Accession Number:

ADA017798

Title:

Turbofan Cycle, Performance and Design Analysis,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1975-03-20

Pagination or Media Count:

28.0

Abstract:

A turbofan cycle analysis has been carried out to predict the effect of cycle independent variables - e.g. compressor pressure ratio, bypass ratio, fan pressure ratio and turbine entry temperature - on specific fuel consumption. Influence of these variables on engine performance for different flight conditions and engine ratings has been shown.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE