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    Title :

    Design of a Mach-6 Quiet-flow Wind-Tunnel Nozzle Using thee^*^*N Method for Transition Estimation


    Contributors:

    Conference:

    36th, Aerospace sciences meeting ; 1998 ; Reno; NV



    Publication date :

    1998-01-01


    Size :

    ALL


    Remarks:

    Nos AIAA 98-0001 to 98-1069 with gaps held only


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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