Three-Dimensional Supersonic Nozzles and Inlets of Arbitrary Exit Cross Section

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1952
Accession Number
ADA380474

Entities

People

  • John C. Evvard
  • Stephen M. Maslen

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Axisymmetric
  • Axisymmetric Flow
  • Boundaries
  • Diffusers
  • Equations
  • Flow
  • Fluid Flow
  • Free Stream
  • Hypersonic Wind Tunnels
  • Mach Number
  • Nozzles
  • Shape
  • Supersonic Nozzles
  • Three Dimensional
  • Two Dimensional
  • Wind Tunnel Nozzles
  • Wind Tunnels

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow