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  • IAC-15/C4/9
  • Paper #27866
  • Paper information

    Paper code

    IAC-15,C4,9,3,x27866

    Order

    3

    Room

    Ballroom B (Crowne Plaza Hotel, -1 floor)

    Title

    effects of primary rocket nozzle expansion ratio on combustion oscillating characteristics in a rbcc engine combustor

    abstract

    View PDF

    Session

    9. Hypersonic and Combined Cycle Propulsion

    symposium

    C4. SPACE PROPULSION SYMPOSIUM

    congress

    IAC-15

    Type of presentation

    oral

    Main author

    Prof. Guoqiang He, Northwestern Polytechnical University, China

    Co-authors

    Mr. Zhiwei Huang, Northwestern Polytechnical University,NPU, China;

    Dr. Fei Qin, China;

    Mr. Ya Jun Wang, College of Astronautics, Northwestern Polytechnical University, China;

    Mr. Xianggeng Wei, Northwestern Polytechnical University, China;