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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    Title :

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


    Contributors:

    Conference:

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


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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