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Overview on Basis and Use of Performance Prediction MethodsThe lecture outlines the basic methods of component matching which are central to the prediction of gas turbine performance. Steady state prediction of off-design performance must be done at the beginning of an engine development program, to ensure that the engine can satisfy all the mission requirements. The matching techniques can be extended to predict transient performance, which is essential for controls development and to ensure good engine handling. The large amount of computation required demands the use of computer modelling and the role of modelling in the development program and the basic requirements for performance modelling are described.
Document ID
19920019216
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
H I H Saravanamuttoo
(Carleton University Ottawa, Ontario, Canada)
Date Acquired
August 15, 2013
Publication Date
May 1, 1992
Publication Information
Publication: Steady and Transient Performance Prediction of Gas Turbine Engines
Publisher: Advisory Group for Aerospace Research and Development (AGARD)
ISBN: 928350674X
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: AGARD Lecture Series 183
Location: Chatillon / Bagneaux
Country: FR
Start Date: June 11, 1992
End Date: June 12, 1992
Sponsors: North Atlantic Treaty Organization
Accession Number
92N28459
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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