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Issues

Volume 121, Issue 3
July 1999
Issue Cover
ISSN 0889-504X
EISSN 1528-8900
In this Issue

Research Papers

Effect of Upstream Rotor Vortical Disturbances on the Time-Averaged Performance of Axial Compressor Stators: Part 1—Framework of Technical Approach and Wake–Stator Blade Interactions
T. V. Valkov, C. S. Tan
J. Turbomach. July 1999, 121(3): 377–386. doi: https://doi.org/10.1115/1.2841330
View articletitled, Effect of Upstream Rotor Vortical Disturbances on the Time-Averaged Performance of Axial Compressor Stators: Part 1—Framework of Technical Approach and Wake–Stator Blade Interactions
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Topics: Blades , Compressors , Rotors , Stators , Wakes , Wake turbulence , Flow (Dynamics) , Vortices , Leakage , Approximation
Effect of Upstream Rotor Vortical Disturbances on the Time-Averaged Performance of Axial Compressor Stators: Part 2—Rotor Tip Vortex/Streamwise Vortex–Stator Blade Interactions
T. V. Valkov, C. S. Tan
J. Turbomach. July 1999, 121(3): 387–397. doi: https://doi.org/10.1115/1.2841331
View articletitled, Effect of Upstream Rotor Vortical Disturbances on the Time-Averaged Performance of Axial Compressor Stators: Part 2—Rotor Tip Vortex/Streamwise Vortex–Stator Blade Interactions
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Topics: Blades , Compressors , Rotors , Stators , Vortices , Wake turbulence , Wakes , Flow (Dynamics) , Leakage , Approximation
Periodic Transition on an Axial Compressor Stator: Incidence and Clocking Effects: Part I—Experimental Data
G. J. Walker, J. D. Hughes, W. J. Solomon
J. Turbomach. July 1999, 121(3): 398–407. doi: https://doi.org/10.1115/1.2841332
View articletitled, Periodic Transition on an Axial Compressor Stator: Incidence and Clocking Effects: Part I—Experimental Data
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Topics: Compressors , Stators , Pressure , Flow (Dynamics) , Suction , Turbulence , Wakes , Blades , Bubbles , Inlet guide vanes
Periodic Transition on an Axial Compressor Stator: Incidence and Clocking Effects: Part II—Transition Onset Predictions
W. J. Solomon, G. J. Walker, J. D. Hughes
J. Turbomach. July 1999, 121(3): 408–415. doi: https://doi.org/10.1115/1.2841333
View articletitled, Periodic Transition on an Axial Compressor Stator: Incidence and Clocking Effects: Part II—Transition Onset Predictions
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Topics: Compressors , Stators , Boundary layers , Turbulence , Airfoils , Blades , Computation , Flow (Dynamics) , Pressure , Separation (Technology)
Design and Testing of Swept and Leaned Outlet Guide Vanes to Reduce Stator–Strut–Splitter Aerodynamic Flow Interactions
A. R. Wadia, P. N. Szucs, K. L. Gundy-Burlet
J. Turbomach. July 1999, 121(3): 416–427. doi: https://doi.org/10.1115/1.2841334
View articletitled, Design and Testing of Swept and Leaned Outlet Guide Vanes to Reduce Stator–Strut–Splitter Aerodynamic Flow Interactions
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Topics: Aerodynamic flow , Design , Guide vanes , Stators , Struts (Engineering) , Testing , Flow (Dynamics) , Engines , Pressure , Stability
Simulation of Vortex Shedding in a Turbine Stage
D. L. Sondak, D. J. Dorney
J. Turbomach. July 1999, 121(3): 428–435. doi: https://doi.org/10.1115/1.2841335
View articletitled, Simulation of Vortex Shedding in a Turbine Stage
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Topics: Simulation , Turbines , Vortex shedding , Blades , Frequency response , Pressure , Wakes , Cascades (Fluid dynamics) , Flow simulation , Shock waves
Unsteady Heat Transfer in Stator–Rotor Interaction by Two-Equation Turbulence Model
V. Michelassi, F. Martelli, R. De´nos, T. Arts, C. H. Sieverding
J. Turbomach. July 1999, 121(3): 436–447. doi: https://doi.org/10.1115/1.2841336
View articletitled, Unsteady Heat Transfer in Stator–Rotor Interaction by Two-Equation Turbulence Model
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Topics: Heat transfer , Rotors , Stators , Turbulence , Pressure , Blades , Coolants , Turbines , Computer simulation , Dimensions
Effect of Unsteady Wake With Trailing Edge Coolant Ejection on Film Cooling Performance for a Gas Turbine Blade
H. Du, S. V. Ekkad, J.-C. Han
J. Turbomach. July 1999, 121(3): 448–455. doi: https://doi.org/10.1115/1.2841337
View articletitled, Effect of Unsteady Wake With Trailing Edge Coolant Ejection on Film Cooling Performance for a Gas Turbine Blade
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Topics: Blades , Coolants , Film cooling , Gas turbines , Wakes , Heat transfer coefficients , Generators , Boundary layers , Cascades (Fluid dynamics) , Heat transfer
Numerical Simulation of the Shock-Tip Leakage Vortex Interaction in a HPC Front Stage
M. Hoeger, G. Fritsch, D. Bauer
J. Turbomach. July 1999, 121(3): 456–468. doi: https://doi.org/10.1115/1.2841338
View articletitled, Numerical Simulation of the Shock-Tip Leakage Vortex Interaction in a HPC Front Stage
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Topics: Computer simulation , Leakage , Shock (Mechanics) , Vortices , Simulation , Flow (Dynamics) , Blades , Compressors , Displacement , Instrumentation
The Role of Tip Leakage Vortex Breakdown in Compressor Rotor Aerodynamics
M. Furukawa, M. Inoue, K. Saiki, K. Yamada
J. Turbomach. July 1999, 121(3): 469–480. doi: https://doi.org/10.1115/1.2841339
View articletitled, The Role of Tip Leakage Vortex Breakdown in Compressor Rotor Aerodynamics
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Topics: Aerodynamics , Compressors , Leakage , Rotors , Vortices , Pressure , Blades , Flow (Dynamics) , Simulation , Suction
Dual-Laser Probe Measurement of Blade-Tip Clearance
H. S. Dhadwal, A. P. Kurkov
J. Turbomach. July 1999, 121(3): 481–485. doi: https://doi.org/10.1115/1.2841340
View articletitled, Dual-Laser Probe Measurement of Blade-Tip Clearance
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Topics: Blades , Clearances (Engineering) , Lasers , Probes , Rotors , Fibers , Flow (Dynamics) , Laser beams , Linings (Textiles) , Particle spin
The Influence of Shrouded Stator Cavity Flows on Multistage Compressor Performance
S. R. Wellborn, T. H. Okiishi
J. Turbomach. July 1999, 121(3): 486–497. doi: https://doi.org/10.1115/1.2841341
View articletitled, The Influence of Shrouded Stator Cavity Flows on Multistage Compressor Performance
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Topics: Cavity flows , Compressors , Stators , Leakage , Cavities , Fluids , Pressure , Rotors , Clearances (Engineering) , Flow (Dynamics)
Endwall Blockage in Axial Compressors
S. A. Khalid, A. S. Khalsa, I. A. Waitz, C. S. Tan, E. M. Greitzer, N. A. Cumpsty, J. J. Adamczyk, F. E. Marble
J. Turbomach. July 1999, 121(3): 499–509. doi: https://doi.org/10.1115/1.2841344
View articletitled, Endwall Blockage in Axial Compressors
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Topics: Compressors , Clearances (Engineering) , Flow (Dynamics) , Design , Blades , Boundary layers , Computer simulation , Pressure , Wind tunnels
Rotating Stall Control in a High-Speed Stage With Inlet Distortion: Part I—Radial Distortion
Z. S. Spakovszky, H. J. Weigl, J. D. Paduano, C. M. van Schalkwyk, K. L. Suder, M. M. Bright
J. Turbomach. July 1999, 121(3): 510–516. doi: https://doi.org/10.1115/1.2841345
View articletitled, Rotating Stall Control in a High-Speed Stage With Inlet Distortion: Part I—Radial Distortion
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Topics: Axial flow , Compressors , Control equipment , Dynamics (Mechanics) , Ejectors , Feedback , Flow (Dynamics) , NASA , Rotors , Testing
Rotating Stall Control in a High-Speed Stage With Inlet Distortion: Part II—Circumferential Distortion
Z. S. Spakovszky, C. M. van Schalkwyk, H. J. Weigl, J. D. Paduano, K. L. Suder, M. M. Bright
J. Turbomach. July 1999, 121(3): 517–524. doi: https://doi.org/10.1115/1.2841346
View articletitled, Rotating Stall Control in a High-Speed Stage With Inlet Distortion: Part II—Circumferential Distortion
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Topics: Axial flow , Compressors , Control equipment , Ejectors , Engineering design processes , Feedback , Flow (Dynamics) , NASA , Pressure , Testing
External Heat Transfer Predictions in a Highly Loaded Transonic Linear Turbine Guide Vane Cascade Using an Upwind Biased Navier–Stokes Solver
A. Gehrer, H. Jericha
J. Turbomach. July 1999, 121(3): 525–531. doi: https://doi.org/10.1115/1.2841347
View articletitled, External Heat Transfer Predictions in a Highly Loaded Transonic Linear Turbine Guide Vane Cascade Using an Upwind Biased Navier–Stokes Solver
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Topics: Cascades (Fluid dynamics) , Guide vanes , Heat transfer , Turbines , Turbulence , Algebra , Boundary-value problems , Finite volume methods , Modeling , Nozzle guide vanes
Physics of Hot Crossflow Ingestion in Film Cooling
E. L. McGrath, J. H. Leylek
J. Turbomach. July 1999, 121(3): 532–541. doi: https://doi.org/10.1115/1.2841348
View articletitled, Physics of Hot Crossflow Ingestion in Film Cooling
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Topics: Film cooling , Physics , Flow (Dynamics) , Coolants , Gas turbines , Computational fluid dynamics , Density , Geometry , Modeling , Reynolds number
Effects of Bulk Flow Pulsations on Film Cooling From Different Length Injection Holes at Different Blowing Ratios
H. J. Seo, J. S. Lee, P. M. Ligrani
J. Turbomach. July 1999, 121(3): 542–550. doi: https://doi.org/10.1115/1.2841349
View articletitled, Effects of Bulk Flow Pulsations on Film Cooling From Different Length Injection Holes at Different Blowing Ratios
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Topics: Film cooling , Flow (Dynamics) , Temperature distribution , Coolants , Gas turbines , Pressure , Shock waves , Turbines
Turbulence Spectra and Length Scales Measured in Film Coolant Flows Emerging From Discrete Holes
S. W. Burd, T. W. Simon
J. Turbomach. July 1999, 121(3): 551–557. doi: https://doi.org/10.1115/1.2841350
View articletitled, Turbulence Spectra and Length Scales Measured in Film Coolant Flows Emerging From Discrete Holes
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Topics: Coolants , Flow (Dynamics) , Spectra (Spectroscopy) , Turbulence , Film cooling , Computation , Computational fluid dynamics , Modeling , Sensors , Wire
Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall
M. B. Kang, A. Kohli, K. A. Thole
J. Turbomach. July 1999, 121(3): 558–568. doi: https://doi.org/10.1115/1.2841351
View articletitled, Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall
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Topics: Heat transfer , Stators , Reynolds number , Pressure , Flow (Dynamics) , Turbulence , Vortices , Kinetic energy , Lasers , Separation (Technology)
Fluid Flow in a 180 deg Sharp Turning Duct With Different Divider Thicknesses
Tong-Miin Liou, Yaw-Yng Tzeng, Chung-Chu Chen
J. Turbomach. July 1999, 121(3): 569–576. doi: https://doi.org/10.1115/1.2841354
View articletitled, Fluid Flow in a 180 deg Sharp Turning Duct With Different Divider Thicknesses
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Topics: Ducts , Fluid dynamics , Turning , Turbulence , Cooling , Corners (Structural elements) , Flow (Dynamics) , Heat transfer , Heat transfer coefficients , Kinetic energy
Dynamics of Large-Scale Structures for Jets in a Crossflow
F. Muldoon, S. Acharya
J. Turbomach. July 1999, 121(3): 577–587. doi: https://doi.org/10.1115/1.2841355
View articletitled, Dynamics of Large-Scale Structures for Jets in a Crossflow
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Topics: Dynamics (Mechanics) , Jets , Vortices , Shear (Mechanics) , Compressibility , Computation , Computer software , Velocity measurement , Wake turbulence , Wakes
A Theory for Predicting the Turbulent-Spot Production Rate
R. E. Mayle
J. Turbomach. July 1999, 121(3): 588–593. doi: https://doi.org/10.1115/1.2841356
View articletitled, A Theory for Predicting the Turbulent-Spot Production Rate
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Topics: Turbulence , Boundary layers , Flow (Dynamics) , Pressure gradient
A Prediction Model for Separated-Flow Transition
A. Hatman, T. Wang
J. Turbomach. July 1999, 121(3): 594–602. doi: https://doi.org/10.1115/1.2841357
View articletitled, A Prediction Model for Separated-Flow Transition
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Topics: Flow (Dynamics) , Separation (Technology) , Bubbles , Airfoils , Turbulence , Reynolds number , Accounting , Boundary layers , Displacement , Flat plates
Numerical Simulation of Impeller–Volute Interaction in Centrifugal Compressors
K. Hillewaert, R. A. Van den Braembussche
J. Turbomach. July 1999, 121(3): 603–608. doi: https://doi.org/10.1115/1.2841358
View articletitled, Numerical Simulation of Impeller–Volute Interaction in Centrifugal Compressors
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Topics: Compressors , Computer simulation , Impellers , Flow (Dynamics) , Boundary-value problems , Design , Pressure , Temperature , Unsteady flow
Comparison of Measurement Data at the Impeller Exit of a Centrifugal Compressor Measured With Both Pneumatic and Fast-Response Probes
C. Roduner, P. Ko¨ppel, P. Kupferschmied, G. Gyarmathy
J. Turbomach. July 1999, 121(3): 609–618. doi: https://doi.org/10.1115/1.2841359
View articletitled, Comparison of Measurement Data at the Impeller Exit of a Centrifugal Compressor Measured With Both Pneumatic and Fast-Response Probes
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Topics: Compressors , Impellers , Probes , Flow (Dynamics) , Geometry , Temperature , Turbines
Improved Model for the Design and Analysis of Centrifugal Compressor Volutes
R. A. Van den Braembussche, E. Ayder, D. Hagelstein, M. Rautenberg, R. Keiper
J. Turbomach. July 1999, 121(3): 619–625. doi: https://doi.org/10.1115/1.2841360
View articletitled, Improved Model for the Design and Analysis of Centrifugal Compressor Volutes
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Topics: Compressors , Design , Pressure , Flow (Dynamics) , Diffusers , Impellers , Flow measurement
The Effect of Inlet Boundary Layer Thickness on the Flow Within an Annular S-Shaped Duct
T. Sonoda, T. Arima, M. Oana
J. Turbomach. July 1999, 121(3): 626–634. doi: https://doi.org/10.1115/1.2841361
View articletitled, The Effect of Inlet Boundary Layer Thickness on the Flow Within an Annular S-Shaped Duct
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Topics: Boundary layers , Ducts , Flow (Dynamics) , Compressors , Pressure , Geometry , Struts (Engineering) , Vortices , Design , Engines

Discussions

Discussion: “The Influence of Shrouded Stator Cavity Flows on Multistage Compressor Performance” (Wellborn, S. R., and Okiishi, T. H., 1999, ASME J. Turbomach., 121, pp. 486–497)
Ruixian Cai
J. Turbomach. July 1999, 121(3): 497. doi: https://doi.org/10.1115/1.2841342
View articletitled, Discussion: “The Influence of Shrouded Stator Cavity Flows on Multistage Compressor Performance” (Wellborn, S. R., and Okiishi, T. H., 1999, ASME J. Turbomach., 121, pp. 486–497)
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Topics: Cavity flows , Compressors , Stators
Closure to “Discussion of ‘The Influence of Shrouded Stator Cavity Flows on Multistage Compressor Performance’” (1999, ASME J. Turbomach., 121, p. 497)
S. R. Wellborn, T. H. Okiishi
J. Turbomach. July 1999, 121(3): 498. doi: https://doi.org/10.1115/1.2841343
View articletitled, Closure to “Discussion of ‘The Influence of Shrouded Stator Cavity Flows on Multistage Compressor Performance’” (1999, ASME J. Turbomach., 121, p. 497)
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Topics: Cavity flows , Compressors , Stators
Discussion: “Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall” (Kang, M. B., Kohli, A., and Thole, K. A., 1999, ASME J. Turbomach., 121, pp. 558–568)
L. S. Langston
J. Turbomach. July 1999, 121(3): 568. doi: https://doi.org/10.1115/1.2841352
View articletitled, Discussion: “Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall” (Kang, M. B., Kohli, A., and Thole, K. A., 1999, ASME J. Turbomach., 121, pp. 558–568)
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Topics: Heat transfer , Stators
Closure to “Discussion of ‘Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall’” (1999, ASME J. Turbomach., 121, p. 568)
M. B. Kang, A. Kohli, K. A. Thole
J. Turbomach. July 1999, 121(3): 568. doi: https://doi.org/10.1115/1.2841353
View articletitled, Closure to “Discussion of ‘Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall’” (1999, ASME J. Turbomach., 121, p. 568)
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Topics: Heat transfer , Stators
All Issues
NUMERICAL ASSESSMENT OF AN AERODYNAMIC PROBE TO ENABLE SHORT FOCAL LENGTH LASER DIAGNOSTICS IN HIGH TEMPERATURE SUPERSONIC FLOWS BASED ON FLOW DISTURBANCE
J. Turbomach
Development of heat exchanger modelling capability for a finite volume aeroelasticity solver
J. Turbomach
MULTI-AEROELASTIC PHENOMENA MODELLING PART I: THE DEVELOPMENT OF WHOLE LPC MODEL FOR CIVIL TURBOFAN ENGINE
J. Turbomach
EFFECTS OF LOCALIZED NON-GAUSSIAN ROUGHNESS ON HIGH PRESSURE TURBINE AERO-THERMAL PERFORMANCE: CONVECTIVE HEAT TRANSFER, SKIN-FRICTION AND THE REYNOLDS' ANALOGY
J. Turbomach
Heat Transfer and Flow Field Characteristics of Variable Aspect Ratio, Serpentine Passages
J. Turbomach
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