Wind-Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics. 5 - Symmetrically Tapered Wing with a Circular Fuselage Having a Horizontal and a Vertical Tail

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1943
Accession Number
ADA800949

Entities

People

  • Arthur R. Wallace
  • Thomas R. Turner

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aeronautical Laboratories
  • Aircrafts
  • Airfoils
  • Airframes
  • Aspect Ratio
  • Coefficients
  • Dynamic Pressure
  • Fluid Dynamics
  • Free Stream
  • Fuselages
  • High Angles
  • Horizontal Stabilizers
  • Reynolds Number
  • Stabilization Systems
  • Surfaces
  • Wind Tunnels