Abstract For a thrust-adjustable rocket motor, to avoid unstable combustion, we not only need to consider nozzle damping before thrust adjustment, but also need to consider nozzle damping variation thereafter, and it is important to learn about the influence of nozzle damping before, and after, thrust adjustment. This chapter discusses wave attenuation method for predicting nozzle damping of the fluidic nozzle, validation of numerical prediction method for nozzle damping, and gives the nozzle damping variation with different secondary flow parameters.


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    Titel :

    Nozzle Damping of the Fluidic Nozzle


    Beteiligte:
    Xie, Kan (Autor:in) / Chen, Xinmin (Autor:in) / Li, Junwei (Autor:in) / Liu, Yu (Autor:in)


    Erscheinungsdatum :

    2019-01-01


    Format / Umfang :

    10 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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