Experimental Influence Coefficients for the Deflection of the Wing of a Full-Scale, Swept-Wing Bomber

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Document Details

Document Type
Technical Report
Publication Date
Apr 22, 1954
Accession Number
AD0029785

Entities

People

  • Alton P. Mayo
  • John F. Ward

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Aeronautical Laboratories
  • Aircrafts
  • Airframes
  • Airplanes
  • Center Of Gravity
  • Coefficients
  • Deflection
  • Government Procurement
  • Governments
  • Law
  • Load Distribution
  • Measurement
  • National Security
  • Outboard
  • Spars
  • Swept Wings