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  • AIRCRAFT PROPULSION AND POWER  (2)
  • 1
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    Unknown
    Distribution analysis for F100(3) engine (1980)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: 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.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-CR-159754 , FR-12087
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
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    Computer modeling of fan-exit-splitter spacing effects on F100 response to distortion (1982)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The distortion response of the F100(3) engine was effected by the fan exit splitter configuration. The sensitivity for a proximate splitter fan is calculated to be slightly greater than a remote splitter configuration with identical airfoils. Predicted response was based upon a multiple segment parallel compressor Model modified to include a bypass ratio representation that effects the performance characteristics of the last rotor and intermediate case struts. The predicted distortion response required an accurate definition of row pre- and post-stall undistorted operation.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-CR-167879 , NAS 1.26:167879 , FR-15596
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
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