Investigation conducted in Langley 4 by 4-ft supersonic pressure tunnel to study effect of surface roughness on skin friction and temperature recovery factor of ogive cylinder body of revolution.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Investigation of distributed surface roughness on body of revolution at Mach number of 1.61


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1954


    Size :

    35 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :