In tests conducted in blowdown tunnel of Langley gas dynamics laboratory optical method was used to study effect; range of roughness Reynolds number and range of roughness height to boundary layer displacement thickness which moved transition less than 10% were found and were functions of turbulence level.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Experimental study at mach number of 3 of effect of turbulence level and sandpaper-type roughness on transition on flat plate


    Additional title:

    NASA -- Memo


    Contributors:
    Jones, R.A. (author)


    Publication date :

    1959


    Size :

    43 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :