Method of Calculating Rocket Engine Nozzle Contour for Optimum Thrust,

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Document Details

Document Type
Technical Report
Publication Date
Aug 03, 1982
Accession Number
ADA118931

Entities

People

  • Tian Minhua

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Angle Of Incidence
  • Control Surfaces
  • Coordinate Systems
  • Curvature
  • Engines
  • Flow
  • Flow Fields
  • Flow Rate
  • Gas Turbine Nozzles
  • Mach Number
  • Nozzles
  • Peak Values
  • Rocket Engines
  • Rockets
  • Specific Heat
  • Surfaces
  • Two Dimensional