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    Title :

    Numerical investigation of two-dimensional supersonic variable-geometry inlet for ramjet


    Contributors:
    Pu, Yongbin (author) / Huang, Guoping (author) / Fengyuan, Zuo (author) / Xia, Chen (author)

    Conference:

    21st AIAA International Space Planes and Hypersonics Technologies Conference



    Publication date :

    2017-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Numerical Investigation of Two-dimensional Supersonic Variable-geometry Inlet for Ramjet (AIAA 2017-2415)

    Pu, Yongbin / Huang, Guoping / Fengyuan, Zuo et al. | British Library Conference Proceedings | 2017



    Inlet efficiency parameters for supersonic combustion ramjet engines

    Curran, E. T. / Bergsten, M. Brian | TIBKAT | 1964


    Investigation of Two-Mode Ramjet/Scramjet Inlet

    Falempin, F. / Montazel, X. / Goldfeld, M. et al. | British Library Conference Proceedings | 1999


    Development of a Supersonic Inlet Capability for Integral Rocket Ramjet Applications

    Stockenstroem, A. / Morelli, M. / International Society for Air Breathing Engines; Australian Committee | British Library Conference Proceedings | 1995