Wind-Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics. 3 - Symmetrically Tapered Wing at Various Positions on Circular Fuselage with and without a Vertical Tail

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1941
Accession Number
ADB806009

Entities

People

  • Arthur R. Wallace
  • Isidore G. Recant

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Aircrafts
  • Aspect Ratio
  • Center Of Gravity
  • Coefficients
  • Directional
  • Dynamic Pressure
  • Flow Separation
  • Free Stream
  • Fuselages
  • Gravity
  • High Angles
  • Intact Stability
  • Reynolds Number
  • Split Flaps
  • Wind Tunnels