Experimental determination of the Yawing Moment due to Yawing Contributed by the Wing, Fuselage, and Vertical Tail of a Midwing Airplane Model

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1943
Accession Number
ADA801265

Entities

People

  • John P. Campbell
  • Ward O. Mathews

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aircrafts
  • Airplanes
  • Airspeed
  • Aspect Ratio
  • Center Of Gravity
  • Coefficients
  • Drag
  • Dynamic Pressure
  • Equations
  • Flight
  • Fluid Dynamics
  • Friction
  • Fuselages
  • High Lift
  • Measurement
  • Oscillation