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    Title :

    Variable Mach Number Design Methodology for the Wide-Speed Range Waverider Generated from Axisymmetric Supersonic Flows (AIAA 2017-2439)


    Contributors:
    Li, Shibin (author) / Huang, Wei (author) / Wang, Zhenguo (author) / Zhang, Tiantian (author) / Yan, Li (author)

    Conference:

    AIAA Interantional Space Planes and Hypersonic Systems and Technologies (Conference)



    Publication date :

    2017-01-01


    Size :

    10 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    Shapeable Hypersonic Waverider Entry Vehicles (AIAA 2017-4880)

    Maxwell, Jesse R. | British Library Conference Proceedings | 2017


    Nr. 2439

    DataCite | 1892


    SUPERSONIC COMBUSTION OF HYDROGEN IN MACH 2 FLOWS OVER AN AXISYMMETRIC MODEL (AIAA 2018-5252)

    Zhao, Mengmeng / Buttsworth, David / Choudhury, Rishabh | British Library Conference Proceedings | 2018