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  • 1
    facet.materialart.
    Unknown
    Flight evaluation of an engine static pressure noseprobe in an F-15 airplane (1981)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The flight testing of an inlet static pressure probe and instrumented inlet case produced results consistent with sea-level and altitude stand testing. The F-15 flight test verified the basic relationship of total to static pressure ratio versus corrected airflow and automatic distortion downmatch with the engine pressure ratio control mode. Additionally, the backup control inlet case statics demonstrated sufficient accuracy for backup control fuel flow scheduling, and the station 6 manifolded production probe was in agreement with the flight test station 6 tota pressure probes.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-CR-163109 , NAS 1.26:163109 , FR-14915
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 2
    facet.materialart.
    Unknown
    Data analysis of P sub T/P sub S noseboom probe testing on F100 engine P680072 at NASA Lewis Research Center (1980)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: Results from the altitude testing of a P sub T/P sub S noseboom probe on the F100 engine are discused. The results are consistent with sea level test results. The F100 engine altitude test verified automatic downmatch with the engine pressure ratio control, and backup control inlet case static pressure demonstrated sufficient accuracy for backup control fuel flow scheduling. The production P6 probe measured Station 6 pressures accurately for both undistorted and distorted inlet airflows.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-CR-159816 , PWA-FR-12540
    Format: application/pdf
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
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