Calculation of Flat Asymmetrical Nozzles with a Supersonic Inlet Velocity,

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Document Details

Document Type
Technical Report
Publication Date
Aug 25, 1977
Accession Number
ADA051474

Entities

People

  • V. N. Zudov
  • V. V. Shumskiy
  • V. V. Zatoloka

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Air Force
  • Combustion
  • Engines
  • Flow
  • Flow Fields
  • Foreign Technology
  • Inlets
  • Jet Engines
  • Nozzles
  • Security
  • Supersonic Inlets
  • Supersonic Nozzles
  • Translations

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow