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  • experimental study on rbcc with oxygen/kerosene firstly combustion

    Paper number

    IAC-13,C4,9,5,x16945

    Author

    Dr. Liang Tian, Beihang University, China

    Year

    2013

    Abstract
    Oxygen/kerosene were used as the firstly combustion propellants to text RBCC on Direct-connected. Rocket ejector with strut characteristic was adopted, and composite injection with strut and wall was used to the secondly combustion. Mass follow rate of rocket ejector, number of nozzle and injection methods were investigated. The results show that, the added fuel can be ignited by fuel-rich gas which was generated by oxygen/kerosene combustion; reasonable composite injection can enhance RBCC performance.
    Abstract document

    IAC-13,C4,9,5,x16945.brief.pdf

    Manuscript document

    IAC-13,C4,9,5,x16945.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.