Accession Number:

AD0754051

Title:

Method of Calculating a Two-Phase Ejector,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1972-12-11

Pagination or Media Count:

20.0

Abstract:

A method of designing a two phase two component injector is presented on the basis of an experimental study. The operation of the injector is compared under subsonic and supersonic conditions. It is shown that for fixed conditions nozzle geometry and initial parameters there is a certain optimum area of the throat of the exit cone where the highest back pressure is reached. Author

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE