Stability and Control Characteristics of a Complete Airplane Model Having a Wing with Quarter-Chord Line Swept Back 40 deg, Aspect Ratio 2.50, and Taper Ratio 0.42

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1951
Accession Number
ADA800919

Entities

People

  • Kenneth W. Goodson
  • Marvin Schuldenfrei
  • Paul Comisarow

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aircrafts
  • Aspect Ratio
  • Boundary Layer
  • Center Of Gravity
  • Control Surfaces
  • Dihedral Angle
  • Dynamic Pressure
  • Fuselages
  • Horizontal Stabilizers
  • Landing Gear
  • Models
  • Pressure Distribution
  • Stabilization Systems
  • Sweptback Wings
  • Wind Tunnels