Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Leading Edge Bluntness Effects on Shock Wave/Boundary Layer Interactions Near a Convex Corner (AIAA 2015-3601)


    Contributors:
    Li, Zhufei (author) / Yang, Jiming (author)

    Conference:

    AIAA international space planes and hypersonic systems and technologies conference



    Publication date :

    2015-01-01


    Size :

    16 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English