Analytical and Experimental Investigation of Performance of Supersonic Ejector Nozzles,

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Document Details

Document Type
Technical Report
Publication Date
Jul 21, 1982
Accession Number
ADA118279

Entities

People

  • Chen Zhongqing
  • Shen Huili

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Boundary Layer
  • Coordinate Systems
  • Experimental Data
  • Flow
  • Flow Fields
  • Flow Rate
  • Gas Turbine Nozzles
  • Inviscid Flow
  • Mach Number
  • Mass Flow
  • Pressure Distribution
  • Secondary Flow
  • Stagnation Pressure
  • Stagnation Temperature
  • Static Pressure
  • Test Facilities
  • Viscous Flow

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow