Analytical and computational techniques were developed to predict the stability behavior of liquid propellant rocket combustors using damping devices such as acoustic liners, slot absorbers, and injector face baffles. Models were developed to determine the frequency and decay rate of combustor oscillations, the spatial and temporal pressure waveforms, and the stability limits in terms of combustion response model parameters.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Combustion stability with baffles, absorbers and velocity sensitive combustion


    Beteiligte:

    Erscheinungsdatum :

    01.02.1980


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch