Theoretical Calculations of the Lateral Force and Yawing Moment Due to Rolling at Supersonic Speeds for Sweptback Tapered Wings with Streamwise Tips. Supersonic Leading Edges

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1950
Accession Number
ADA380589

Entities

People

  • John C. Martin
  • Sidney M. Harmon

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Aspect Ratio
  • Cartesian Coordinates
  • Center Of Gravity
  • Conversion
  • Equations
  • Flow
  • Incompressible Flow
  • Leading Edges
  • Mach Number
  • Skin Friction
  • Thin Wings
  • Trailing Edges
  • Wing Tips

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow