Acoustic dissipation studies were carried out to determine effect of purely geometric variables on acoustic performance leading to axial mode combustion instability; by using interchangeable parts, it was possible to vary nozzle throat diameter and to simulate geometry of cylindrical-bore grain at various motor burn times; model was acoustically driven by pulse decay, steady-state decay, and steady-state resonance; methods are compared, and applicability of each is discussed; steady-state-resonance method is suitable and promising.


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    Title :

    Acoustic attenuation experiments on subscale, cold-flow rocket motors


    Additional title:

    AIAA J


    Contributors:

    Published in:

    AIAA Journal ; 5 , n 2


    Publication date :

    1967


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Acoustic attenuation experiments on subscale, cold-flow rocket motors.

    BUFFUM, F. G. / DEHORITY, G. L. / PRICE, E. W. | AIAA | 1967


    Acoustic attenuation experiments on subscale, cold-flow rocket motors

    BUFFUM, JR., F. / DEHORITY, G. / PRICE, E. | AIAA | 1966


    Subscale cold-flow simulation of the port flow in solid rocket motors

    Yeh, Y. / Heaman, J. / Ramachandran, N. et al. | AIAA | 1994


    Subscale Cold-Flow Simulation of the Port Flow in Solid Rocket Motors

    Yeh, Y. P. / Heaman, J. P. / Ramachandran, N. et al. | British Library Conference Proceedings | 1994


    Ballistic anomaly trends in subscale solid rocket motors

    BECKMAN, C. / GEISLER, R. | AIAA | 1982