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    Titel :

    Influence of Boundary Layer Transition on the Trajectory Optimisation of a Reusable Launch Vehicle (AIAA 2014-2362)



    Kongress:

    19th, AIAA international space planes and hypersonic systems and technologies conference ; 2014 ; Atlanta, GA



    Erscheinungsdatum :

    2014-01-01


    Format / Umfang :

    22 pages


    Anmerkungen:

    Includes bibliographical references and author index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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