An update on the Moog SureFly vehicle acoustic hover test and predictions is presented. Data were acquired for a 15’ hover altitude. Preliminary predictions using CAMRAD coupled with ANOPP have been completed. The predictions are currently using a generic blade geometry. High resolution blade scans have been initiated for the same type of rotor as that used on the SureFly vehicle and the resulting coordinates will be implemented in future prediction efforts. Plans for a future hover test at higher altitudes are discussed.


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    Titel :

    Status of Moog SureFly Hover Test and Progress on Noise Prediction Efforts


    Beteiligte:
    Brenda Henderson (Autor:in) / Jordan Cluts (Autor:in) / Alexander Svetgoff (Autor:in)

    Kongress:

    Spring NASA Acoustics Technical Working Group Meeting ; 2023 ; Hampton, VA, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Moog SureFly® Hover Test Update

    Brenda Henderson / Jordan Cluts / Devin Boyle et al. | NTRS


    Preliminary Analysis of Moog SureFly Electric Motor Noise Measurements

    Brenda Henderson / Jordan Cluts / Devin Boyle et al. | NTRS


    NOISE MEASUREMENTS FROM GROUND TESTS OF THE MOOG SUREFLY VEHICLE

    Huff, Dennis L. / Henderson, Brenda S. / Cluts, Jordan D. et al. | TIBKAT | 2021


    Noise Measurements from Ground Tests of the Moog SureFly Vehicle

    D. Huff / B. Henderson / J. Cluts et al. | NTIS | 2020


    Moog SureFly® Hover Test Update

    B. Henderson / J. Cluts / D. Boyle et al. | NTIS | 2022