The results of an investigation of the rotor-stator interaction phenomena in turbomachines are presented. Numerical study was carried out by solving the unsteady Euler equations in the blade-to-blade direction for a variety of cascade geometries. The problem of uneven rotor and stator blades is addressed by adopting the tilted time domain technique. Computed solutions are presented and discussed for a NACA 0012 type cascade and the first stage fuel turbopump of the Space Shuttle Main Engine (SSME).
Unsteady Euler cascade analysis
Analyse von instationaeren Euler-Kaskaden
AIAA-Papers ; Jan ; 1-7
1989
7 Seiten, 11 Bilder, 10 Quellen
Conference paper
English
Unsteady Euler cascade analysis
AIAA | 1989
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