A numerical technique is presented for the calculation of shocked flows in compressor cascades. The problem is posed in the time-dependent form and the asymptotic solution at large times provides the solution of the steady physical problem. The solutions exhibit the formation and movement of shocks as the static pressure ratio across the cascade is varied. The resulting inlet and outlet angles and total pressure loss are also shown.
- International Gas Turbine Institute
Computation of Shocked Flows in Compressor Cascades
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Gopalakrishnan, S, & Bozzola, R. "Computation of Shocked Flows in Compressor Cascades." Proceedings of the ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show. ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show. San Francisco, California, USA. March 26–30, 1972. V001T01A030. ASME. https://doi.org/10.1115/72-GT-31
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