0
TECHNICAL PAPERS

A Review of the History of the National Advisory Committee for Aeronautics Centrifugal Compressor Program and Arrival at Current Computational Design Procedures

[+] Author and Article Information
Joseph T. Hamrick

Aerospace Research Corporation, 5454 Aerospace Road, Roanoke, VA 24014

J. Fluids Eng 127(1), 94-97 (Mar 22, 2005) (4 pages) doi:10.1115/1.1855326 History: Received August 25, 2004; Revised September 07, 2004; Online March 22, 2005
Copyright © 2005 by ASME
Your Session has timed out. Please sign back in to continue.

References

Stodola, A., 1927, Steam and Gas Turbines, Vol. II, McGraw–Hill, New York, pp. 990–997.
Hamrick,  J. T., Ginsburg,  A., and Osborn,  W. M., 1952, “Method of Analysis for Compressible Flow Through Mixed Flow Impellers of Arbitrary Design,” NACA Report 1082, NACA, Washington, D.C.
Anderson,  R. J., Ritter,  W. K., and Dildine,  D. M., 1947, “An Investigation of the Effect of Blade Curvature on Centrifugal Impeller Performance,” NACA TN 1313, NACA, Washington, D.C.
Stanitz,  J. D., 1951, “Approximate Design Method for High-Solidity Blade Elements in Compressors and Turbines,” NACA TN 2408, NACA, Washington, D.C.
Hamrick,  J. T., and Beede,  W. L., 1956, “Some Investigations With Wet Compression,” Trans. ASME, 75, pp. 409–418.
Smith,  K. J., and Hamrick,  Joseph T., 1955, “A Rapid Approximate Method for the Design of the Hub-Shroud Profiles of Centrifugal Impellers of Given Blade Shape,” NACA TN 3399, NACA, Washington, D.C.
Kramer,  J. J., Osborne,  W. M., and Hamrick,  J. T., 1960, “Design and Test of Mixed Flow and Centrifugal Impellers,” J. Eng. Power, 82, pp. 127–135.
Hamrick,  J. T., 1956, “Some Aerodynamic Investigations in Centrifugal Impellers,” Trans. ASME, 78, pp. 591–602.
Moore, J., and Moore, J. G., 1988, “Secondary Flow, Separation, and Losses in the NACA 48-Inch Centrifugal Impeller at Design and Off-Design Conditions,” ASME Paper 88-GT-101.
Moore, J. G., 1985, “An Elliptic Calculation Procedure for 3D Viscous Flow,” 3D Computational Techniques Applied to Internal Flows in Propulsion Systems, Agard Lecture Series No. 140, NATO, Paris.
Moore, J. G., 1985, “Calculation of 3D Flow Without Numerical Mixing,” 3D Computational Techniques Applied to Internal Flows in Propulsion Systems, Agard Lecture Series No. 140, NATO, Paris.
Moore, J., and Moore, J. G., 1990, “A Prediction of 3D Viscous Flow and Performance of the NASA Low-Speed Centrifugal Compressor,” ASME Paper 90-GT-234.
Moore, J., 1985, “3D Computation Techniques Applied to Internal Flow and Propulsion Systems,” 3D Computational Techniques Applied to Internal Flows in Propulsion Systems, Agard Lecture Series No. 140, NATO, Paris.
Meier, R. H., and Schiller, R. N., 1976, “Development and Testing of a New High Flow Centrifugal Pipeline Booster,” Proc. 6th Turbomachinery Symposium, Gas Turbine Laboratories, Texas A&M University, College Station, TX.

Figures

Grahic Jump Location
Velocity distribution and blade shape for the MFI-1 impeller
Grahic Jump Location
The hub and shroud shape for the MFI-1
Grahic Jump Location
Performance map for the MFI-1A
Grahic Jump Location
Hub and shroud velocities for three impellers with modified shrouds
Grahic Jump Location
Performance before and after modification for parabolic bladed impeller

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In