Analysis of patients treated during four Disaster Medical Assistance Team deployments von Nufer, Kevin E., Wilson-Ramirez, Gina, Shah, Mark B., Hughes, Christopher E., Crandall, Cameron S.

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Benefits of Swept-and-Leaned Stators for Fan Noise Reduction von Woodward, Richard P, Elliott, David M, Hughes, Christopher E, Berton, Jeffrey J

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Fan Noise Reduction with Increased Bypass Nozzle Area von Woodward, Richard P, Hughes, Christopher E, Podboy, Gary G

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NASA Collaborative Research on the Ultra High Bypass Engine Cycle and Potential Benefits for Noise, Performance, and Emissions von Hughes, Christopher E.

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Ultra High Bypass Ratio Engine Research for Reducing Noise, Emissions, and Fuel Consumption von Hughes, Christopher E., Schweitzer, Jeff

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An Overview of the NASA Fundamental Aeronautics Program Subsonic Fixed Wing Project and Ultra High Bypass Partnership Research Goals von Hughes, Christopher E.

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Steady and unsteady flow field measurements within a NASA 22-inch fan model von Podboy, Gary G, Krupar, Martin J, Helland, Stephen M, Hughes, Christopher E

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Acoustic Performance of an Advanced Model Turbofan in Three Aeroacoustic Test Facilities von Woodward, Richard P., Hughes, Christopher E.

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Acoustic Performance of the GEAE UPS Research Fan in the NASA Glenn 9- by 15-Foot Low-Speed Wind Tunnel von Woodward, Richard P., Hughes, Christopher E.

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Aircraft Engine Technology for Green Aviation to Reduce Fuel Burn von Hughes, Christopher E., VanZante, Dale E., Heidmann, James D.

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NASA / GE Aviation Collaborative Partnership Research in Ultra High Bypass Cycle Propulsion Concepts von Hughes, Christopher E., Zeug, Theresa

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The Aerodynamic Performance of an Over-the-Rotor Liner With Circumferential Grooves on a High Bypass Ratio Turbofan Rotor von Bozak, Richard F., Hughes, Christopher E., Buckley, James

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The Effect of Bypass Nozzle Exit Area on Fan Aerodynamic Performance and Noise in a Model Turbofan Simulator von Hughes, Christopher E., Podboy, Gary, G., Woodward, Richard P., Jeracki, Robert, J.

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Aerodynamic Performance of Scale-Model Turbofan Outlet Guide Vanes Designed for Low Noise von Hughes, Christopher E.

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Turbofan Noise Studied in Unique Model Research Program in NASA Glenn's 9- by 15-Foot Low-Speed Wind Tunnel von Hughes, Christopher E.

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Testing of a Microwave Blade Tip Clearance Sensor at the NASA Glenn Research Center von Woike, Mark R., Roeder, James W., Hughes, Christopher E., Bencic, Timothy J.

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Low-Noise Potential of Advanced Fan Stage Stator Vane Designs Verified in NASA Lewis Wind Tunnel Test von Hughes, Christopher E.

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An Assessment of Current Fan Noise Prediction Capability von Envia, Edmane, Woodward, Richard P., Elliott, David M., Fite, E. Brian, Hughes, Christopher E., Podboy, Gary G., Sutliff, Daniel L.

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Turbofan Noise Reduction Associated With Increased Bypass Nozzle Flow von Woodward, Richard P., Hughes, Christopher E.

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Noise Benefits of Increased Fan Bypass Nozzle Area von Woodward, Richard P., Hughes, Christopher E.

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