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The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges.


AD037709

Publication Date 1954
Personal Author EPSTEIN, M.
Page Count 45
Abstract No abstract available.
Keywords
  • Flutter
  • Wings
  • Fuselages
  • Load distribution
  • Supersonic flow
Source Agency
  • Non Paid Delimited ADS
  • Invalid Source Agency Code
Corporate Authors Aeronautical Systems Div Wright-Patterson AFB Ohio Flight Control Lab
Document Type Technical Report
NTIS Issue Number 198104
The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges.
The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges.
AD037709

  • Flutter
  • Wings
  • Fuselages
  • Load distribution
  • Supersonic flow
  • Non Paid Delimited ADS
  • Invalid Source Agency Code
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