Analysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory /

Analysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory /

Bibliographic Details
Main Author: Adamczyk, John J.
Corporate Authors: Lewis Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Format: Government Document Book
Language:English
Published: [Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; 1978.
Series:NASA technical paper ; 1345.
Subjects:
Flutter (Aerodynamics)
Ultrasonic waves > Speed.
Disks, Rotating.

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Call Number: NAS 1.60:1345
 
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NAS 1.60:1345 Available