Test executed from June 6 through July 3, 2011. Objectives -  Understand maneuver acoustics -  Validate ground footprint acoustic codes -  Incorporate maneuvers into acoustic ground footprint prediction codes Acoustic measurement of -  Source noise - Steady and transient maneuvers - Approach profiles Large test crew: 23 people from 7 organizations. Acquired 410 individual data points over 10 testing days and 30.6 flight hours. All “Priority One” and “Priority Two” test conditions measured.


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    Titel :

    Maneuver Acoustic Flight Test of the Bell 430 Helicopter


    Beteiligte:
    Michael Watts (Autor:in)

    Kongress:

    NASA Fundamental Aeronautics Program 2012 Technical Conference ; 2012 ; Cleveland, OH, US


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Maneuver Acoustic Flight Test of the Bell 430 Helicopter

    M. E. Watts / R. Snider / E. Greenwood et al. | NTIS | 2012


    Maneuver Acoustic Flight Test of the Bell 430 Helicopter

    Watts, Michael E. / Snider, Royce / Greenwood, Eric et al. | NTRS | 2012


    Maneuver Acoustic Flight Test of the Bell 430 Helicopter

    Snider, R. / Greenwood, E. / Baden, J. et al. | British Library Conference Proceedings | 2012


    Maneuver Acoustic Flight Test of the Bell 430 Helicopter Data Report

    Watts, Michael E. / Greenwood, Eric / Smith, Charles D. et al. | NTRS | 2014


    Maneuver Acoustic Flight Test of the Bell 430 Helicopter Data Report

    M. E. Watts / E. Greenwood / C. D. Smith et al. | NTIS | 2014