Accession Number:

AD0641111

Title:

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

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Voroguishin,V. T.

Report Date:

1966-04-18

Pagination or Media Count:

13.0

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

Descriptors:

• (*RAMJET ENGINES
• SUPERSONIC FLIGHT)
• HEAT EXCHANGERS
• PERFORMANCE(ENGINEERING)
• TEMPERATURE
• THRUST
• VELOCITY
• USSR

Subject Categories:

• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE