Open cavities exposed to a grazing flow can exhibit large pressure fluctuations, which may result in damage to stores or components carried within a weapon bay. This study investigates the use of passive resonant absorbers based on Helmholtz resonators to attenuate the problematic pressure fluctuations that arise in cavity flows, under both transonic (0.80


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Passive Attenuation of Modal Cavity Aeroacoustics Under Supersonic and Transonic Conditions



    Published in:

    Publication date :

    2015




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik / 55.60 / 50.93 / 55.50 / 50.93 Weltraumforschung
    Local classification TIB:    770/7040



    Passive Attenuation of Modal Cavity Aeroacoustics Under Supersonic and Transonic Conditions

    Roberts, David A. / MacManus, David G. / Johnson, Rudy A. et al. | AIAA | 2014


    CONJUNCTION OF AEROELASTICITY AND AEROACOUSTICS IN TRANSONIC CAVITY FLOW

    Nilsson, S. / Yao, H. / Karlsson, A. et al. | TIBKAT | 2023


    The Aeroacoustics of Transonic Helicopter Blades

    Morgans, Aimee / Dowling, Ann | AIAA | 2002


    Aeroacoustics of supersonic elliptic jets

    Khavaran, Abbas / Georgiadis, Nicholas | AIAA | 1996


    Aeroacoustics of transonic shock-boundary layer interactions

    Pirozzoli, Sergio / Berardini, Matteo / Grasso, Francesco | AIAA | 2007