Showing 1 - 14 results of 14 for search 'Hughes, Christopher E', query time: 0.75s Refine Results
  1. 1
    Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan /

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    Government Document Book
  2. 2
    The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator /

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    Government Document Book
  3. 3
    NASA collaborative research on the ultra high bypass engine cycle and potential benefits for noise, performance, and emissions /

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    Government Document Book
  4. 4
    Flowfield measurements in the NASA Lewis Research Center 9- by 15-foot low-speed wind tunnel
    by Hughes, Christopher E
    Published 1989

    Government Document Book
  5. 5
    Experimental investigation of the subsonic high-altitude operation of the NASA Lewis 10- by 10-foot supersonic wind tunnel
    by Hughes, Christopher E
    Published 1988

    Government Document Book
  6. 6
    Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack
    by Hughes, Christopher E
    Published 1989

    Government Document Book
  7. 7
    The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  8. 8
    Performance optimization of a rotor alone Nacelle for acoustic fan testing /

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    Government Document Book
  9. 9
    Aircraft engine technology for green aviation to reduce fuel burn /

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    Government Document Book
  10. 10
    Acoustic performance of an advanced model turbofan in three aeroacoustic test facilities /
    Other Authors: “...Hughes, Christopher E...”

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    Government Document Book
  11. 11
    Acoustic performance of the GEAE UPS research fan in the NASA Glenn 9- by 15-foot low-speed wind tunnel /
    Other Authors: “...Hughes, Christopher E...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  12. 12
    Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions
    by Woodward, Richard P
    Published 1990
    Other Authors: “...Hughes, Christopher E...”

    Government Document Book
  13. 13
    Noise of a counterrotation propeller with simulated fuselage and support pylon at takeoff/approach conditions
    by Woodward, Richard P
    Published 1989
    Other Authors: “...Hughes, Christopher E...”

    Government Document Book
  14. 14
    Performance optimization of a rotor alone Nacelle for acoustic fan testing /
    by Cunningham, C. C
    Published 2000
    Other Authors: “...Hughes, Christopher E...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
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