A series of experiments were conducted in an anechoic hover chamber to investigate the noise and performance of an ideally twisted rotor design. The results of this test were compared with those of noise prediction tools.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Ideally Twisted Rotor Testing and Predictions


    Contributors:

    Conference:

    NASA Acoustics Technical Working Group ; 2018 ; Hampton, VA, US


    Publication date :

    2020-04-08


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Acoustic and Performance Characteristics of an Ideally Twisted Rotor in Hover

    N. A. Pettingill / N. S. Zawodny / C. S. Thurman et al. | NTIS | 2020


    Acoustics and Performance Characteristics of an Ideally Twisted Rotor in Hover

    Nicole A. Pettingill / Nikolas S. Zawodny / Christopher S. Thurman et al. | NTRS


    ACOUSTIC AND PERFORMANCE CHARACTERISTICS OF AN IDEALLY TWISTED ROTOR IN HOVER

    Pettingill, Nicole A. / Zawodny, Nikolas S. / Thurman, Christopher et al. | TIBKAT | 2021


    Acoustic and Performance Characteristics of an Ideally Twisted Rotor in Hover

    Pettingill, Nicole A. / Zawodny, Nikolas S. / Thurman, Christopher et al. | AIAA | 2021


    Acoustic and Performance Characteristics of an Ideally Twisted Rotor in Hover

    Nicole A. Pettingill / Nikolas S. Zawodny / Christopher S. Thurman et al. | NTRS