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Unsteady Euler cascade analysisThe 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).
Document ID
19890041035
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Liu, Jong-Shang
(NASA Lewis Research Center Cleveland, OH; Textron Lycoming, Stratford, CT, United States)
Sockol, Peter M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 89-0322
Accession Number
89A28406
Distribution Limits
Public
Copyright
Other

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