Significance of acoustic gains and losses to problem of rocket motor stability and progress made toward understanding of loss mechanisms; with respect to acoustic gains, burning surface of propellant is recognized to be principal source of acoustic amplification, and efforts are directed towards determination of propellant response function; theoretical unpublished calculations indicate that under some conditions radiation may exert important influence on acoustic response of burning surface, especially at low burning rates; nature of new calculations and some of numerical results.


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    Title :

    Linear acoustic gains and losses in solid propellant rocket motors


    Additional title:

    AIAA J


    Contributors:
    Cantrell, R.H. (author) / Hart, R.W. (author) / McClure, F.T. (author)

    Published in:

    AIAA Journal ; 2 , n 6


    Publication date :

    1964


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Linear acoustic gains and losses in solid propellant rocket motors

    CANTRELL, R. H. / HART, R. W. / MC CLURE et al. | AIAA | 1964




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