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Frequency response of a jet engine test facility air supply systemThe frequency response of a laboratory scale model of a portion of the air supply system of an engine test facility is obtained both experimentally and using one-dimensional, small-signal, distributed parameter theory. The effects of line terminations and mean flow are considered. Good agreement between experiment and theory is obtained. Predictions are extended to a full scale test facility air supply system operating under several possible test conditions.
Document ID
19850037334
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Franke, M. E.
(USAF, Institute of Technology, Wright-Patterson AFB OH, United States)
Ross, M. L.
(NASA Johnson Space Center Houston, TX; USAF, Institute of Technology, Wright-Patterson AFB, OH, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 85-0053
Accession Number
85A19485
Distribution Limits
Public
Copyright
Other

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