Aerodynamic and Thermodynamic Characteristics of Supersonic Ramjet Engine with Mach Number between 3 and 7. Part II. Calculation and Analysis of Thermodynamic Properties,

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Document Details

Document Type
Technical Report
Publication Date
Mar 17, 1980
Accession Number
ADA082963

Entities

People

  • Liu Kao-lien
  • Liu Tien-kuei
  • Tiao Chen-kang
  • Wu Chung-hua

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Materials and Manufacturing Processes
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Back Pressure
  • Combustion
  • Combustion Chambers
  • Combustion Products
  • Efficiency
  • Energy Efficiency
  • Equations
  • Flight Paths
  • Heat Energy
  • Heat Transfer
  • High Temperature
  • Hydrocarbon Fuels
  • Mach Number
  • Ramjet Engines
  • Subsonic Combustion
  • Supersonic Combustion
  • Thermodynamic Properties

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow