The transition process of boundary layers on a low-speed wind-tunnel contraction wall was experimentally investigated using flow visualizations and hot-wire/hot-film measurements. The process has several classifications depending on the Reynolds number.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Technical Report of National Aerospace Laboratory: Transition Process of Boundary Layers on a Low-Speed Wind-Tunnel Contraction Wall


    Contributors:
    A. Nishizawa (author) / T. Sobagaki (author) / S. Takagi (author) / N. Tokugawa (author) / I. Misu (author)

    Publication date :

    2003


    Size :

    28 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English