The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1947
Accession Number
ADB805606

Entities

People

  • Richard Scherrer

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Altitude
  • Bodies
  • Boundaries
  • Boundary Layer
  • Equations
  • Flight
  • Heat Energy
  • Heat Transfer
  • Laminar Boundary Layer
  • Layers
  • Mach Number
  • Pressure Distribution
  • Revolutions
  • Reynolds Number
  • Supersonic Flight
  • Surface Temperature
  • Temperature Gradients

Technology Areas

  • Hypersonics