"Analysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory" - Information and Links:

Analysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory - Info and Reading Options

"Analysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory" was published by National Aeronautics and Space Administration, Scientific and Technical Information Office in 1978 - [Washington], it has 55 pages and the language of the book is English.


“Analysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory” Metadata:

  • Title: ➤  Analysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory
  • Author:
  • Language: English
  • Number of Pages: 55
  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office
  • Publish Date:
  • Publish Location: [Washington]

“Analysis of supersonic stall bending flutter in axial-flow compressor by actuator disk theory” Subjects and Themes:

Edition Specifications:

  • Pagination: 55 p. :

Edition Identifiers:

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