Laminar Boundary Layer on Cone in Supersonic Flow at Large Angle of Attack

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1953
Accession Number
ADA278326

Entities

People

  • Franklin K. Moore

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Biomedical
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Air Force
  • Aircrafts
  • Boundaries
  • Boundary Layer
  • Boundary Value Problems
  • Differential Equations
  • Engineering
  • Equations
  • Flow
  • Friction
  • Laminar Boundary Layer
  • Layers
  • Skin Friction
  • Supersonic Flow
  • United States

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers