Span Load Distributions Resulting From Angle of Attack, Rolling, and Pitching for Tapered Sweptback Wings With Streamwise Tips. Supersonic Leading and Trailing Edges

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1952
Accession Number
ADA380384

Entities

People

  • Isabella Jeffreys
  • John C. Martin

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aeronautical Laboratories
  • Aspect Ratio
  • Cartesian Coordinates
  • Center Of Gravity
  • Differential Equations
  • Equations
  • Flow
  • Flow Fields
  • Free Stream
  • Leading Edges
  • Load Distribution
  • Mach Number
  • Partial Differential Equations
  • Pressure Distribution
  • Sweptback Wings
  • Trailing Edges

Technology Areas

  • Hypersonics