In the process of developing the variable thrust rocket engine, combustion vibrations are encountered in the low end of the operating conditions. We used a lateral baffle to satisfactorily solve the problem. This paper mainly introduces the experimental results and qualitative analysis. The approach is novel. It can be used as a reference. (Keywords: rocket engines)


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    Titel :

    Approach of Preventing Combustion Vibrations of Rocket Engine with Lateral Baffle


    Beteiligte:
    D. Lianshun (Autor:in) / X. Fuyuan (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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