SELECTION OF THE OPTIMUM PARAMETERS OF A SUPERSONIC RAMJET ENGINE WITH A HEAT EXCHANGER,

Abstract

The work contains the procedure for computing the supersonic ramjet engine with a heat exchanger. In it there is analysed the influence of the temperature of heat, the flow T*, and the speed of flight on the value and the coefficient of thrust, and the influence of a series of parameters on the required heat emitting surface. The results of the work enable one to proceed with the choice of the original optimum parameters in the computation of the supersonic ramjet engine with a heat exchanging apparatus. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 18, 1966
Accession Number
AD0641111

Entities

People

  • V. T. Voroguishin

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Coefficients
  • Computations
  • Engines
  • Heat Exchangers
  • Heat Transfer Devices
  • Ramjet Engines

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Regression Analysis.

Technology Areas

  • Hypersonics