This report results from a contract tasking Dipanmento Di Ingegneria Aerospaziale as follows: The contractor will review Russian works on response function of solid propellant combustion to oscillatory pressure and on acoustic admittance. Differences and similarities between US and Russian approaches to this problem shall be considered.


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    Title :

    Nonlinear Interaction Between Acoustics and Propellant Combustion


    Contributors:

    Publication date :

    1996


    Size :

    42 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English