Shock Position Control for Mode Transition in a Turbine Based Combined Cycle Engine Inlet Model

by National Aeronautics and Space Adm Nasa

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  • ISBN10 1793962405
  • ISBN13 9781793962409
  • Publish Date 13 January 2019
  • Publish Status Temporarily Withdrawn
  • Imprint Independently Published
  • Format Paperback (US Trade)
  • Pages 26
  • Language English