Unsteady transonic flows in an axial flow compressor
Author:
A. R. Manwell
Journal:
Quart. Appl. Math. 43 (1985), 369-383
MSC:
Primary 76H05
DOI:
https://doi.org/10.1090/qam/814234
MathSciNet review:
814234
Full-text PDF Free Access
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Additional Information
- E. T. Copson, Partial differential equations, Cambridge University Press, Cambridge-New York-Melbourne, 1975. MR 0393746
- R. Courant and K. O. Friedrichs, Supersonic Flow and Shock Waves, Interscience Publishers, Inc., New York, N. Y., 1948. MR 0029615
- R. Courant and D. Hilbert, Methods of mathematical physics. Vol. I, Interscience Publishers, Inc., New York, N.Y., 1953. MR 0065391
Ferri, A., Esperienze su di un biplano iperacustica tipo Busemann, Atti di Guidonia No. 37–38, 1940
Ferri, A., Aerodynamic properties of supersonic compressors, High Speed Aerodynamics and Jet Propulsion, Vol. X (Edit. W. R. Hawthorne) Princeton, 1964
Goldstein, M. E., Cascade with subsonic leading-edge locus, AIAA Journ. 13 1117 (1975)
Goldstein, M. E., Braun, W. and Adamczyk, J. J., Unsteady flow in a supersonic cascade with strong in-passage shocks. J. Fluid Mech. 83, 569 (1977)
Hutton, M. F., Supersonic inflow onto turbine blading: the unique incidence theorem, Gen. Elect. Gen Board Res. Rept. R/M/M 159, 1974
Kantrowitz, A., The supersonic axial-flow compressor, N.A.C.A. Tech. Rep. no. 974, 1950
Kurosaka, M., On the unsteady supersonic cascade with a subsonic leading edge- an exact first order theory-Part I. Trans. ASME, A,96 13(1974)
Lamb, R., Hydrodynamics (6th ed.)Cambridge, 1952
Levine, P., Two-dimensional inflow conditions for a supersonic compressor with curved blades. J. Appl. Mech. 24, 165 (1957)
Lichtfuss, H-J and Starken, H., Supersonic cascade flow, Progress in Aerospace Sciences 15, Edit. D. Kuchemann, Pergamon, 1974
Mani, R. and Horvay, G., Sound transmission through blade rows, J. Sound Vib. 12, 59 (1970)
- A. R. Manwell, A uniqueness theorem for the moving medium reduced wave equation, Applicable Anal. 12 (1981), no. 3, 215–228. MR 638233, DOI https://doi.org/10.1080/00036818108839361
Manwell, A. R., Supersonic cascade flows with subsonic axial Mach number, Univ. Camb. Eng. Dept. Rep. CUED/A-Turbo/TR110, 1982
Miles, J. W., The potential theory of unsteady supersonic flow, Cambridge
Morfey, C. L. and Fisher, M. J., Shock wave radiation from a supersonic ducted rotor, Aer. Journ. 74, 579 (1970)
Nagashima, T and Whitehead, D. S., Linearized supersonic unsteady flow in cascades, Aer. Res. Coun. R & M No. 3811, 1977
Picard, É, Leçons sur quelque équations aux dérivée partielles, Paris, Gauthier-Villars, 1927
Picard, É, Leçons sur quelque équations fonctionelles, Paris, Gauthier-Villars, 1928
Stratford, B. S. and Sansome, G. E., The performance of supersonic turbine muzzles, Aer. Res. Coun. R & M No. 3273, 1959
Verdon, J. M. and McCune, J. E., Unsteady supersonic cascade in subsonic axial flow, AIAA Journ. 13, 193 (1975)
Copson, E. T., Partial differential equations, Cambridge, 1975
Courant, R. and Friedrichs, K. O., Supersonic flow and shock waves, 1948 Interscience
Courant, R and Hilbert, D., Methods of mathematical physics, Vol. II, Interscience, 1962
Ferri, A., Esperienze su di un biplano iperacustica tipo Busemann, Atti di Guidonia No. 37–38, 1940
Ferri, A., Aerodynamic properties of supersonic compressors, High Speed Aerodynamics and Jet Propulsion, Vol. X (Edit. W. R. Hawthorne) Princeton, 1964
Goldstein, M. E., Cascade with subsonic leading-edge locus, AIAA Journ. 13 1117 (1975)
Goldstein, M. E., Braun, W. and Adamczyk, J. J., Unsteady flow in a supersonic cascade with strong in-passage shocks. J. Fluid Mech. 83, 569 (1977)
Hutton, M. F., Supersonic inflow onto turbine blading: the unique incidence theorem, Gen. Elect. Gen Board Res. Rept. R/M/M 159, 1974
Kantrowitz, A., The supersonic axial-flow compressor, N.A.C.A. Tech. Rep. no. 974, 1950
Kurosaka, M., On the unsteady supersonic cascade with a subsonic leading edge- an exact first order theory-Part I. Trans. ASME, A,96 13(1974)
Lamb, R., Hydrodynamics (6th ed.)Cambridge, 1952
Levine, P., Two-dimensional inflow conditions for a supersonic compressor with curved blades. J. Appl. Mech. 24, 165 (1957)
Lichtfuss, H-J and Starken, H., Supersonic cascade flow, Progress in Aerospace Sciences 15, Edit. D. Kuchemann, Pergamon, 1974
Mani, R. and Horvay, G., Sound transmission through blade rows, J. Sound Vib. 12, 59 (1970)
Manwell, A. R., A uniqueness theorem for the moving medium reduced wave equation. Appl. Anal. 12, 215 (1981)
Manwell, A. R., Supersonic cascade flows with subsonic axial Mach number, Univ. Camb. Eng. Dept. Rep. CUED/A-Turbo/TR110, 1982
Miles, J. W., The potential theory of unsteady supersonic flow, Cambridge
Morfey, C. L. and Fisher, M. J., Shock wave radiation from a supersonic ducted rotor, Aer. Journ. 74, 579 (1970)
Nagashima, T and Whitehead, D. S., Linearized supersonic unsteady flow in cascades, Aer. Res. Coun. R & M No. 3811, 1977
Picard, É, Leçons sur quelque équations aux dérivée partielles, Paris, Gauthier-Villars, 1927
Picard, É, Leçons sur quelque équations fonctionelles, Paris, Gauthier-Villars, 1928
Stratford, B. S. and Sansome, G. E., The performance of supersonic turbine muzzles, Aer. Res. Coun. R & M No. 3273, 1959
Verdon, J. M. and McCune, J. E., Unsteady supersonic cascade in subsonic axial flow, AIAA Journ. 13, 193 (1975)
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Article copyright:
© Copyright 1985
American Mathematical Society
