A Low Speed Wind Tunnel Investigation of Reynolds Number Effects on a 60-Deg Swept Wing Configuration with Leading and Trailing Edge Flaps

by National Aeronautics and Space Adm Nasa

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  • ISBN10 1729462715
  • ISBN13 9781729462713
  • Publish Date 2 November 2018
  • Publish Status Temporarily Withdrawn
  • Imprint Independently Published
  • Format Paperback (US Trade)
  • Pages 70
  • Language English