Effect of Aspect Ratio and Taper on the Pressure Drag at Supersonic Speeds of Upswept Wings at Zero Lift

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1947
Accession Number
ADA381081

Entities

People

  • Jack N. Nielsen

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms
  • C4I
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Aircraft Equipment
  • Aircrafts
  • Aspect Ratio
  • Boundaries
  • Coefficients
  • Drag
  • Dynamic Pressure
  • Flow
  • Free Stream
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Static Pressure
  • Trailing Edges
  • Wing Tips

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow