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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Approach of Preventing Combustion Vibrations of Rocket Engine with Lateral Baffle


    Contributors:
    D. Lianshun (author) / X. Fuyuan (author)

    Publication date :

    1987


    Size :

    26 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Control Effects of Baffle on Combustion Instability in a LOX/GH2 Rocket Engine

    Feng, Songjiang / Nie, Wansheng / He, Bo et al. | AIAA | 2010



    Cooled Baffle Development for M-1 Engine Using a Subscale Rocket Engine

    E. W. Conrad / J. K. Curley / J. P. Wanhainen | NTIS | 1966



    Flow Induced Vibrations in a Rocket Engine Manifold

    Peugeot, John / Frendi, Abdelkader | AIAA | 2012