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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    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


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Buglia, J.J. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :