Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Shock tunnel investigation of boundary-layer transition at M equals 5.5.


    Author / Creator :

    RUSHTON, G. H. /AVCO CORP., AEROPHYSICS DEPT., WILMINGTON, MASS./., STETSON, K. F.


    Contributors:

    Published in:

    AIAA Journal ; 5 , 5 ; 899-906


    Publication date :

    1967-01-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English