Effect of Wing Loading and Altitude on Lateral Stability and Control Characteristics of an Airplane as Determined by Tests of a Model in the Free-Flight Tunnel

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1943
Accession Number
ADA801113

Entities

People

  • Charles L. Seacord Jr.
  • John P. Campbell

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aircrafts
  • Airplanes
  • Airspeed
  • Altitude
  • Boundaries
  • Coefficients
  • Dihedral Angle
  • Directional
  • Dynamic Pressure
  • Fixed Wing Aircraft
  • Flight
  • Free Flight
  • Level Flight
  • Moment Of Inertia
  • Sea Level
  • Split Flaps