Theoretical Evaluation of Engine Auxiliary Inlet Design for Supersonic V/Stol Aircraft

by National Aeronautics and Space Adm Nasa

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  • ISBN10 1730998151
  • ISBN13 9781730998157
  • Publish Date 8 November 2018
  • Publish Status Temporarily Withdrawn
  • Imprint Independently Published
  • Format Paperback (US Trade)
  • Pages 100
  • Language English