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    Title :

    Research Progress of Hypersonic Inlet Inverse Design Based on Curved Shock Compression System (AIAA 2015-3647)


    Contributors:

    Conference:

    AIAA international space planes and hypersonic systems and technologies conference



    Publication date :

    2015-01-01


    Size :

    14 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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