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Distribution analysis for F100(3) engineThe F100(3) compression system response to inlet circumferential distortion was investigated using an analytical compressor flow model. Compression system response to several types of distortion, including pressure, temperature, and combined pressure/temperature distortions, was investigated. The predicted response trends were used in planning future F100(3) distortion tests. Results show that compression system response to combined temperature and pressure distortions depends upon the relative orientation, as well as the individual amplitudes and circumferential extents of the distortions. Also the usefulness of the analytical predictions in planning engine distortion tests is indicated.
Document ID
19800008813
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Walter, W. A. (Pratt and Whitney Aircraft Group West Palm Beach, FL, United States)
Shaw, M. (Pratt and Whitney Aircraft Group West Palm Beach, FL, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
FR-12087
NASA-CR-159754
Report Number: FR-12087
Report Number: NASA-CR-159754
Accession Number
80N17073
Funding Number(s)
CONTRACT_GRANT: NAS3-20835
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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