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    Title :

    Research on Dynamic Derivatives Test Technique for Integrative Hypersonic Vehicle with Internal and External Flow in Wind Tunnel (AIAA 2017-2334)


    Contributors:

    Conference:

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



    Publication date :

    2017-01-01


    Size :

    7 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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