The inadequacy of axisymmetric theory in modeling the structure of the shock system in a transonic compressor rotor is shown with a simple model. A more accurate model for the flow near the sonic radius is proposed, which is supported by some flow visualization data and three-dimensional computations.
Shock structure in transonic compressor rotors
AIAA Journal ; 17
1979-04-01
Sonstige
Keine Angabe
Englisch
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