RESEARCH PAPERS: Gas Turbines: Aircraft

A Conceptual Design Methodology for Predicting Bleed and Horsepower Requirements of Military Aircraft Engines

[+] Author and Article Information
J. D. Cyrus

Naval Aircraft Warfare Center, Warminster, PA 18974

J. Eng. Gas Turbines Power 118(3), 481-485 (Jul 01, 1996) (5 pages) doi:10.1115/1.2816671 History: Online November 19, 2007


Conceptual design codes have been developed to provide conceptual design estimates of bleed and horsepower extraction requirements of advanced military aircraft. This paper describes the methodology for the computer codes. The validity of the models was assessed by generating bleed and horsepower estimates for four advanced air-craft configurations not included in the data base and comparing the model estimates to manufacturer’s estimates.

Copyright © 1996 by The American Society of Mechanical Engineers
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