Assessment of a Flow-Through Balance for Hypersonic Wind Tunnel Models with Scramjet Exhaust Flow Simulation

by National Aeronautics and Space Adm Nasa

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  • ISBN10 1729311237
  • ISBN13 9781729311233
  • Publish Date 27 October 2018
  • Publish Status Temporarily Withdrawn
  • Imprint Independently Published
  • Format Paperback (US Trade)
  • Pages 56
  • Language English