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    Titel :

    Computational Fluid Dynamics Study of Optimized Hypersonic Leading Edge Geometries (AIAA 2015-3509)


    Beteiligte:

    Kongress:

    AIAA international space planes and hypersonic systems and technologies conference



    Erscheinungsdatum :

    2015-01-01


    Format / Umfang :

    13 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



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    Nr. 3509

    DataCite | 1912


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