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RISTransonic Cascade Flow Solved by Separate Supersonic and Subsonic Computations With Shock Fitting
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A new method to solve the transonic flow past a plane cascade with inlet bow wave and a passage shock extending from the leading edge all the way across the flow channel is presented. In ...
Closure to “Discussion of ‘Transonic Cascade Flow Solved by Separate Supersonic and Subsonic Computations With Stock Fitting’” (1985, ASME J. Eng. Gas Turbines Power, 107, pp. 335–336)
Publisher: The American Society of Mechanical Engineers (ASME)