The liquid rocket engine stability prediction software (LCI) predicts combustion stability of systems using LOX-LH2 propellants. Both longitudinal and transverse mode stability characteristics are calculated. This software has the unique feature of being able to predict system limit amplitude.


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    Titel :

    Nonlinear Combustion Instability Prediction


    Beteiligte:
    Flandro, Gary (Autor:in)


    Erscheinungsdatum :

    2010-09-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Combustion instability prediction using a nonlinear bipropellant vaporization model

    Hoffman, R. J. / Wright, R. O. / Breen, B. P. | TIBKAT | 1968


    On nonlinear combustion instability

    Malhotra, S. / Flandro, G. | AIAA | 1997


    Nonlinear combustion instability data reduction

    Flandro, G. / Malhotra, S. / Garza, D. | AIAA | 1996