Accession Number:

AD0603947

Title:

THE PROBLEM OF DETERMINING THE OPTIMUM CRITICAL OPERATING PARAMETERS FOR A NONISOBARIC MOTOR WITH DIVERGENT NOZZLE,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1964-08-04

Pagination or Media Count:

56.0

Abstract:

A solution is given to the problem of nonsteady state operation of a liquid rocket motor, using the dynamical differential equations of turbulent flow. The solutions are used to determine the optimum and critical parameters, together with the stability limits, on the basis of a nonisobaric motor model. The determination of these parameters makes it possible to correct the design method used for rocket motors. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE