Accession Number:

AD0606653

Title:

INLET EFFICIENCY PARAMETERS FOR SUPERSONIC COMBUSTION RAMJET ENGINES

Descriptive Note:

Technical Report,01 Nov 1962,30 Apr 1963

Corporate Author:

AIR FORCE AERO PROPULSION LAB WRIGHT-PATTERSON AFB OH WRIGHT-PATTERSON AFB

Personal Author(s):

Report Date:

1964-06-01

Pagination or Media Count:

59.0

Abstract:

In this report, the various definitions of inlet efficiency, which are currently in use for supersonic combustion ramjet engines, are surveyed. Derivations of each of these parameters and the relationships between them are presented. Charts for the conversion from one parameter of efficiency to another are included. These charts are based on real gas properties. Attention is drawn to the application of available energy concepts to the supersonic combustion ramjet engine, and a definition of inlet effectiveness is introduced.

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE