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Summary of investigations of engine response to distorted inlet conditionsA survey is presented of experimental and analytical experience of the NASA Lewis Research Center in engine response to inlet temperature and pressure distortions. Results of experimental investigations and analytical modeling are reviewed together with a description of the hardware and the techniques employed. Distortion devices successfully simulated inlet distortion, and knowledge was gained on compression system response to different types of distortion. A list of NASA research references is included.
Document ID
19870015044
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Biesiadny, Thomas J.
(NASA Lewis Research Center Cleveland, OH, United States)
Braithwaite, Willis M.
(NASA Lewis Research Center Cleveland, OH, United States)
Soeder, Ronald H.
(NASA Lewis Research Center Cleveland, OH, United States)
Abdelwahab, Mahmood
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1987
Publication Information
Publication: AGARD Engine Response to Distorted Inflow Conditions
Subject Category
Aircraft Propulsion And Power
Accession Number
87N24477
Distribution Limits
Public
Copyright
Other
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