Analysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory
By: John J. Adamczyk, Lewis Research Center
Contributors: Lewis Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: NASA technical paper ; 1345
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1978
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 55
Subjects: Flutter (Aerodynamics); Ultrasonic waves -- Speed; Disks, Rotating
Notes: Nov. 1978

Includes bibliographical references