Stability and Control Characteristics of a Fighter Airplane in Inverted Flight Attitude as Determined by Model Tests

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1945
Accession Number
ADA801211

Entities

People

  • Charles V. Bennett
  • John W. Paulson

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Aircrafts
  • Airplanes
  • Center Of Gravity
  • Coefficients
  • Deflection
  • Directional
  • Dynamic Pressure
  • Fighter Aircraft
  • Flight
  • Free Flight
  • Leading Edges
  • Model Tests
  • Propeller Blades
  • Propellers
  • Wind Tunnels