A comparison of predicted and measured inlet distortion flows in a subsonic axial inlet flow compressor rotor

by National Aeronautics and Space Adm Nasa

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  • ISBN10 1790377749
  • ISBN13 9781790377749
  • Publish Date 9 April 2020
  • Publish Status Temporarily Withdrawn
  • Imprint Independently Published
  • Format Paperback (US Trade)
  • Pages 200
  • Language English