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A Model of Compressor Blade Row Interaction with Shock Induced Vortex Shedding

Author(s):
  • M. Turner ( University of Cincinnati, Cincinnati, OH )
  • S. Gorrell ( U.S. Air Force Research Laboratory, Wright-Patterson AFB, OH )
  • D. Car
Publication title:
AIAA meeting papers on disc
Title of ser.:
AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:
2006
Pub. Year:
2006
No.:
2006-4459
Paper no.:
AIAA Paper 2006-4459
Pub. info.:
Reston, Va: American Institute of Aeronautics and Astronautics
ISSN:
10877215
Language:
English
Call no.:
A07400/200616 [CD-ROM 2006 Disc 16]
Type:
Technical Paper

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