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Flowfield measurements in the NASA Lewis Research Center 9- by 15-foot low-speed wind tunnel by Hughes, Christopher E.
Published 1989Call Number: Loading…
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2
Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack by Hughes, Christopher E.
Published 1989Call Number: Loading…
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3
Experimental investigation of the subsonic high-altitude operation of the NASA Lewis 10- by 10-foot supersonic wind tunnel by Hughes, Christopher E.
Published 1988Call Number: Loading…
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4
Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations by Hughes, Christopher E.
Published 1988Call Number: Loading…
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5
The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator / by Hughes, Christopher E.
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Government Document eBook -
6
NASA collaborative research on the ultra high bypass engine cycle and potential benefits for noise, performance, and emissions / by Hughes, Christopher E.
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Government Document eBook -
7
Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan / by Hughes, Christopher E.
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Government Document eBook -
8
Performance optimization of a rotor alone Nacelle for acoustic fan testing / by Cunningham, C. C., Thompson, W. K., Hughes, Christopher E.
Published 2000Call Number: Loading…Online Access
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Government Document eBook -
9
Aircraft engine technology for green aviation to reduce fuel burn / by Hughes, Christopher E., Van Zante, Dale E., Heidmann, James D.
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10
The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor / by Bozak, Richard F., Hughes, Christopher E., Buckley, James (Mechanical engineer)
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11
Acoustic performance of the GEAE UPS research fan in the NASA Glenn 9- by 15-foot low-speed wind tunnel by Woodward, Richard P.
Published 2012Other Authors: “…Hughes, Christopher E.…”
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12
Acoustic performance of an advanced model turbofan in three aeroacoustic test facilities by Woodward, Richard P.
Published 2012Other Authors: “…Hughes, Christopher E.…”
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13
Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions by Woodward, Richard P.
Published 1990Other Authors: “…Hughes, Christopher E.…”
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14
Noise of a counterrotation propeller with simulated fuselage and support pylon at takeoff/approach conditions by Woodward, Richard P.
Published 1989Other Authors: “…Hughes, Christopher E.…”
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15
Flow analysis for the nacelle of an advanced ducted propeller at high angle-of-attack and at cruise with boundary layer control by Hwang, Danny P.
Published 1994Other Authors:Call Number: Loading…
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16
Performance optimization of a rotor alone Nacelle for acoustic fan testing by Cunningham, C. C.
Published 2000Other Authors:Call Number: Loading…
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Related Subjects
Acoustic properties
Wind tunnels
Aerodynamic characteristics
Aerodynamic noise
Low speed wind tunnels
Aeroacoustics
Automatic control
Error analysis
Fan blades
Fixed wings
Fuel consumption
NASA programs
Nacelles
Propellers, Aerial
Rotor speed
Test chambers
Wind tunnel tests
Acoustic measurement
Aerodynamics
Aeronautical engineering
Aeronautical laboratories
Air flow
Aircraft configurations
Aircraft engines
Aircraft fuels
Aircraft models
Aircraft noise
Aircraft performance
Angle of attack
Blade tips