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.


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    Titel :

    Ideally Twisted Rotor Testing and Predictions


    Beteiligte:

    Kongress:

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


    Erscheinungsdatum :

    08.04.2020


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Acoustics and Performance Characteristics of an Ideally Twisted Rotor in Hover

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    Acoustic and Performance Characteristics of an Ideally Twisted Rotor in Hover

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


    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