Nose of model had surface roughness of 2 to 5 μin. as measured with interferometer; comparison with results from rougher models indicated that high degree of polish was instrumental in delaying transition from laminar to turbulent flow.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Heat transfer and boundary-layer transition on highly polished hemisphere-cone in free flight at mach numbers up to 3.14 and Reynolds numbers up to 24×106


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    26 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :