1–20 of 28 hits
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    Flow disruption devices for the reduction of high lift system noise

    Free access
    HUTCHESON FLORENCE V / BROOKS THOMAS F | European Patent Office | 2019

    Flow Disruption Devices for the Reduction of High Lift System Noise

    Free access
    HUTCHESON FLORENCE V / BROOKS THOMAS F | European Patent Office | 2016

    Blade Wake Interaction Noise for a Main Rotor

    Brooks, Thomas F. | Online Contents | 2004

    Flap-edge aeroacoustic measurements and predictions

    Brooks, Thomas F. | Online Contents | 2003

    Low-Noise Rotorcraft Blades

    Brooks, Thomas F. | NTRS | 1994

    Airframe Noise from a Hybrid Wing Body Aircraft Configuration

    Hutcheson, Florence V. / Spalt, Taylor B. / Brooks, Thomas F. et al. | AIAA | 2016

    Airframe Noise from a Hybrid Wing Body Aircraft Configuration (AIAA 2016-2708)

    Hutcheson, Florence V. / Spalt, Taylor B. / Brooks, Thomas F. et al. | British Library Conference Proceedings | 2016

    Jet Noise Shielding Provided by a Hybrid Wing Body Aircraft

    Doty, Michael J. / Brooks, Thomas F. / Burley, Casey L. et al. | AIAA | 2014

    Acoustic Data Processing and Transient Signal Analysis for the Hybrid Wing Body 14- by 22-Foot Subsonic Wind Tunnel Test

    Bahr, Christopher J. / Brooks, Thomas F. / Humphreys, William M. et al. | AIAA | 2014

    Acoustics and Surface Pressure Measurements from Tandem Cylinder Configurations

    Hutcheson, Florence V. / Brooks, Thomas F. / Lockard, David P. et al. | AIAA | 2014

    Shielding of Turbomachinery Broadband Noise from a Hybrid wing Body Aircraft Configuration

    Hutcheson, Florence V. / Brooks, Thomas F. / Burley, Casey L. et al. | AIAA | 2014

    Calibrations of the NASA Langley 14- by 22-Foot Subsonic Tunnel in Acoustic Configuration

    Spalt, Taylor B. / Brooks, Thomas F. / Bahr, Christopher J. et al. | AIAA | 2014

    Noise Scaling and Community Noise Metrics for the Hybrid Wing Body Aircraft

    Burley, Casey L. / Brooks, Thomas F. / Hutcheson, Florence V. et al. | AIAA | 2014

    Development of a Microphone Phased Array Capability for the Langley 14- by 22-foot Subsonic Tunnel

    Humphreys, William M. / Brooks, Thomas F. / Bahr, Christopher J. et al. | AIAA | 2014

    Reduction of Helicopter Blade-Vortex Interaction Noise by Active Rotor Control Technology

    Yu, Yung H. / Gmelin, Bernd / Splettstoesser, Wolf et al. | NTRS | 1997

    Noise Scaling and Community Noise Metrics for the Hybrid Wing Body Aircraft

    Burley, Casey L. / Brooks, Thomas F. / Hutcheson, Florence V. et al. | NTRS | 2014