” here—are reviewed. The subject, being of dynamic objects, spans fluid dynamics, materials, and control, as well as their integration. The emphasis is on understanding the underlying science and design principles and applying them to transition to human usefulness rather than to conduct any biomimicry. First, the gaps between nature and man-made devices in terms of fluids engineering characteristics are quantitatively defined. To bridge these gaps, we then identify the underlying science principles in the production of unsteady high-lift that nature is boldly using, but that engineers have preferred to refrain from or have not conceived of. This review is primarily concerned with the leading-edge vortex phenomenon that is mainly responsible for unsteady high-lift. Next, design laws are determined. Several applications are discussed and the status of the closure of the gaps between nature and engineering is reviewed. Finally, recommendations for future research in unsteady fluids engineering are given.

FIGURES IN THIS ARTICLE
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The goal of this review is to discuss how fluids engineering is benefiting by learning from the march of biology. Fluids engineering has normally taken physics as its fountain of inspiration—and with remarkable successes that dot our life today. Looking at biology for inspiration therefore is a departure. It is thought that the physics discipline is matured, and its return on investment is declining with time. By and large, swimming and flying platforms are visually the same today as they were decades ago, and the efficiency of motors—the most common electromechanical device—remains low, with most of the input energy being wasted and with their operation remaining noisy. Turbulence models, as they are accounting for more and more of flow complexities, are becoming ever so narrowly applicable. There is a need to understand why, while we have more in-depth information about fluid dynamics, the impact on performance is not proportionately as high. Truly predictive capabilities are still scarce. One could list many examples to show that today’s engineering—fluids engineering, in our case—has matured to a great extent.

If we look at the march of natural history, one would expect such mature engineering to converge with biology. Therefore, a useful starting point is to quantify the gap between biology and engineering. Understanding the reasons why this gap exists should then be a target of queries and a means to advance. The reason why one should look for convergence of engineering with biology is as follows. Both biology and engineering are designs; they are tradeoffs of many competing mechanisms with sometimes different optimization and cost criteria (1). If there are gaps between the two, the approach should be to study the underlying mechanisms that are in play and determine whether those in nature should be inducted into engineering. This review examines such approaches and outlines successes.

A relative distinction between science and design, or basic and applied research, can be carried out in the following manner. In an elementary sense, from the point of view of basic and applied research, the broad rationale for biological inspiration in engineering may be viewed as shown schematically in the layered model in Fig. 1(1). Physics, which deals with fundamental forces and uncovers the laws of nature, is the core of science. All other layers deal with application in one form or another. The first adjacent layer is chemistry, which can be described as applied molecular physics. The next outer layer is biology, which is nature’s application of physics and chemistry into self-contained, autonomous systems. We assign the next outer layer to engineering, which is man’s application of physics and chemistry. The disciplines are relatively treated as more basic as we approach the core and more applied as we move to the outer layers. Biology and engineering are then both basically design. The degrees of freedom, number of actuators and sensors, redundancy, and autonomy generally decline in engineering systems compared with biological systems. All this echoes Engineer Fuller, who said that “In nature, technology has already been at work for millions of years” (2). Biological systems have higher degrees of freedom and, yet, are reliable over many cycles of operation. Cost and reliability, on the other hand, have deterred engineers in the past from building systems based on unsteady principles of aerodynamics or hydrodynamics. Therefore, it is essential that biology-inspired designs have large performance gains, and the induction of new materials, sensors, and power and control technology should help to improve reliability. Appropriate integration of these subsystems is also a key to the technology transition of the principles of swimming and flying animals. Because both biology and engineering are the subjects of design, the starting questions should be formulated carefully: What basic principles are in play? or, How is it built? The former is rooted in science, while the latter is in biomimicry.

If the goal of new approaches to fluids engineering is to improve performance, the first question that should be asked is as follows: How much improvement should we aim for? For example, if the hydrodynamic efficiency of a lifting surface improves from 50% to 75%, is that a large improvement? We argue below that such an absolute scale is misleading. The answer has to be sought in a systems context, and that is why there is a need to be cognizant of the component sciences that are integrated to build a device with durable advantage. Consider an elementary example. Imagine a person paddling a boat. What would be the impact on the overall efficiency if the hydrodynamic efficiency of the paddle was improved from 50% to 75%? An engineering alternative would have the paddler replaced with motor drives for electromechanical conversion and an engine converting chemical/nuclear fuel to electromotive energy. A well-built electric motor is 30% efficient, and an engine is 20% efficient. So, the result would be a system efficiency improvement of 3–4.5%. This is a sobering finding. We also take this opportunity to note that if the world is faced with a dwindling supply of hydrocarbon-based energy, then clearly addressing the gargantuan energy losses might well be more telling, although less glamorous, than drilling deeper into Earth’s crust. One alternative is to bypass the inefficient engine and go directly from fuel to electromotive energy, which is what a fuel cell does. The best practical fuel cell efficiency is below 50–60% due to waste heat, purity and system requirements. Another alternative is to improve the electromechanical efficiency of motors, and for this we need to delve into polymer- and carbon-based artificial muscles. Such muscles are even more efficient when they are in a bath of chemical fuel. So, in principle, biology does provide a design paradigm for impacting not only fluids engineering per se, but also the entire fluids engineering-based system if we are willing to integrate such nature-based hydrodynamic mechanisms with artificial muscles.

There is growing paleontologic evidence for the notion that all living birds of today—from ostriches to hummingbirds to ducks—trace their lineage to those that once lived by the shore. In other words, aquatic birds led to modern birds, and swimming and flying animals have a common ancestry. However, both in nature and in man-made devices, swimming and flying cover a large range of Reynolds numbers and mass, and conflicting requirements of required lift and thrust forces need to be met. Therefore, their design varies considerably. Here, Reynolds number is defined as a ratio of inertia to viscous forces usually in the form Re=UL/v, where U is the forward speed, L is the length scale, and ν is the kinematic viscosity of the fluid medium.

The interest in high-lift arose among biologists in a bid to explain how flying animals can keep themselves aloft in a low-density medium such as air, which is 840 times lighter than water. Many aquatic animals can control buoyancy, which is not practical in air. Some birds certainly have a very large wing span—the wandering albatross has a wingspan of 3.4 m; an extinct vulturelike bird called the giant teratorn (Argentavis magnificens) is estimated to have weighed 75 kg and to have had a wingspan of 8 m. Also, early fossils show insect wing spans of 10–710 mm. Thus, high-lift in animals is certainly an intriguing issue. Since both swimming and flying animals range from the tiniest to very large species, the high-lift mechanism is utilized over a very large Reynolds number range.

At the other end of the spectrum, flying insects weigh from 20μg to 3 g and span Reynolds numbers from 10 to 10,000. Insects produce far more lift forces than thrust compared with their bodyweights. (For swimming animals, the demand is the opposite, as buoyancy mechanisms are used to support gravity and aquatic animals tend to have a large percentage of saline water in their body making them nearly neutrally buoyant.) Low Reynolds number wings use the fling and clap method of high-lift. But insects of higher Reynolds numbers use a leading-edge vortex for high-lift. In fling and clap, the wings clap above the insect body. While flinging open, they create suction and a high-lift vortex is produced. Although fling and clap produces higher-lift forces than leading-edge dynamic stall vortex, the clap process tends to damage the wings. Not much is known at the lowest Reynolds number of 10, where thrips fly. Thrips have bristled wings. Measurements on geometrically scaled bristled and smooth wings show that the former produces lower levels of forces—not higher—during cruise or maneuver (3). More research is needed on hairy appendages at low Reynolds numbers. Much of academic biorobotics is focusing on replicating the function and motion of animals. This effort is driven by curiosity and the hope for discoveries, inventions, and practical applications. One practical impetus is to keep man out of harm’s way—for example, as in hazardous underwater salvage operations.

There are two distinct approaches to biorobotics. One seeks to understand the science principles first and then apply them, while the other merely mimics biology. Biology is not always superior to engineering. While turtles can navigate from the Florida coast to Africa and return to the same location within 100 m, undersea vehicles can roam around the globe and dock at their home pier within <1m. While insect flight muscles have an efficiency of <10%(4), the efficiency of motors can be 30%. While evolution took millions of years, the laboratory or numerical “genetic” simulation of fin efficiency (5) and eel kinematics (6) can take minutes to hours, respectively. Thus, there is no guarantee that mimicry will fill a need. For these reasons, in this review, we identify the mechanisms and function in animals and their appendages first. Then, we discuss the successes in the practical renderings of the mechanisms. The focus is on leading-edge vortex formation by unsteady wings—a mechanism extensively used in swimming and flying animals and now being explored for engineering renditions.

How can the integration of unsteady hydrodynamics with different disciplines help close the gaps between the performance of animals and that of current similar man-made vehicles and devices? There is a need to conduct careful measurements in the natural environment because they best show how energy storage, sensory inputs, stability, and navigation are integrated in one system. Future animal flight research is proceeding toward controlled experiments in simulated natural environments where different disciplines are integrated (7). Biorobotics also needs to do the same for rapid success in application. To make a case for animal-inspired fluids engineering, it is useful to quantify the gaps between the performance of current man-made vehicles and those of animals. The performance gaps in several variables in the underwater context have been determined in a series of investigations (5,8-9). The variables considered are the turning radius of underwater vehicles, efficiency, radiated noise, sonar characteristics, and suction adhesion.

Figure 2 compares underwater noise for several ships and fish, with sea state 3 as a baseline. The vertical axis is in increments of 200 m and is not in dB. While ships are noisier than fish, the German frigate carried out noise abatement modifications to contain or absorb noise, leading to a remarkable improvement. The goal is to explore means of reducing noise and vibration at the source—i.e., at the propulsor and the power drives. Possible solutions include reducing propulsor rotational rates, which can be accomplished by implementing higher-lift hydrofoils, and improving the electromechanical efficiency of drives and power trains (10). Profiles of new hydrofoils digitized from cadavers of swimming animals are discussed in a later section of this review. The hydrodynamic characteristics of these hydrofoils are worth exploring for improvement in propulsor performance.

One method of quantifying the performance gap between man-made vehicles and animals is to focus on underwater sound levels. The sound level under water is equivalent to the sound level in air plus 62 dB. A large airliner has a sound level of 120 dB (noise level at 1 m). This is equivalent to 182 dB in water. A cargo ship/tanker of sound level 190 dB is noisier than a large airliner. Even a tug and barge at 10 kn produces 170 dB. The onset of whale and dolphin avoidance response to industrial noise is at 120 dB, the ambient level in calm seas is 100 dB, and the coastal bay with snapping shrimp produces a noise level of 70 dB. Obviously, propulsion in man-made commercial vehicles is poorly designed compared with even large transcontinental swimming animals.

The variation in turning radius for constant normal acceleration between fish (such as bluefish and mackerel) and underwater vehicles of 1950s vintage and 1980s vintage shows gaps of several orders of magnitude (11-12). Bluefish and mackerel are endowed with both speed and maneuverability. The fish data were generated from trajectories of fish navigating about obstacles in a laboratory environment. The vehicle data are from unmanned underwater vehicles traversing a figure-eight trajectory of scale on the order of kilometers in the ocean. The same trajectory curvature algorithm was used in both data sets. The comparison shows that for constant acceleration, fish make shorter radii turns. The gap in turning ability has been narrowed over time, although a factor-of-10 gap remains. The narrowing is attributable to improvements in digital controllers and not to any hydrodynamics. Below, we discuss how the high-lift principles of swimming and flying animals have helped to close the gap completely.

A biorobotic autonomous underwater vehicle (BAUV) has been fabricated at the Naval Undersea Warfare Center implementing the dynamic stall high-lift principles of swimming and flying animals (5,8,13). The cylindrical hull vehicle has six penguinlike fins that roll and pitch at the same frequency, with a 90 deg phase difference in between (Fig. 3). The kinematics of each fin is independently controlled. The fins undergo dynamic stall and produce higher-lift than is possible in steady flow. Figure 3 shows that it is now possible to take a cylinder and make it turn at zero radius. Figure 3 shows the digitized vehicle position at different times, with the vehicle undergoing clockwise and counterclockwise turns. The length of each line represents the vehicle axis. It is shown that the center of the vehicle moves little in comparison to the radius of turning or the length of the vehicle. This is a clear demonstration that the high-lift principles of swimming and flying animals have helped not only to match the turning abilities of fish but perhaps even to surpass them (11-12).

The distribution of propulsion power density of man-made underwater vehicles and that of swimming animals for which muscle energy density data are available have been compared (8). The comparison shows propulsive power versus vehicle or fish volume. For cruise, there is a remarkable convergence between the two groups from nuclear submarines down to the tiny bonito—a stretch of eight decades of power and displacement. The animal-inspired BAUV vehicle (Fig. 3) is in excellent agreement with shark of similar size. Tactical-scale man-made maneuvering vehicles from the open literature are not generally speaking well designed, perhaps for lack of reference. Smaller and more maneuverable vehicles are likely to gain in performance from comparison with animals.

What is the gap in efficiency between swimming and flying animals and man-made fins and vehicles inspired by such animals? The answer to this question is shown in Fig. 4. Different kinds of efficiencies are shown. There is a dearth of reliable efficiency data on animals. These general trends may be tentatively discerned. Man-made unsteady fins can now be as highly efficient as those in animals as long as the leading-edge vortex high-lift sources are generated by appropriate rolling and pitching motions. However, in both animals and man-made vehicles comprising a multitude of single actuators, efficiency is much lower. In the two generations of man-made vehicles with animal-inspired high-lift actuators, efficiency has improved, although it is still lower than that in flying insects. The efficiency of insect flight muscle is quite low—less than 10% (4). Good quality electric motors have an efficiency of 20% or higher. So, what could explain the lower efficiency of man-made vehicles where the individual fins are just as efficient as those in swimming and flying animals? The answer may be frictional losses and the lack of a resonant design, and these possibilities are considered below.

In insects, wings operate in a narrow frequency band and a resonant oscillator design is employed. The quality Q of an oscillator in the neighborhood of resonance is defined as (14)Display Formula

Q=2πEpEd
(1)
where Ep is peak kinetic energy of the oscillator and Ed is the energy dissipated per cycle. Sometimes, the numerator is taken to be the total kinetic energy stored in one cycle. The Q factor can be taken as the number of cycles it takes for the kinetic energy to dissipate to 1/e2π=1/535 of its original value. A resonant system can be considered critically damped (Q=0.5), overdamped (Q<0.5), or underdamped (Q>0.5). The Q factor is 6.5 for the fruit fly, 10 for the hawkmoth, and 19 for the bumblebee. For biological systems, these values are “impressive.” In other words, the bumblebee wings resonate at higher amplitude at the resonant frequency than fruit fly wings do and their amplitude drops off more rapidly as well when the frequency moves away from resonant frequency. Flapping machines should also be designed as resonant systems. The controllers of underwater vehicles employing flapping fins do not have a resonant design, and the actuator drives have higher frictional losses.

Finally, a dolphin-inspired interaural time differencing sonar for underwater ranging at distances on the order of 100 m has been fabricated (15). Emitter sound frequencies and the interaural spatial gaps are in the range of those in dolphins. It was found that the angular resolution can be about 1 deg—similar to that of dolphins, but higher than that of human beings. However, apparently much more energy needs to be input into the water for pinging than that used by dolphins, which employ short-duration, nonlinear chirps. The engineered sonar requires very little processing compared with conventional sonars; it is lightweight in air, neutrally buoyant in water, low powered in comparison, and fits biorobotic vehicles, which tend to be on the scale of 1 m. In these criteria, the biology inspiration did lead to some advantageous performance. However, a large gap in performance exists, and a better understanding of how dolphins process acoustic returns and create three-dimensional images of their surroundings could lead to greater benefits.

Origin and Mechanism

The mechanisms of insect flight/fish swimming and the mechanics of animal-inspired control surfaces have been reviewed earlier (16-20). The reader might also like to refer to the special journal issues on biology-inspired engineering (1,5,21). Engineers can find a summary of the aspects of the fluid dynamics of swimming and flying animals that biologists think are of relevance in Ref. 22. They may also see how gravity, jets, pumps, friction, and waves are being dealt with by swimming and flying animals and the diversity of boundary conditions and solutions for the same problem statement—after all, there are 1000 species of bats and 28,000 species of fish. While engineers may shudder to openly speculate, biologists consider speculation an extremely useful tool for research. Biologists, who in general are strong in observation and intuition, tend not to be adept in the mathematical tools of fluids engineers. A teaming of engineers and biologists could be very fruitful in bringing rigor to the evaluation of mechanisms and reigning controversies, such as follows: Are rotational effects or wake capture new phenomena? Are they present in flying animals? Is the leading-edge vortex spiraling and stable?

One can go farther by swimming and flying than by walking. So, swimming and flying have given a vast opportunity for diversity to animals. The biomechanics of swimming and flying are treated in Ref. 23. A comprehensive account of what is known about insect flight and the directions of future research is also available (24). The reader should also be on the lookout for a coming treatise on the biomechanics of flying by Ellington.

Our understanding of the mechanisms of high-lift in swimming and flying animals is based on scaling laws and models (such as physical and analytical models), but largely on physical models. Scaling laws have been mostly based on experimental observations of live animals. Physical modeling has been based primarily on experiments with model wings (in the case of flight) and on live animals (in the case of swimming). Computational fluid dynamics and quasisteady modeling have provided verification and clarification of the physical models to some extent. The quasisteady models provide design laws for scaling. The models have provided checks on internal consistencies in measurements and on our understanding. Controversies between physical models and differences between robotic models and live animals have helped to advance our understanding. In what follows, the understanding from these various approaches is first treated separately and then synthesized. Caution needs to be exercised in linking biorobotics to animal mechanics too sanguinely. For example, sometimes the leading-edge vortex (LEV) has been likened to the delta wing LEV. However, the delta wing has a detached vortex lift, whereas the flapping wing has an attached vortex lift. Of course, neither is shed and both are stable.

The high-lift mechanism of swimming and flying animals has been examined from several different perspectives. The emphasis has been on vorticity production on solid surfaces, the spatial distribution of vortices in the wakes, and measurement and modeling of the forces produced. The approaches may be likened to observers trying to decipher what an animal is like based on its footprints. One group of observers has managed to collect the information from under the foot while the animal was in the process of treading on the surface, while another group is examining the footprints after the animal has already left. Some researchers have looked for evidence of the mechanism on the control surface but on scaled models of dragonfly, fruit fly, and abstracted penguin wings. Others have extensively explored the behavior of vorticity in the near wake using the particle image velocimetry (PIV) technique with live fish in controlled laboratory flows. The notable results are summarized as follows. Ellington and Dickinson showed that dynamic stall is the primary high-lift mechanism in insect flying. Dynamic stall has been implicated for high hydrodynamic efficiency of propulsion (5,8). Direct evidence that fish exploit vortex flow properties for minimization of the cost of locomotion comes from the PIV work, where it was found that trout slalom between Kármán vortices with lowered muscle activity (25). It has been shown that fish caudal fins have a universal dominant Strouhal number of 0.25–0.35, and they produce a reverse Kármán vortex train of thrust jets (26).

In science, new diagnostics have led to new understanding, new data, and new product development. The use of digital particle image velocimetry (DPIV) for free-swimming animals in a controlled laboratory environment has allowed the development of new hydrodynamics models of fish swimming mechanisms for cruise and turning (27). Forces and moments produced by free-swimming fish can be estimated from DPIV wake vortex traverse (28). Fish with similar morphologies, such as superperch and sunfish, were found to use vortex dynamics differently. For this reason, one could argue that investigation of muscles and actuators is inherently linked to unsteady hydrodynamics and should be carried out in an integrated manner for comprehensive understanding. Some authors have focused on the near-wake vortex structures and not on the flow over the control surfaces. The following modern measurement techniques, if used for flow over the control surfaces, might fill this gap and lead to further developments. A projected comb fringe method of tracking the deformation of the transparent wings of a dragonfly in real time in free flight has been developed (29). This method allows identification of a body-centered coordinate system using the natural landmarks on the dragonfly. The comb fringe pattern is projected onto the wing with high intensity and sharpness, and images of the distorted wing are then recorded using a high-speed camera. (The only assumption is that the leading edge is rigid.) The instantaneous attitude of the fly is also measured. This method needs to be explored in water. One method that might be useful in the list of contexts mentioned below is multi-exposure digital holographic cinematography. Such a portable instrument in fluids engineering context has been developed (30). Over a depth of field on the order of 1 mm–1 cm, one can compare scanning planar systems with holograms, both with similar resolution. Measurement of velocities instantaneously over a larger depth of field is the advantage of the holographic method. The holographic method produces a large amount of data, and one tends to analyze only a small fraction of the data. Further development is expected to focus on the improvement of the quality of holograms and automation of analysis of holograms. Fluid velocity diagnostics based on digital imaging techniques have matured. They have been widely used by biologists and fluids engineers to examine wake vortex structures. However, this technique has not been used to examine the boundary layer flow on the lifting surfaces, which is the origin of the vorticity. This region is thin, particularly in animals, so measurement there is challenging. Movements of surfaces are further complications. But how to combine the above fringe method of measuring the movement of flexible, solid lifting surfaces with a diagnostic of the LEV roll-up in a live animal is perhaps the ultimate measurement challenge in biorobotics. Another area where high-resolution surface movement and flow velocity diagnostics would be useful is in exploring the mechanism and function of small surface roughnesses and irregularities that are widely found in the control surfaces of animals. Limited scaled-up experiments do not indicate what the value of these surface irregularities is and, in fact, suggest deterioration in performance. Swimming animals have mucus, so surface hot films cannot be used on such flexible surfaces. The holographic technique could be useful in such flow problems and could also be useful in investigating octopus suckers from behind roughened Plexiglas walls to understand if suckers are more active than they are credited with being (9). For example, to determine if sucker adhesion to a porous surface is actively controlled, it would be useful to track the suckers’ nerves, the motion of their microscopic surface irregularities, control of mucus surface tension, and flow rate with cup pressure, simultaneously. Such experiments would utilize advanced measurement techniques with animal-inspired active control to explore their fluids engineering value. The fringe method can give micrometer-level resolution in real time and, thus, could prove useful to fluids engineering investigations of intricate lifting surfaces of small swimming and flying animals. We have emphasized the importance of free-flight and free-swimming experiments in animals. These are difficult to conduct. High-speed photography of insects in free flight has been carried out (31). A projection analysis technique that measures the orientation of the animal with respect to the camera-based coordinate system is used. The wing kinematics and body axes can be obtained from single frames.

Origin of High-Lift as Gleaned From Flight of Insects

In this section, we examine the wings of flying animals and pectoral fins of swimming animals as siblings, but treat the caudal fins of swimming animals differently. Also, with practical transition in mind, among vortex-based mechanisms we focus more on LEV, reverse Kármán vortex streets, and traveling waves, and leave others as tentative. For example, in flapping fins, there is general agreement regarding dynamic stall as a high-lift mechanism. However, there is some controversy regarding rotational effects and wake capture to be of general relevance.

Clap and Fling Mechanism of High-Lift

We first consider the rather uncommonly observed clap and fling mechanism in flying animals. In clap and fling, a pair of lift- and thrust-producing control surfaces is subjected to antiphase rotational oscillation and translation and the angle of attack constantly changes. With this mechanism, it is essential to have the surfaces in pairs. The earliest systematic investigation of insect high-lift and physical modeling (32) was followed by the analytical two-dimensional and inviscid modeling of the clap and fling mechanism (33). A series of experiments and physical modeling (34-38) clarified the mechanism and set in motion a torrent of interest. LEV was implicated in high-lift and soon became the focus of investigations and applications that continue today. Flow visualization experiments with a pair of scale-model wings of wasps were carried out in an attempt to explain how they sustain their weight in flight in a low-density medium such as air—something that is difficult to account for by several factors with classical aerodynamics (32). The clap and fling lift enhancement mechanism denoting the 0–180 deg and 180–360 deg phases of the wing motions was proposed. During clap, the leading edges of the two wings first come closer, producing two LEVs, which are the sources of high-lift. Then, the trailing edges rotate to close, ejecting the intervening fluid as a jet and augmenting the thrust. Subsequently, the leading edges rotate apart, again forming two LEVs. This is followed by the trailing edges rotating and translating apart, which again rushes in fluid as a jet and augments the vortex lift. During both the clap and fling phases, vortices do not form at the trailing edges. The LEVs form first during both clap and fling, which probably inhibits the formation of the trailing edge vortices. Other explanations for the absence of trailing edge vortices also appear in literature. The problem with this model of high-lift has been that many insects never clap, even though 25% higher-lift is produced compared with conventional wing beat (39)—probably because clapping damages the wings or because the wings have higher drag during forward flight. Because the clap and fling mechanism is not widely prevalent in nature, Ellington and co-workers resumed the search for the ubiquitous mechanism of high-lift. The stable attached LEV is the subsequent discovery implicated in high-lift, attributed to Ellington, which has withstood the pressure of time. It is presented below in various manifestations in flight and in swimming, also spurring novel applications. This review is built on this kernel. High-speed photography of many different insects in free flight shows that there are many variations of the clap and fling mechanism (31). How much the two wings touch and how far they stay apart vary between species and during maneuvering. It may be that the separation distance provides a fine control of the lift forces produced (31). The insect lift enhancement research shows two kinds of insect and bird wing beats—clap and fling (which is less prevalent) and conventional wing beat. LEV is produced in the latter. Maximum lift per unit flight muscle mass is 5463Nkg1 in those with conventional wing beats and 7286Nkg1 in those with clap and fling (39). Insects using conventional wing beats and birds and bats had the same former limiting muscle-lift characteristic, implying evolutionary convergence in performance but not in morphology, which remains diverse. In other words, each animal has retained its specialized wings and kinematics while achieving a universal level of efficiency characteristic of the type of their wing beat. The present review implicates the near-universality of LEV for conventional wing beat.

Leading-Edge Vortex Mechanism of High-Lift

The LEV mechanism is the most commonly observed wing kinematics in flying and swimming animals. In contrast to the clap and fling mechanism, with LEV a single control surface simultaneously heaves and pitches at the same frequency with a preferred phase difference between the two, whereby the angle of attack constantly changes. In addition to heave and pitch, or roll and pitch, twist may also be present in the wing/fin. Insect and bird flights have been modeled on the lines of propellers and rotating disks (34-36,40). The rate of change in momentum flux in the downward jet is equated to the weight. This analytical approach remains the foundation of experiments and of physical models. Experiments and numerical simulations have focused on circulation in the wake. For many insect wings, the spanwise variation in chord can be described by a beta function, implying universal wing loading behavior (41). The presence of LEV on Menduca sexta has been shown (42). Keeping these vortices attached for as long as possible is a strategy that insects probably use. Such studies on actual full insects are rare and difficult. The strategies that animals use to keep the stall vortices attached to their wings are open research topics. Research on the high-lift of animal control surfaces treats hovering and cruise separately. Biologists tend to conduct biomechanics experiments both on real animal wings and on models of animal control surfaces that are accurate to minute details. In hovering animals, in the Reynolds number range from 1100 to 26,000 and for aspect ratios of 4.53–15.84, aspect ratio has little effect on force coefficients (43-44). The cause is attributed to the presence of clear LEVs. On the other hand, in conventional propellers (including wind turbines), delayed stall occurs only near the wing root. In the above, the fin aspect ratio is given by AR=s/c, where s is the span and c is the chord of the fin. The plate geometry ratio R=ctip/xtip has been used to compare rectangular and triangular approximations of insect wings, such as butterfly wings, where ctip is the chord at the tip and xtip is the distance to the tip from the axis of rotation (45). Dragonflies align their stroke plane normal to the thrust in contrast to what was previously thought (46). Measurements of thermal changes after flight show that their mechanical efficiency is between 9% and 13%. The maximum muscle specific power is 156–166 W/kg.

Much controversy exists in our understanding of animal flight mechanisms or scaling laws. If dynamic stall is such a great boon from nature, then are there any system limitations in scaling up? The traditional view has been challenged (47). It was thought that mass specific power from flight muscles varies as m1/3, where m is the body mass. In other words, less power is available with increasing mass, and different animals can fly in narrower and narrower speed ranges. Instead, it can be argued that lift production deteriorates with increasing size at lower speeds and mass specific power is not an intrinsic criterion (47). Force and moment coefficients can be of instantaneous values of forces and moments or of averaged values over several cycles. Force (F) such as thrust or lift and drag is expressed as a coefficient, based on fin planform area or the swept area of the trailing edge, the former of the form as C=F/12ρU2cs, where c is the fin chord and s is the fin span.

Wing interactions

The dragonfly uses fore and hind wings to fly. Wing sets can interact strongly. Even minor changes in wing kinematics can lead to dramatic changes in the forces produced. The effects of all four wings can be modeled as a single actuator disk (46). The vortex interactions of a pair of two-dimensional upstream and downstream wings, cylinder and wings (48), and also the interactions of fish swimming with upstream Kármán vortices (25) are considered later. The flight muscle efficiency of insects is less than 10%, and their muscles have a good elastic storage of the inertial energy to oscillate their wings (4). How insects manage wing rotation during turning has been examined (49). Direct evidence of active control of timing between the left and right wings shows that this is done at the ends of strokes when the wing flips. The flip control in flying insects is then a method of executing maneuvers. Measurements of lift and drag and flow visualization on impulsively started two-dimensional flapping insect wings at an intermediate Reynolds number of 10–1000 have been carried out (50). Studies on impulsively started wings are instructive for insect flight biomechanics. Several experiments have reported that, in impulsively started bluff bodies, the peak transient forces lag wing acceleration (51-56). The aerodynamics during wing flip (i.e., rapid wing rotation during upstroke-to-downstroke transition), which is more prevalent in insects, has been investigated (57) using two-dimensional wings. It has been observed that the generation of maximum lift is increased if the wing travels through the wake of previously generated vortices, and a lift coefficient as high as 4 has been reported. Force measurements and flow visualization have been carried out with tethered fruit flies (58). Each cycle was found to produce one vortex loop. No shedding of wing tip vorticity has been observed. The circulation of the vortex loop has been estimated and an unsteady high-lift mechanism confirmed, and a small but observable phase lag in the force time history relative to the wing stroke has been reported—the measured forces are generated after some delay from what one would expect from a visualization of the vortex patterns. The reasons are not definitively known. This delay could be related to Wagner effects, which are treated later (5,17). A large data set of time histories of forces produced for a large parameter range of fin oscillation is available (59). The Reynolds number is 115. Stroke plane deviation between the left and right wings of insects is suggested as a control scheme for turning. The authors also present a quasisteady model. The inadequacies of their model, particularly for drag, have led them to question past estimates of mechanical power based on wing kinematics. From examining the forces on a hovering, flapping, mechanical wing starting from start, it can be concluded that force production is influenced by vortices produced in previous cycles (51). This is known as wake capture and is thought to be an acceleration-reaction force caused by the downwash from vortices formed in the previous cycles acting on the fin (60).

Two-dimensional computations have been compared with measurements on three-dimensional robotic foils simulating fruit fly wings (61). For hovering, pressure forces make a dominant contribution to fluid forces—something that would escape PIV diagnostics. Interestingly, the disagreements between computations and measurements become more obvious during the periods when the foil decelerates and accelerates at the ends of strokes. We note that circulation does not vary along the span in a two-dimensional foil, and tip losses of finite span are absent. It is unclear what lessons can be unambiguously learned by comparing two-dimensional computations with three-dimensional foil measurements where it is known that spanwise flow plays an important role in LEV stabilization.

The presence of the LEV due to flapping foils at low Reynolds numbers of 120 and 1400 has been confirmed (62). In the past, LEVs were not seen clearly below a Reynolds number of 5000. Further, it has been shown that at the lowest Reynolds numbers the LEV is stable and spirals from the root to the tip of the foil. However, the severity of the tip-ward flow is Reynolds number dependent. There is a large unexplored area of theoretical research in flapping foils—namely, the Reynolds number dependent stability of leading-edge dynamic stall vortices.

The quasisteady model originally developed for hovering flight has been modified and extended for forward flight (63). Measurements indicate that added mass effects make a small but measurable contribution to the forces produced. Detailed measurements of the velocity field around dynamically scaled flapping wings of insects have been carried out (64). It was found that there is a stable pair of counter-rotating vortices at the leading edge, rather than a single vortex. Extensive smoke visualization of the flow around free and tethered flying dragonflies has been carried out (65). The work largely confirms the attached stable LEV model of insect flight. Spanwise flow is found to be present in both directions but is not thought to be dominant. The LEV is formed when the angle of attack increases rapidly. Qualitative differences are found between model studies and those of live dragonflies. Both the formation and shedding of LEVs are controlled during extreme changes in angles of attack. The mean farfield around flying insects has been related with the nearfield wing kinematics, and semi-empirical theory has been developed (66-67). The mean induced flow is approximately a function of flapping frequency and stroke amplitude, and the remaining effects are accounted for by a calibration factor that is wing shape dependent.

In addition to LEV, there can be other mechanisms in insect flight, such as wing-wing interactions and wing-wake interactions (17). Traditional aerodynamic theories predict that performance improves with aspect ratio and stiffness. Swimming and flying animals have a vast diversity in aspect ratio and flexibility of their lifting surfaces. Unsteady potential flow analysis shows that aspect ratio and the proportion of wing area in the outer span determine the optimal wing form. Traditional notions apply only to low frequencies of wing motions and when the wings are stiff and tapered. Further work is needed to incorporate the nearfield unsteady wing kinematics into theoretical models of wing shape optimization.

Measurements of time histories of forces produced by a flapping wing of a fruit fly show that most of the lift force is attributable to two spikes produced near stroke reversal (68). One of the spikes correlates with wing rotation, and the other occurs after the rapid wing rotation during stroke reversal. Combes and Daniel (68) attributed the rotation-dependent first peak in lift to a rotational mechanism similar to the well-known irrotational (inviscid) Magnus lift that is produced by the flow past a rotating cylinder. They attributed the rotation-independent second peak to wake capture, which is an interaction with the vortex formed during a previous cycle. These notions have been challenged (69). An alternative explanation is that the first peak is due to vorticity produced because of wing rotation, and the second peak is because of reaction to accelerating an added mass of fluid (70). Finite element computation of the forces produced by a fruit fly wing has been carried out (71). The results are qualitatively similar to the measurements (68). Some 50% of the forces are generated by the outer 25% of the wings. Advancing the phase of wing rotation with respect to stroke reversal was found to enhance force production, and the combination of translational and rotational mechanisms was thought to be important. A spiraling spanwise flow in the LEV was not found (72). Also, the flow due to a maneuvering fruit fly has been simulated (73). Both the wings and thorax, albeit in abstracted forms, were considered. There is a dearth of animal or biorobotic data on maneuvering to allow simulations to be compared accurately. Experimentally observed wing kinematics was used to show that turning (a sudden turning called saccade) involves a phase difference of 13 deg in the stroke angle between the left and the right wings, and the angle of attack in the inner wing is smaller by 6 deg. It was found that the leading edge and the tip vortex form a loop that is shed as a lambdalike vortex. It may be that the wake vortex loops for maneuvering animals, compared with the “simple” ring or elliptical vortices due to straight motion, have higher azimuthal modes of distortions. The role of vorticity structure harmonics in flight control is unknown. As synthesized in the section on LEV classification, each animal might have its own characteristic wake vortex topology produced during typical turning.

Effects of camber

Camber deformation in insect flight has minor effects (50,74). But, some show otherwise (29). Measurements on free-flying dragonflies have been carried out in the laboratory at a Reynolds number of 4×104. Positive camber deformation of the hind wing during the downstroke generates a vertical force for supporting weight, and negative camber deformation of the wing during the upstroke generates a thrust force. Some have speculated that the time-varying camber deformation is a strategy for delaying the formation and shedding of LEVs and enhancing the delay of dynamic stall (29).

How sinusoidal is the wing motion in insect flight?

Photographs of insects in free flight show that, as a first approximation, the wing motion may be considered sinusoidal (31). However, there is an unmistakable presence of durations of higher accelerations and decelerations at either end of the wing beat, with constant velocities in the middle of half stroke. The second and third moments of angular accelerations are, respectively, 4% and 9% lower than those in simple harmonic oscillations.

Generalized wake vortex model for bird flight

Experiments with bird flight in a very large wind tunnel have been carried out in an effort to develop a universal model of the wake vorticity pattern (75). For one species (thrush nightingale), the entire speed range up to 11 m/s was covered. For birds, the mean flow speed can vary over 1–20 m/s and the mean chord over 1–10 cm. Thus, the Reynolds number can vary by a factor of 200. The work is a description of the Reynolds number effects on the wake vorticity. At low Reynolds numbers, the wake may appear to be dominated by elliptical vortices and, at high Reynolds numbers, the wing tip trailing vortices dominate the wake. However, the wake pattern is basically universal—it consists of a train of a pair of elliptical vortices followed by a rectangular vortex, the two being interconnected. The elliptical vortex is formed during the upstroke, while the rectangular vortex is formed during the downstroke. The vortex structures have sufficient momentum to support the weight of the bird. Note that dragonflies produce significant lift forces during the downstroke and thrust during the upstroke (29). It may be that the elliptical vortex represents lift forces and the rectangular vortex represents thrust force; the former is more obvious at lower Reynolds numbers and the latter at higher Reynolds numbers.

Classification of leading-edge vortices

How many kinds of LEVs have been reported? The preliminary answer is two or three or four based on their topology. It is unclear if the variations are attributable to the differences in the sources, namely, the insect species (76). The LEV descriptions and their variations are based on flapping mechanical models of a wasp (37) and of a tethered hawkmoth and dragonflies (77), and on tethered hawkmoths (72,76) and fruit fly models (7). All descriptions of LEVs satisfy Kelvin’s theorem that all vortices either form continuous loops or end on the surface. Based on Kelvin’s theorem, there are two classes. The LEVs are differentiated largely based on whether the two LEVs from the two wings are connected at their roots over the thorax to form one continuous vortex, or whether the two LEVs attach to the solid surface at the root. If the two vortices connect at the thorax, then they inflect downstream to do so. Otherwise, there is no inflection and they attach to the surface at the root.

What about spanwise flow in the LEV? Maxworthy (37) pointed out that the spanwise core flow is necessary for stability, that is, for the LEV to remain on the near surface. In its absence, the LEV would continue to be fed with new vorticity generated at the leading-edge stagnation point and grow and, given enough time, would eventually be shed. Maxworthy (37) and Ellington et al. (72) clearly indicated spanwise core flow in their LEVs. Dickinson et al. (7) indicated spanwise flow but downstream of the LEV and not in the core. Dickinson et al. (7) reported a spiraling flow and a conical LEV with a root focus situated near the root. Therefore, a spanwise core flow can be expected. Dickinson et al. (7) observed that a boundary layer fence did not lead to the shedding of the LEV and suggested that the spanwise core flow is not essential for stability even in a conical LEV. Luttges (77) claimed two-dimensional flow and did not show any spanwise flow at any phase of wing motion. A synthesis of results shows that the Strouhal number, time period of flapping, and circulation can probably be tuned so that a vortex can grow in the absence of spanwise core flow, but not enough to be shed into the wake during the time period of flapping (76).

Insect LEVs are conical, blooming from the thorax outboard, but much less so in the case of the tethered hawkmoth and dragonfly LEV (77). The tethered hawkmoth (72) and fruit fly model (7) LEVs are about 30% of the chord at midspan, and the tethered hawkmoth and dragonfly LEVs are higher. However, the tethered hawkmoth (76) LEV is in a class by itself, bearing some commonality with all of the above. This LEV is uniform from wing tip to wing tip through the thorax, with core thickness being about 10% of the chord and hardly any spanwise core flow. The LEV supports 10–65% of the bodyweight.

What about in water? Surface shear measurements in a penguin wing model flapping below 2 Hz in water have been carried out (78). It was shown that the leading-edge stagnation point oscillates in space about the mean location sinusoidally in synchrony with the flapping waveform. This would mean that the LEV and the spanwise flow also oscillate in space with time. In other words, the LEV is quasistable and not steady. Surface sensor array and complementary dye flow visualization clearly identify two nodes—the forward stagnation point and the reattachment point. Including the rear stagnation point, there are three nodes. Arguing conversely, it can be asserted (79) that the LEV probably has a saddle at the wing base outside the wing. Future work should focus on stability analysis to determine if spanwise core flow in the LEV is essential for LEV stability. The evidence so far seems to be that every swimming and flying animal has its own kind of LEV critical point topology. Ideally, one needs to do experiments with live animals rather than robotic models if one seeks to understand the mechanism of animal flight or swimming. A close-scaled replica of the entire animal would be the second choice. However, for primary effects (such as whether the LEV is present or not and its contribution to forces and efficiency), the value of studies on robotic models of the control surfaces of animals has been vindicated.

Scaling law of flight

The variation in wing kinematics of birds with body size has been examined (80). It was found that the common Strouhal number for direct fliers is 0.21, and intermittent fliers are at 0.25. Strouhal number is defined as fA/U, where f is the wing beat frequency, A is the stroke amplitude, bsin(θ/2), where b is the wing span and θ is the stroke angle, and U is forward speed. The stroke angle follows the empirical power relationship θ=67b0.24. Direct measurements of propulsive efficiency are lacking. It is believed that the propulsive efficiency reaches maximum values at these Strouhal numbers. Currently, animals are thought to oscillate their wings or tails in the Strouhal number range of 0.2–0.4. Future research should examine if the optimized Strouhal values vary with cruise and different kinds of maneuvering, such as hovering and constant-radius turning. Optimization experiments have been carried out on a two-dimensional translating and rotating flat plate to show that in the absence of rotation a stable LEV is not formed (81). The ratio of the horizontal distance traveled by the plate to the projected chord is believed to be a key parameter for the formation of the LEV.

Bat flight: Effects of variable camber, droop, and membrane tension

Bat flight, which is dominated by large camber, droop, and the use of a thin membrane in tension, is being examined (82). The downstroke consists of abduction, stretching of the wing, and large cambering and droop, while the return upstroke consists of adduction and retraction of the wing, resulting in loss of camber, droop, and membrane tension. During the downstroke, a wing tip vortex is shed. Stall occurs at higher angles of attack and is gentler compared with a similar wing with nondeforming membrane. A qualitative model of the compliant membrane is given, proposing that aerodynamic load is proportional to membrane tension. Direct evidence of the existence of any LEV and high-lift is yet to be available.

Vortex method

Simple models for analyzing the force production due to the wing beats of insects have been proposed (32,41). Also, a vortex method of calculating the pressure distribution of insect wings has been developed. The forces and moments from these three methods have been compared with measurements (45). The methods are in good agreement when the nondimensional plate geometry ratio R is less than 0.5. The simple models are not accurate when R1 (low-aspect-ratio wing). It is also not possible to take into account the interference between the two wings in these methods. The vortex method is accurate when R is 1 or is large (>2) and can take into account the interference of two wings. It is important to calculate the added mass effect accurately—particularly in the case of three-dimensional multiwing insects (45).

The vortex method has been used to analyze the takeoff flight of the butterfly (74). To do that, the time histories of normal force and moment on a pair of finite triangular plates rotating symmetrically about an axis have been computed (45). The potential flow method is used to compute the pressure field around the plates. The total velocity potential is divided into two components—noncirculatory and circulatory. The noncirculatory part of the velocity potential satisfies the wall boundary condition and Kutta condition at the edge. It does not shed vortices into the flow and is expressed by sources and sinks. The circulatory part does not affect the boundary condition on the plate and is generated by the vortices shed into the flow. The noncirculatory part of the velocity potential satisfies Laplace’s equation, which is solved using the vortex lattice method. The total velocity potential is also obtained from Laplace’s equation. Flow visualization is used to identify the outer edges where dominant vortices are formed that induce higher velocities and greater effect on pressure distribution on the plate. The wake is a sum of these vortices shed from the outer edge. These vortices reside on a surface extending to the triangular plate. The strength of this vortex sheet is calculated from the circulation at the four corners of elements of numerical calculation. In this manner, the velocity induced by the vortex sheet is calculated. Unsteady Bernoulli’s equation is used to calculate the total normal force and moment from dynamic and impulsive pressures. The noncirculatory part of the normal force has two components—one is proportional to the angular acceleration, including the added mass and added moment of inertia effects; and the other is proportional to the square of the angular velocity. Expressions of shape factors are given that are proportional to the added mass and added moment of inertia, which are calculated by both numerical and experimental methods (74). The added mass and added moment of inertia are functions of the opening angle between the two plates or wings and are constant in the case of one plate. The shape factors are also functions of the plate shape and separation distance of the plates. A similar method has been given where the flow is taken to be the summation of distributed singularities of sources and sinks on the solid surface and the shedding of discrete vortices. However, instead of using a panel method for numerical solution, Dickinson and Gotz (50) gave an unsteady analytical solution where the unsteady Laplace equation is solved to satisfy the Kutta condition at the leading and trailing edges. The method is used in a two-dimensional, rigid flat plate only. Comparison is made with measurements. It is concluded that the forces originate from added mass effects that act immediately and from the delayed effects of the shedding of leading and trailing vortices and body image vortices.

Potential flow theory of unsteady wings

An analytical method based on potential theory has been developed for the calculation of aerodynamic forces due to two-dimensional wings that are slightly cambered and are undergoing heaving, surging, and feathering motions (83). The suction force at the leading edge of steady airfoils is obtained using Blasius’s formula. Polhamus’s leading-edge suction analogy of vortex lift is used to treat the flow separation at the leading edge. An analytical inviscid method has been given for calculating forces produced by two-dimensional models of fruit fly wings (84). The wing is thin, rigid, and uncambered. A potential reference is developed in which the wing is at rest, whereby Blasius’s theorem is applicable. The model includes bound circulation and also a LEV circulation that is stationary with respect to the plate. The Kutta–Joukowski condition is then applied at both edges. To allow comparison with measurements where the wings are three dimensional and the velocity changes along the span, a method simpler than the blade element method is used. The velocity used to evaluate forces is taken as the wing tip velocity times the square root of the nondimensional second moment of the wing area. Good agreement is obtained with the measurements (59). It is proposed that because the stabilization of the LEV is attributable to flow three-dimensionality, wing camber might be an essential requirement.

Origin of High-Lift as Gleaned From Swimming Animals

Flying animals need to support their body mass against gravity, but swimming animals such as penguins do not very much need to. (Buoyancy devices are not considered here). Therefore, differences in the wings of swimming and flying animals can be expected. A golden eagle has nearly the same mass (4.7 kg) as a Humboldt penguin (4.2 kg). However, the planform area of the eagle wing is 38 times larger than that of the penguin (85).

Fish that use their body and caudal fins to move are fast swimmers. Those that use fins are good at maneuvering but are not fast swimmers. In this review, we concentrate on high-lift that comes primarily from the control surfaces (such as fins), and we focus, in particular, on the pectoral fins of sunfish, boxfish, bird wrasse, dolphins, and penguins, which include a range of decreasing flexibility (increasing rigidity) and increasing aspect ratio. In large-aspect-ratio wings, a substantial part of the lift force is produced in the outer part of the wing. Therefore, interesting questions can be raised. Are flexibility and aspect ratio two sides of the same coin? Is flexibility an extreme means for producing the results of large aspect ratio in low aspect ratio?

Many of the principles of fish swimming that are still with us date back to critical observations of long ago (86). For motion, a fish generally uses its body to apply lateral forces in the water that cancel in the time mean but produce a net forward thrust. Body motion is in the form of a wave called a flexion. The form of this wave along the body is used to classify fish into three or four categories. Anguilliform swimming, named after eels, has been studied much less. In eels, the flexion amplitude remains unchanged, nose to tail. There is no discernable jet in the wake of an eel (87). Sharks, which are also of the anguilliform, swim constantly and are suspected to be efficient. In carangiform and subcarangiform swimming, the flexion amplitude increases toward the tail, and more of the front part of the body is rigid. Lighthill used his elongated body theory to propose that this form of swimming is most efficient because there is the least amount of body motion and thrust is produced only in the tail. Carangiform swimming produces a jet in the wake. Most fish fall in this category and have been widely studied. In thunniform swimmers, only the caudal fin and a small part of the tail body move. The tuna fish, with an active crescent-shaped caudal fin, is an example.

Due to viscous friction, swimming is thought to require more power than is required by human-engineered land vehicles (88). But aquatic animals are frugal in oxygen consumption as a result of breath holding. For example, the aerobic capacity of emperor penguins is lower than that of an emu or dog of the same mass (89). This apparent paradox, which is akin to Gray’s paradox (105), can be resolved by proposing that aquatic animals resort to drag reduction techniques and need to produce such minimal thrusts. However, aquatic animals may not only be lowering their drag but may also be lowering their abdominal temperature to lower metabolic rates for energy saving (90). This possibility points out the importance of systems approach rather than a purely fluids engineering approach, when it comes to understanding the mechanisms of swimming and flying animals and their application.

Classification of Aquatic Propulsion

A survey of aquatic propulsion, followed by an analysis based on elongated body theory (91), has led to the classification of swimming in terms of Reynolds number (low and high), efficiency (greater than or less than 0.5), the variation in body undulation with length, and where in the body length the undulation starts. The theoretical hydrodynamic reasons for the distinctions between anguilliform and carangiform swimming can be deduced. In the former, the mass of water energized by the anterior part is not in phase with the trailing edge motion, resulting in a lower efficiency. In the latter, the amplitude of the basic undulation grows toward the trailing edge and the energized water is in phase with the trailing edge, resulting in a higher efficiency. The explanation seems to be that the distribution of total inertia along the length, a combination of fish body mass and the virtual mass of water, is optimized to minimize “recoil,” resulting in high thrust and efficiency. The evolution in several different lines to the common final result—namely, the lunate tail, which is a pair of highly-swept-back wings, for the enhancement of speed and efficiency—has been examined (92). The need to reduce caudal fin area in relation to depth to reduce drag without significant loss of thrust leads to this planform. The hydromechanical advantages of lifting surfaces require leading or trailing edges to bow forward. This last remark may bear some relevance to the convoluted form that flexible pectoral fins (such as those of sunfish) undergo (93).

To Flap or to Row?

Many fish use their pectoral fins for propulsion, and this is known as labriform locomotion. Swimming with pectoral fins has been described by biologists in their two extremes—namely, drag-based (i.e., rowing) and lift-based (i.e., flapping) (22,94). In rowing, which is used at low speeds, the fin moves forward and backward and there is little flow over the fin. In flapping, which is efficient at higher speeds, there is flow over the fin. Therefore, over a range of speeds, both types can be expected to be in use. The kinematics and related muscle activity of aquatic animals, focusing on the three-dimensional aspects of aquatic flight, have been examined (95). Bird wrasse, for example, primarily use the lift-based mechanism—the fin twists, thereby changing the angle of attack along the span. In the abducted position, the bird wrasse pectoral fin planform is similar to that of insect wings. Six muscles actuate the fin motion in antagonistic groups. A simplified linkage model of the fin has been proposed. A blade element model has been used to compare the mechanical efficiency and thrust produced by an idealized fin undergoing elementary sinusoidal rowing or flapping motion (96). In rowing, the fin rotates backward and forward about a vertical axis; in flapping, the fin moves up and down about a horizontal axis. Flapping fins are wing shaped and they taper away from the root, while paddle-shaped fins expand away from the root. Better performing pectoral fins of fish that rely on them for propulsion have a higher aspect ratio and a longer leading edge (compared with the trailing edge), and the center of the fin area is located closer to the root (97). Efficiency is found to be higher in flapping, while thrust is higher in rowing, and it is suggested that rowing is useful in low-speed maneuvering, while flapping is useful in power-conserving cruising. These classifications receive some support from measurements (98-99).

Experiments show that as the frequency of flapping is increased, a foil no longer produces drag but starts to produce thrust attributable to a clear reverse Kármán vortex street (100). Boundary layer thickness on the foil and Reynolds number do not play strong roles. It has been observed that fish and cetaceans flap their tails in a Strouhal number (fA/U) range of 0.25–0.35 (26). A thrust-producing jet is convectively unstable, with a narrow range of frequencies of oscillation (101). There is no modal competition between the natural mode (the absolutely unstable mode) and the forced mode, unlike that in bluff bodies. The flapping fin wake acts like a frequency-selective amplifier. Thrust reaches a maximum per unit of input energy at the frequency of maximum oscillation. The authors point out that saithe is an exception to the rule of preferred Strouhal number in nature and has a lower Strouhal number.

Flow visualization at a Reynolds number of 1100 and measurements of force and power at 40,000 on a two-dimensional heaving and pitching foil have been carried out (102). Propulsive efficiency as high as 87% was reported, which is similar to the 85% claimed theoretically for whale flukes (103). The following parameters were found to lead to optimum efficiency: a Strouhal number of 0.25–0.40, heave-to-chord (h/c) ratio of 1.0, angles of attack between 15 deg and 25 deg, and a phase angle of 75 deg between heave and pitch. For two-dimensional foils, the h/c ratio is important because maximum efficiency is achieved for h/c=0.751.0.

Based on flow visualization, it is concluded that the vortex dynamics responsible for high efficiency involves the formation of a LEV in every half-cycle, which amalgamates with the trailing edge vortex to form a reverse Kármán vortex street. More careful later measurements (104) have tended to lower earlier efficiency measurements made in the same laboratory (102). Efficiencies as high as 71.5% were reported, and the optimum phase angle between heave and pitch was found to be 90 deg for best thrust and efficiency. Therefore, the high efficiencies and the low angles of phase difference between heave and pitch for optimum efficiency and thrust in Ref. 102 are not supported. It has been shown (104) that a higher harmonic should be introduced to the heave motion to make the angle-of-attack time history sinusoidal. This produced a higher thrust coefficient at higher Strouhal numbers. Impulsively started foils are shown to produce mean force coefficients of up to 5.5 and instantaneous lift coefficients of up to 15.0, which could be useful for maneuvering.

Early History of Fish Biomechanics

The principles of swimming known to us are based on the early works of Gray (105), followed by Bainbridge (106-107), and Lighthill (91). The historical milestones of modeling, scaling, measurement techniques, and debates on the 50th anniversary of Bainbridge’s works on scaling laws of fish swimming have been recounted (108). Gray’s modeling work (105) on energetics and maximum speed focused attention on the relationship between fish speed and size. Bainbridge (106-107) carried out measurements in circular channels, which were replaced later with water tunnels, allowing more accurate measurements. He showed that tailbeat frequency controls speed, and he proposed a universal relationship of size, tailbeat frequency, and stride length (distance traveled per beat), U/L=0.25[L(3f4)], where U, L, and f are speed, length, and frequency, respectively. This is reminiscent of the advance ratio in propeller theory, J=V/2ϕnR=(V/(nR))/2ϕ, which is translational speed divided by the product of rotational rate and diameter, where V is the flight velocity, ϕ is the peak-to-peak wing beat amplitude in radians, n is the wing beat frequency, and R is the wing length (109). In other words, advance ratio is forward speed in wing lengths per wing beat divided by 2ϕ. Note that this analogy leads to the representation of speed in terms of body length per second—a legacy from Bainbridge (106-107) that survives today. Gray’s work (105) indicated paradoxes of unexplained differences between available and apparent power, and Bainbridge’s (106-107) representation of speed showed that large fish swim faster, but that their relative speeds in terms of body length are lower. The works of Gray (105) and Bainbridge (106-107) influenced the slender body model of Lighthill (110-111) and gave a framework for estimating power and efficiency.

Interaction of Body and Pectoral Fin in Swimming

The steady swimming and rising or sinking of sturgeon and shark have been compared, which determine where large vertical forces are produced—in the main body or in the pectoral fins (112). These are long, slender fish with pectoral fins. With their long body aspect ratio, these fish tilt their body in a manner similar to what is used in the underwater hydrodynamics of cylinders at lower speeds (L/D10, where L and D are length and diameter, respectively)—larger angles of attack at lower speeds to generate lift. This is one clue that pectoral fins are not needed to produce lift in such fish. The technique of near-wake traverse using DPIV was used to indirectly estimate the forces and moments produced. During steady swimming, the pectoral fins produce no lift; instead, the positive angle of the body produces lift and the two balance moments. However, sinking or rising is initiated by the pectoral fins to produce a starting vortex whose central jet thrust helps alter the pitch of the body. The rear half of the pectoral fin is used as a flap to do this. The authors point out that two-dimensional simplification of pectoral fins can be grossly in error. The interaction of the body and the pectoral fin is strong in sturgeon. The leopard shark also uses its body and pectoral fin interaction in much the same manner to control moments for cruise and maneuvering, such as initiation of rising and sinking (113). It further uses the dihedral angle between its body and its two pectoral fins to control roll motion. How does the bamboo shark control the morphology of its body and its slightly flexible pectoral fin for station-keeping near a floor, and how does it rise or sink (113)? The behavior is compared with that during steady horizontal swimming. This shark basically promotes maneuverability over stability. It uses a combination of body angle of attack (positive or negative angles and their amplitude) and the concavity of the pectoral fin (concavity upward or downward and the amplitude of the resulting dihedral angle) to produce the required vectored vortex jets.

Heterocercal Fish Tail: Why Is It Asymmetric?

High-speed photography and DPIV have been used to understand the role of heterocercal tails of free-swimming sturgeon (114). Long, slender fish such as sturgeon and shark have such tails. Homocercal fins are symmetrical, but heterocercal fins are asymmetrical and have unequal lobes—the vertebral column turns upward into the larger lobe. This question is too complex and there is a need to know the force distributions along the body of free-swimming sturgeon and shark (114). This topic is well suited to computational analysis and should consider maneuvering to reveal the mechanism.

Finlets and Caudal Fins: Are They Like Strakes and Delta Wings?

A synthesis of literature suggests that we should discuss finlets and caudal fins jointly because they might be working in a synergistic manner, although they do not seem to have been examined jointly in the emerging context of high-lift. Fish such as chub mackerel, bonito, and tuna have several small nonretractable triangular fins in the body margin between the main dorsal/anal fins and the caudal fins—that is, on both sides of the tail end of the body margin in the vertical plane. Some of them are rigid and flat, while others are flexible. It is unclear if the finlets are actively controlled. The total surface area of the finlets is only 15% of the caudal fin area. What is their role? It is hypothesized that these finlets direct the flow in the vicinity of the body toward the caudal fin to augment the vortex jet in the tail (115). This hypothesis receives some support from visualization—the finlets produce a combination of longitudinal converging flow and a counter-rotating flow with axial vorticity (116). The fish wake consists of a linked array of tilted, elliptical vortex rings with induced central jets (117). The minor axis of the elliptical rings remains equal to the span of the caudal fin irrespective of speed, while the major axis in the axial direction scales with speed.

The finlets and the caudal fins are closely located and produce vortex-dominated flows. Are they related? Some have thought that the finlets control turbulence or drag or cancel vortices (118-121)). The suggestion (122) that the finlets produce longitudinal flow to augment caudal fin lift has been both partially supported and criticized (123) based on morphology. It is suggested that vortex enhancement is marginal (123). While different biologists have focused on different species with variations in morphology, it would be useful to find any universal mechanism. None of the authors appear to have dwelled explicitly on vortex-based high-lift as the universal mechanism of finlets and caudal fins. We synthesize the available understanding to suggest the following vortex lift hypothesis to spur investigations. We draw analogy to the Swedish Viggen fighter jet’s high-lift aerodynamics. The Viggen aircraft has two small strakes upstream of the main delta wing; these strakes both operate at high angles of attack, whereby they both produce LEV and high-lift. The strake vortex enhances the delta wing lift. In a similar manner, we speculate that the finlets and the caudal fin work in unison to produce vortex thrust for propulsion. The finlets enhance the main thrust jet by producing a pair of counter-rotating vortices with an intervening jet converging toward the tail, and they are formed alternately along the left and right vertical surfaces of the fish body. The finlet vortices rest on the low-pressure side of the caudal fin and enhance its lift force and augment the jet. It would be useful to conduct computational evaluation of this hypothesis.

Lateral Lagged Oscillation of Symmetric Fish Tail Fins

The caudal fins of homocercal species such as mackerel have extremely symmetrical caudal fins, and the symmetry extends to internal musculature. However, it has been shown that the posterior part of the caudal fin has fine motor control and the tail moves laterally as an acutely angled blade (124-126). During the tail beat, tail height and area expand and contract. Lateral cyclic motion is lagged—the dorsal lobe (the upper part of the tail fin) leads the ventral lobe (the lower part of the tail fin)—and it undergoes a 15% greater lateral excursion. It has been suggested that such asymmetric motion produces upward lift during steady swimming (126). The role of this fine control is not definitively known. This precision lateral tail fin actuation problem might benefit from computational investigation.

Multiple-Fin Propulsion in Fish

Some insects have a pair of wings for propulsion and lift. By and large, fish probably use multiple fins more commonly to cruise or maneuver. Wake traverse using PIV visualization has been done to determine the forces produced by various fins in bluegill sunfish (127). For cruise, 50% of the thrust is produced by the pectoral fins, 40% of the thrust is produced by the caudal fin, and 10% is produced by the soft dorsal fins. For one example of turning, 65% of the force was produced by the pectoral fin and 35% was produced by the soft dorsal fin. The dorsal and caudal fin vortices interact to reinforce circulation, and they partition the force production among the fins. The control of moment may be an important determinant of multiple fin propulsion and their relative budgeting.

Production of Asymmetric Forces by Pectoral Fins for Turning

Fish spend a significant amount of time in turning compared with cruising. DPIV experiments on sunfish have been carried out to understand how asymmetric forces are produced by the pectoral fins that result in turning (127). The fins modulate the pectoral fin stroke timing and wake momentum. The pectoral fin on the side from which the fish is turning away produces a lateral force that is four times the force it normally produces during cruising. The pectoral fin on the side of the fish toward which it is turning produces a thrust force that is nine times the force it normally produces for cruising. The result of the former is rotation of the body, while the result of the latter is linear translation of the body toward the center of turning. Fish obviously have a controller, yet to be discovered, that can partition or resolve the force and moment vectors instantaneously and assign monochromatic tasks (forces or moments) to independent fins. It may be that force production in fish for maneuverability and cruising is apportioned in such a manner that the net ability is conserved (128). The hydrodynamics of bluegill sunfish and black superperch, which have similar fin morphology and are assumed to have similar reserves of energy, have been compared. Superperch have about twice the maximum speed, but sunfish are more maneuverable. They both use their pectoral fins to swim at low speeds and combine pectoral fins with the caudal fin at higher speeds. Pectoral fins are implicated in maneuvering. The superperch pectoral fin wake at all speeds consists of two vortex rings per fin cycle detached from the body. The sunfish pectoral fin wake consists of one detached vortex ring per fin cycle at low speeds and two vortex rings per fin cycle, with one attached to the body, at higher speeds. The orientation of the vortex rings is, however, characteristically different in the two—the sunfish pectoral fin rings always predominantly lie in the lateral plane, while the superperch rings predominantly lie in the horizontal plane. The orientation of the central jet in the vortex rings explains why sunfish are marvels at maneuvering and superperch excel in speed.

Maneuverability and Flexible Pectoral Fins

Fish that swim in circles work harder than those that swim straight (129). Power consumption density for propulsion based on red and white muscles, as well as that for underwater vehicles, is higher during maneuvering than during cruise (8). Fish having flexible pectoral fins are highly maneuverable. The sunfish’s pectoral fins are highly flexible, three dimensional, and have a low aspect ratio (130). PIV studies show that attached vortices are formed at both edges of their fin (5). A proper orthogonal decomposition of this fin’s kinematics shows the fin modes with the proportion of forces that are produced (131). The approximate three-dimensional vortex structure around an entire sunfish in steady swimming in the laboratory has been constructed from two-dimensional PIV measurements of velocity fields (132). Longitudinal vortex structures found near the tips of all fins are reminiscent of wing tip vortices of three-dimensional bodies in a uniform flow—the signatures of induced drag. The maneuverability of rigid-bodied fish, such as box fish, propelled by multiple flexible fins, has been examined (133). The results could help the design of autonomously stable underwater vehicles and automobiles. Most of the body of the box fish is made of inflexible bones, and its rigid body is restrictive of motion. Consequently, the fish has developed a set of fins to oscillate in a phase sequence to produce exquisite maneuvering ability in narrow confines. Flow visualization shows that large-scale tip vortex pairs are created at the sharp ventrolateral keels, and their trajectories relative to the body are manipulated to control stability autonomously. The body performs like a delta wing at a high angle of attack that has a detached LEV. One could conclude that the box fish is using its keel to produce the LEV, although largely to stabilize itself in a pre-existing stream. As a starting point to understanding fish motion, one could create a portfolio of the kinematics of pectoral fins, dorsal/anal fins, and caudal fins that fish (such as box fish, bird wrasse, etc.) use to produce braking, acceleration, spinning, cruising, hovering, and reversing (134). Generally, for maneuvering, fish control the phase synchronization of several fins to produce a maneuvering motion. Sunfish are an exception; they use their pectoral fins only for station-keeping. Further research is needed on the controllers that manipulate the phase between a set of fins, or the dynamic flexibility of one set of fins to achieve the same result, and on how sensors such as lateral lines are integrated with controllers to close the loop.

Jets or Fins?

Primarily, fish use fins and squid use jets for propulsion. What is more efficient and what is worth considering for application? Squid typically have five to seven times higher oxygen consumption than fish (135), which suggests that jet propulsion is inefficient in comparison. There are squid, however, that use a mix of the two, apparently to compensate for the deficiency (136). The limitation of jets comes from the fact that the rate of momentum transfer to water is greater with fins than with jets—the size of the bladder expelling fluid is limited and higher jet velocity costs more energy (=velocity squared). Jets due to ring vortices underpredict thrust, and entrained fluid also needs to be taken into account (137). Environments, nozzle surface quality, active control, and appendages can all affect entrainment. In jet-dominated creatures, their effects on entrainment need closer scrutiny.

Conclusions on Pectoral Fin Mechanism

The hydrodynamic control surfaces on swimming animals have been categorized as passive and active (20). Leading-edge tubercles of whale flippers and riblets on the skins of shark are passive devices that act as a boundary layer fence and viscous drag-reducing surface elements, respectively. Examples of active devices would include the flexible sunfish pectoral fins or penguin wings. Based on PIV measurements (made largely on station-keeping sunfish in a laboratory environment and not on maneuvering), the major conclusions for the biomechanics of the sunfish pectoral fin are as follows: The fin produces thrust throughout the movement cycle during steady swimming and does so by a combination of changes in the fin kinematics, which include (1) spanwise and chordwise flexibilities, which act to stabilize the upper edge vortex and orient the surface pressure force in the forward direction even during the outstroke; (2) active camber control of the fin surface; (3) an increase in surface area during the in-stroke to increase thrust; (4) surface deformation (cupping shape) to reduce within-stroke oscillation in lift (vertical forces) by producing dual simultaneous LEVs of opposite sign; and (5) a bending wave from root to tip to increase downstream (thrust) momentum. The penguin wing is much less flexible in comparison to the sunfish pectoral fin. The chordwise flexibility of the penguinlike wing increases its hydrodynamic efficiency from a maximum of 0.62 for rigid wings to 0.86 for an optimized wing, while the thrust coefficient remains unaffected (18).

Flexibility

The formation and evolution of vorticity from the wings and the body suggest that aquatic animals (such as sunfish) use their highly flexible fins to control the loading along the span, and the convolution is a dynamic optimization in synchrony with the unsteady high-lift mechanism. Recall that fish use lateral lines to sense the pressure field, and such a convoluted vortex sheet that might evolve into more than one vortex ring could offer a greater moment for stability control. But there is no evidence yet that the sunfish wake produces more than one vortex ring. Time-domain panel computation of flexible wings, whose planform is similar to that of whale flukes, has been carried out (138). It was shown that passive operation of the wing degrades propulsive efficiency. However, if the phase of the spanwise flexibility is carefully controlled with respect to the wing motion kinematics, propulsive efficiency can be enhanced. The wing tip should be moved in the same direction of the overall wing. An attached flow is assumed, so future work needs to account for what we now know about LEVs, appropriately scaled for aquatic simulation. A pneumatically operated flexible microactuator made of silicon rubber, circumferentially reinforced with fibers, has been used to build a flexible fin for underwater use (139). Shore stiffness is varied along the length by varying the density of the fiber reinforcement. Higher curvature is produced by increasing internal pneumatic pressure. A feathering motion has been produced.

Power

Because of the main role played by unsteady mechanisms, existing aerodynamic theories that use steady-state lift and drag coefficients cannot be used for estimating the induced power of swimming and flying (40). Yet, fundamentals relating circulation and lift are applicable. Vorticity is produced only on the solid surface of the wings and body. One could track the trajectories of points on the surfaces during a wing stroke and arrive at the vorticity sheet. For a sunfish, this sheet is going to be highly convoluted. During hovering, the vortex sheet is simpler than during maneuvering. The presence of this sheet is a result of force generation—loading of the wings and the body. The sheet quickly rolls into ring vortices to arrive at a more stable configuration. The work done to create the rings can be used to estimate the induced power (the force produced is the reaction of the vortex ring momentum per stroke period). Thus, accurate measurement of the ring vortices in the near-wake and of circulation is an indirect but practical tool for determining the induced power of swimming and flying animals. Many researchers devoted much effort to using dye, smoke, and PIV visualization to document the formation and roll-up of vorticity on the wing surfaces and also of its roll-up into large ring vortices in the near-wake of swimming and flying animals.

Understanding of Mechanism From Computational Fluid Dynamics

Insect flight covers a Reynolds number range of 10105(140). Swimming animals tend to fall in the lower part of the range—the lower range of the limit drops to 102 for swimming sperm. The distribution of Reynolds numbers for swimming animals and man-made vehicles appears in Fig. 10 in Ref. 19. A comprehensive theory of force production in swimming and flying animals is not available. Measurements, modeling, and numerical simulation are filling the void in bits and pieces. Numerical and analytical simulations of fruit flies of wing planforms that are slightly smaller than those in earlier works have been carried out (70). The computed time histories are similar to those measured (49,59), but with a constant shift to higher values. The claim in Ref. 72 that there is an attached dynamic stall vortex formed at the leading edge is supported; the vortex does not get shed and there is no stall. In agreement with other works (72,141), wake capture (59,68) does not exist apparently because the LEV is not shed. The Magnus effect as the origin of one of the peaks in lift has also been questioned (68). Note that lift produced by a surface at an angle of attack is Magnus-like, but it is unclear how a Magnus-like force can be attributed directly to the rotation of the wing about its span. In any case, a Magnus effect is irrotational, but a peak in drag accompanies the peak in lift attributed to a Magnus effect. Instead, added mass effects and vortex formations are the causes of the two lift peaks before and after the stroke reversal. It has been shown that the unsteady oscillation of the wings can indeed support the weight of hovering flies as measurements show (32). Wing kinematics that is yet unexplored might produce higher lift forces. The drag of fruit flies is estimated to be 1.27 times the lift force required to sustain the fly’s weight. The body mass specific power is 28.7 W/kg, the muscle-mass specific power is 95.7 W/kg, and the muscle efficiency is 17%. This drag-to-lift ratio is higher compared with those in large fast birds or in hovering helicopters. Computational methods (70,141) have been used to study dragonfly wing interactions, and very little of any interaction is found (142). Both fore and aft wings produce lift peaks during their downward strokes. During those times, they produce vortex rings with downward momentum.

Navier–Stokes computation has been carried out on a full bird wrasse swimming underwater using an adaptive mesh grid (143). The pectoral fins are flexible, although the dynamic geometry is not as detailed as that in later investigations of sunfish pectoral fins. Also, detailed time histories of forces produced on a bird wrasse are not available, and an accurate comparison of the computation is hindered. The authors in any case show that in the flexible fin swimming under water the LEV is large, is not of the spiraling type, there is no strong spanwise flow, and the LEV is shed during the upstroke. The flexible pectoral fin is dominated by a strong axial flow and not a spanwise flow. The forces produced by fish-inspired pectoral fins attached to a 30-cm-long and 10-cm-diameter rigid cylinder have been computed (144). The unsteady Navier–Stokes solver with automatic adaptive remeshing had an unstructured grid. Station-keeping at 1.5 m/s could be possible with these parameters: 20 deg angle of attack at the root of the fin, 2 Hz flapping frequency, and a 114 deg flapping amplitude. The mean power required is 1.573 W, which is 0.79 J/cycle. Numerical simulation of flexible fins has been carried out (131). Photographs of sunfish pectoral fins swimming in a constant-speed stream in a controlled laboratory environment were digitized to determine the variation in fin topology with time. The flow around the moving boundaries was simulated using Cartesian-grid-based, immersed boundary algorithm pioneered earlier (145) for flows in hearts and lungs (146). The large-eddy simulation method was used to compute the forces produced by the fin. The method of proper orthogonal decomposition was used to determine the modes of the fin topology and determine their contributions to the thrust produced. Mode-1, which visually appears to capture most of the cupping shape of the fin, produces 45% of the total mean thrust, the glaring omission being the peak during the second half of the cycle. The addition of Mode-2 raises the contribution to 63%, and the second peak is partially generated. Although the further addition of Mode-3 generates 92% of the thrust, reproduction of the second peak remains elusive. Videography shows (simplistically, to this reviewer) that there may be at least two distinct kinds of deformations—those that are of the scale of the chord and span, resulting in cupping of the fin, and those that are distinctly smaller and extend over only a part of the fin. It would be worthwhile to examine the nonlinear interaction of these two scales of deformations, particularly in the augmentation of force peaks over a part of the cycle.

Numerical simulation of the flow due to flapping, rigid ellipsoids with varying aspect ratio has been carried out (147). The relevance of freely flapping, rigid ellipsoids to the flapping fins of fish is unclear. The authors show that the gains in thrust and efficiency remain confined to aspect ratios of 2–3, and this is claimed to be the reason why such aspect ratios are commonly found in the pectoral fins among labriform swimmers. The fin wake is found to consist of vortex loops that convect downstream in two oblique directions to the flow, and their intervening angle is inversely proportional to the aspect ratio of the ellipsoid. Numerical simulation of a pair of rigid and finite flapping fins in tandem in the absence of a body has been carried out. As to be expected, certain spatial gaps between the fins can augment thrust and efficiency. However, the relevance of the two-dimensional rigid fin results to the hypothesis on the interaction between the dorsal and caudal fins of sunfish is tenuous (28). The value of the vortex interaction and moment distribution due to fins around a body to the control of the whole animal/vehicle could be more important than thrust augmentation. The biomechanics works of biologists and biology-inspired hydrodynamics are yet to focus on the relationship of hydrodynamic properties and control.

Analysis

Vortex theory rests on the presence of concentrated regions of vorticity in the flow. The earliest vortex theory of insect and bird flights, developed to firmly supplant the momentum jet theory of continuous wake generation, is due to Rayner (40,148). Both hovering and forward flights are considered. In hovering, the wake vortices are a stack of horizontal, coaxial, and circular rings. In forward flight, the rings are elliptical, but neither horizontal nor coaxial. Power reduction motivates the choice of flight style. This is illustrated by a comparison of the mallard and pheasant, which are large birds (>1kg) that are not good in all conditions, such as hovering and fast flights. The mallard has large-aspect-ratio, thin, pointed wings, and the pheasant has low-aspect-ratio, broad, rounded wings. The mallard has lower power per unit mass and lower aerodynamic power at higher speeds. This explains why the mallard patters long before takeoff, while the pheasant can take off vertically if need be. Also, the mallard is one of the fastest flying birds, while the pheasant has a labored flight and rarely flies for long duration. The author gives a good discussion of the theoretical methods for estimating induced power. A theoretical model of how wing kinematics affects induced flow over insect bodies and the far-wake shows that wing beat frequency, stroke amplitude, and wing shape affect induced flow (66). Navier–Stokes computations of a flapping wing at a low Reynolds number of 100 show the spanwise pressure gradient that prevents the LEV from being shed (149). For the accurate determination of locomotive forces from wake traverse, both velocity and pressure field information are required (150).

Computation of Flow Due to Biorobotic Vehicles

Finite volume simulation of the inviscid forced-motion hydrodynamics of the MIT Robotuna vehicle has been carried out (151). The Navier–Stokes equations are expressed in arbitrary Lagrangian–Eulerian form, and a mesh movement algorithm based on a modified form of the Laplace equation is developed to handle moving boundaries. The computed mean power compares with measurements within 10–15%, and the mean thrust compares with the nonlinear potential method (152) within 12%. There is an intriguing phase difference in force and power time histories between the two computations.

Differences Between Rigid and Flexible Fins

Low-aspect-ratio, flexible fins produce LEVs that do not spiral, and the flow is dominated by axial flow and shedding of vortices. Large-aspect-ratio, rigid fins have strong LEVs that spiral spanward, creating vortex stability. We have preferred to demarcate, as above, in terms of flexibility rather than in terms of swimming and flying. Highly flexible, low-aspect-ratio wings do not seem to be used in flying where flapping frequencies need to be very high (×10 to 100) and, apparently, it is difficult to flex simultaneously at such high frequencies. Avian flight analysis suggests that large-aspect-ratio wings are more suitable for high-speed sustained flight, while low-aspect-ratio wings are better suited for hovering.

Wagner Effects

The Wagner effect is one of the unsteady effects that need to be considered in the mechanism of force production in swimming and flying animals. It is known that there is a time delay in the production of forces in impulsively started lifting surfaces. This delay is called the Wagner effect, and it has been experimentally elucidated (153). Due to viscous effects, there is a delay in the development of the asymptotic value of the circulation around the lifting surface, that is, a delay in the establishment of the Kutta condition. The proximity of the starting vortex near the trailing edge in the early stages also affects this delay. The reduction in lift and drag can be estimated using the simple Wagner function, accounting for the distance traveled during stroke reversal (154). Some have suggested that this effect might not be strong in insect flight (50,68), although others think differently (69,96). Force measurements have been carried out in an abstracted penguin wing at chord Reynolds numbers of up to 125,000 at tow speeds up to 1.25 m/s (5). During hovering and at low speeds (→0), a hysteretic effect reminiscent of the Wagner effect has been observed in the wing kinematics and forces measured. Because the accuracy of the estimation of the representative induced speed during hovering is somewhat doubtful, instead of relying only on lift coefficients, torque sensors were also used to determine if the observed hysteresis was genuine. The torque sensor measurements showed that some amount of hysteresis is definitely present, although it is not as large as given by the force coefficient plots. In addition, the hysteresis dropped as Reynolds number increased. A correlation of the motion of the stagnation point and lift forces also shows a phase difference reminiscent of the Wagner effect.

In the insectlike motion of wings, the wing mostly has steady kinematics except near the end, where the flip is rapid (59). A time delay in forces has been observed during rapid wing flips at the end of wing travel, and it has not been examined if this happens when the flip is more gradual, as is the case in underwater experiments (8). Models and numerical simulations do not compute lift and drag forces accurately during the rapid flips that are characteristic of insects, although they are otherwise accurate during the remaining phase of oscillation (59,61). This is an area that needs further investigation. Also, future work is needed on the origin of the time delays found in the kinematics relevant to swimming and flying animals.

Added Mass Effects

When a lifting surface accelerates through a fluid, it experiences a reactive force due to the accelerated fluid. This is known as the added mass effect. It has also been termed “acceleration reaction” (60) and “virtual mass” (41,92), reflecting the authors’ emphasis on the domination of acceleration or virtual mass for force generation. Due to the simultaneous presence of circulatory forces, it may be difficult to calculate forces due to added mass. Added mass components can be estimated using empirically derived coefficients measured for various bodies (155). For fish, added mass coefficients for an entire fish are 0.405 and 0.9255 in the fore-aft and up-down directions, respectively, and 1.0 for the pectoral fin sections (134). An expression for calculating the force due to the inertia of the added mass of the fluid has been given (156). For a three-dimensional wing, it is calculated for each blade element and then is integrated along the span of the wing. In a pair of wings undergoing the “fling” motion, the interference of a pair of plates can increase the added mass of each plate, but only when the opening angle between the plates is small (45). A method is available for estimating forces produced by swimming animals from the PIV measurements of velocity and added mass in the animal wake (157).

Effects of Twisting

High-speed photography of insects in free flight shows that the wing profile twists and flexes (31). The wing is twisted along its span—the angle of attack being higher at the root. A theoretical model has been compared with measurements on a flapping foil that was passively twisting along its span (99). The mechanical efficiency depended on advance ratio and wing twist, the maximum reaching a value of 0.83. This reviewer and co-workers have conducted measurements on twisting penguinlike fins, which show that twist affects efficiency (5%) and thrust (24%).

Flagellar Swimming: EEL Swimming

Here, we consider the swimming of eels and spermatozoa. Their kinematics and relationship to performance are summarized. Eels can swim thousands of kilometers and they have enough fat to undertake such a journey (158). We consider eel swimming particularly because a robotic eel has been built and is an example of one of the earliest examples of robotic fish. The gait and low frequencies are amenable to shape memory alloys. Unlike fish, eels do not have a downstream pointing jet that is a reverse Kármán vortex (159). However, they produce transverse jets. PIV measurements show that the drag and thrust vorticities in eels are not differentiated spatially as clearly as in carangiform fish, and the result is that the thrust jet is not discernable (87). The cost of producing the wake increases with speed to the power of 1.48 and not 2.0. Eel propulsion efficiency is reported to be 0.43–0.97 (160). Because of such wide disagreements, direct measurements of thrust forces produced are required and accurate measurements of efficiency are needed. Numerical simulation of eel swimming has been carried out where the kinematics for efficient swimming is obtained using a “genetic” algorithm to understand the relationship between body movement and forces produced (6). It is unclear how comprehensively the technique has been validated, and claims of differences in flow physics with those observed experimentally are subjects of future studies. For example, an optimized Strouhal number in the range 0.6–0.7 has been reported, whereas it is known to be 0.2–0.4 for swimming and flying animals. However, while the condition of optimization of efficiency has been rigorously prescribed in the numerical simulations, most experiments have reported the Strouhal number of fin oscillation but have made no accurate measurements of efficiency. High efficiency is implicit in the popular Strouhal number—but this is not a rigorously established fact. Therefore, the questions are as follows: What is the efficiency of eel swimming? What is the optimized Strouhal number? Eels have two swim modes of kinematics; one is for efficient but slow swimming, and the other is for fast but inefficient swimming (161-162). In the former, eels, nematoads, lamprey, or spermatozoa—whatever the flagellating animal may be—the animals undulate side to side down the length. In the latter, the front part of the body is kept straight and the thrust is generated in the rest of the body. In both kinds, ring vortices are shed and jets are produced. In any case, the reported work clarifies the vorticity composition of the wake. The lateral jets observed by experimenters (87,159) are shown to be due to ring vortices that are shed by the eel, two per cycle. One could then say that eels generate two lateral Kármán vortex streets and not one, and that they are vectored to the direction of motion. In this sense, their swimming is a variation in fish swimming. The experimenters also show that eel kinematics produces significant secondary flow, and the body undulation appears to interact with that. Producing too many vortices per cycle and draining energy to the secondary flows might seem counterintuitive to efficient (or fast) swimming, as some indeed believe eel swimming to be. The interaction of the undulating body with the secondary flow might seem to be of higher order importance unless there is an exquisite nonlinear fluid and structure interaction. These are intriguing fluid-structure interactions in eel that require further investigation.

Flagellar Propulsion: Spermatozoa Swimming

Like eels, spermatozoa also use flagellar propulsion (6). Swimming sperms have probably the lowest Reynolds number (102) among swimming animals. A typical sperm is 1μm in diameter and 2555μm in length—the head length is 5μm, the remaining part being the flagellum (the tail). The helical flagellum is rotated at about 100 Hz by molecular motors embedded in the cell membrane. Its linear speed is reported to be between 0 and 160μm/s(163). It is estimated to consume 2×1018W of power, which can be obtained from the hydrolysis of a single adenosine triphosphate (ATP) molecule; this is considered to be efficient. ATP is like a “molecular currency” of intracellular energy transfer; it transports chemical energy within cells for metabolism. An exception to high-lift swimming and flying is the swimming of bacteria using the traveling wave of a rotating helical filament. The molecular drive is similar to that of a motor, with clearly identifiable stators and rotors. The stator has torque-generating units, and the rotor is made of ten rings of 45 nm diameter. The torque is generated in steps. The electrochemical gradient of sodium ion causes the stator to move or change shape, thereby imparting a torque to the rotor to which the filament is attached. The gradient could be used to slow down the filament rotational rate. The assembly of the molecular motor and the filament is called the flagellum. This is probably an example of the smallest rotary propulsor in nature.

Flagellar Motion

Typically, bacteria use four helical filaments to swim, rotating their body and the filaments. Depending on the direction of rotation (counterclockwise or clockwise), the filaments either bundle or disperse. Bundling allows propulsion. When the filaments disperse, the bacteria tumble and change direction. Experimental simulation has been carried out on a scale-model of bacterial flagellar bundling (164). In the absence of the body, the bundling phenomenon was found to be purely mechanical—attributable to hydrodynamic interactions, bending and twisting elasticities, and geometry.

Propulsion of Microscopic Swimming Animals

The marine environment is teeming with microscopic animals swimming and feeding, while being constantly in motion. They swim in the transition range between Stokes (Re1) and Oseen (Re1) flows. An ocean-going, submersible, three-dimensional, digital, holographic system has been developed for tracking the motion of such small animals in their similarly scaled, naturally seeded surroundings (30). The animals investigated are copepods of scale 1 mm, nauplii of scale 0.1 mm, and dinoflagellates of scale 1030μm. It is shown that the copepod has two kinds of motion—a periodic 0.5 mm upward jump to a point that is just short of the (lower) stagnation point of the previous recirculation zone, and a slower propulsion between jumps that partially counters the terminal sinking speed, thereby allowing the animal to see the same fluid as it slowly sinks. During the latter stage, the copepod develops a recirculation bubble spanning its extremities. When the recirculation bubble is fully explored or used for feeding, it initiates a jump to an as yet unexplored volume of fluid. The mechanism by which the feeding appendages produce the propulsive jet is not fully understood.

Limitations of Current Biomechanics Studies

The limitations of current biomechanics studies are discussed here from the point of view of engineering implementation. Fin kinematics is related to force production. Because application is system-based, the question is what kinematics can a fin produce under all circumstances from system point of view, and not what we observe it to have in a narrow, controlled environment. Although animal studies may seem to be closer to the biological world than the studies on their robotic appendages, tethered animal flight, for example, could still not be representative of untethered flight. For example, fruit flies clap their wings during tethered flight, but not in untethered flight (17). Apparently, the tethered animal flies in desperation to escape trying to maximize wing roll and lift production. It may be that, counter to researchers’ best intentions, stressed animals have more mechanisms in their portfolios and are, in fact, harder animals to conduct controlled experiments with than their untethered brethren. For example, it is known only from “genetic” algorithm-based numerical simulation that anguilliform animals have two modes of swimming—a leisurely but efficient swimming and a fast but inefficient swimming (6). Most biological studies are limited in their range of flight or swim styles and, therefore, may not be representative of insect flight or aquatic swimming in general (46). So, measurements of animal swimming or flying in a controlled laboratory stream cannot always be generalized.