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Aircraft Engine SystemsThe objective is to develop the capability to numerically model the performance of gas turbine engines used for aircraft propulsion. This capability will provide turbine engine designers with a means of accurately predicting the performance of new engines in a system environment prior to building and testing. The 'numerical test cell' developed under this project will reduce the number of component and engine tests required during development. As a result, the project will help to reduce the design cycle time and cost of gas turbine engines. This capability will be distributed to U.S. turbine engine manufacturers and air framers. This project focuses on goals of maintaining U.S. superiority in commercial gas turbine engine development for the aeronautics industry.
Document ID
20030068085
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Veres, Joseph P. (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2003
Publication Information
Publication: 2002 Computing and Interdisciplinary Systems Office Review and Planning Meeting
Subject Category
Aircraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle20030068074Collected Works2002 Computing and Interdisciplinary Systems Office Review and Planning Meeting
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