This paper presents a control-oriented model of the flow, reaction, and transport processes in liquid propellant rocket combustion chambers, based on the multicomponent conservation laws of gas dynamics. This model provides a framework for the inclusion of detailed chemical kinetic relations, viscous and other dissipative effects, a variety of actuators and sensors, as well as process and measurement disturbances. In addition to its potential usefulness to the designer in understanding the dynamical complexity of the system and the sources of model uncertainty, the model provides a rigorous basis for control system design. An appraisal of current and feasible actuators and sensors, and their mathematical representation are included.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Control-oriented modeling of combustion and flow processes in liquid propellant rocket engines


    Beteiligte:

    Erscheinungsdatum :

    01.07.1990


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Combustion instability analysis for liquid propellant rocket engines

    Kim, Y. M. / Chen, C. P. / Ziebarth, J. P. | NTRS | 1992




    On Nonlinear Combustion Instability in Liquid Propellant Rocket Engines

    Flandro, Gary / Sims, Joseph / Majdalani, Joseph | AIAA | 2004