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Advanced exhaust nozzle technology

Conference:

Abstract

Recent developments in turbine engine exhaust nozzle technology include nonaxisymmetric nozzles, thrust reversing, and thrust vectoring. Trade studies have been performed to determine the impact of these developments on the thrust-to-weight ratio and specific fuel consumption of an advanced high performance, augmented turbofan engine. Results are presented in a manner which provides an understanding of the sources and magnitudes of differences in the basic elements of nozzle internal performance and weight as they relate to conventional, axisymmetric nozzle technology. Conclusions are presented and recommendations are made with regard to future directions of advanced development and demonstration. 5 refs.
Publication Date:
Jan 01, 1981
Product Type:
Conference
Report Number:
CONF-8105204-
Reference Number:
EDB-83-067733
Resource Relation:
Journal Name: AGARD Conf. Proc.; (France); Journal Volume: 301; Conference: AGARD symposium on fluid dynamics panel, Toulouse, France, 11 May 1981
Subject:
32 ENERGY CONSERVATION, CONSUMPTION, AND UTILIZATION; AIRCRAFT; GAS TURBINES; EXHAUST SYSTEMS; FUEL CONSUMPTION; NOZZLES; MILITARY EQUIPMENT; ENERGY CONSUMPTION; EQUIPMENT; MACHINERY; TURBINES; TURBOMACHINERY; 320201* - Energy Conservation, Consumption, & Utilization- Transportation- Air & Aerospace
OSTI ID:
6484995
Research Organizations:
US Air Force Wright Aeronaut Lab, Wright-Patterson AFB, Ohio, USA
Country of Origin:
France
Language:
English
Other Identifying Numbers:
Journal ID: CODEN: AGCPA
Submitting Site:
HEDB
Size:
Pages: 14.1-14.11
Announcement Date:
Feb 01, 1983

Conference:

Citation Formats

Glidewell, R J, and Warburton, R E. Advanced exhaust nozzle technology. France: N. p., 1981. Web.
Glidewell, R J, & Warburton, R E. Advanced exhaust nozzle technology. France.
Glidewell, R J, and Warburton, R E. 1981. "Advanced exhaust nozzle technology." France.
@misc{etde_6484995,
title = {Advanced exhaust nozzle technology}
author = {Glidewell, R J, and Warburton, R E}
abstractNote = {Recent developments in turbine engine exhaust nozzle technology include nonaxisymmetric nozzles, thrust reversing, and thrust vectoring. Trade studies have been performed to determine the impact of these developments on the thrust-to-weight ratio and specific fuel consumption of an advanced high performance, augmented turbofan engine. Results are presented in a manner which provides an understanding of the sources and magnitudes of differences in the basic elements of nozzle internal performance and weight as they relate to conventional, axisymmetric nozzle technology. Conclusions are presented and recommendations are made with regard to future directions of advanced development and demonstration. 5 refs.}
journal = {AGARD Conf. Proc.; (France)}
volume = {301}
place = {France}
year = {1981}
month = {Jan}
}