Distribution analysis for F100(3) engine
- Author
- Shaw, M.
- Published
- Jan 1, 1980.
- Physical Description
- 1 electronic document
- Additional Creators
- Walter, W. A.
Online Version
- hdl.handle.net , Connect to this object online.
- Restrictions on Access
- Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access - Summary
- The 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.
- Other Subject(s)
- Collection
- NASA Technical Reports Server (NTRS) Collection.
- Note
- Document ID: 19800008813.
Accession ID: 80N17073.
NASA-CR-159754.
FR-12087. - Terms of Use and Reproduction
- No Copyright.
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