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    Title :

    AIAA-2005-1110 EXPERIMENTAL INVESTIGATION OF A THREE-DIMENSIONAL SCRAMJET INLET TESTED IN HIGH ENTHALPY IMPULSE WIND TUNNEL AT MACH 6



    Conference:

    17th, International symposium on air breathing engines ; 2005 ; Munich, Germany



    Publication date :

    2005-01-01


    Size :

    87 pages


    Remarks:

    Includes bibliographical references and index; Papers on CD-ROM



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English






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