HYPERSONIC FLOW OVER A SLENDER CONE WITH GAS INJECTION

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Document Details

Document Type
Technical Report
Publication Date
Nov 05, 1962
Accession Number
AD0295154

Entities

People

  • Hartley H. King

Organizations

  • University of California, Berkeley

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Boundary Layer
  • Boundary Layer Flow
  • Curvature
  • Data Reduction
  • Drag
  • Flow
  • Flow Rate
  • Fluid Dynamics
  • Geometry
  • Inviscid Flow
  • Mass Flow
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Skin Friction
  • Wind Tunnels

Technology Areas

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