Program to obtain data on thick airfoils to be used for pressure-jet rotor system; hovering performance of rotor for tip Mach number from 0.27 to 0.76 and corresponding blade tip Reynolds number range; performance characteristics of thick airfoils may be seriously limited by stall starting at trailing edges of airfoils; hovering performance of rotor with vortex generator compared with smooth-blade rotor.


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    Titel :

    High-tip-speed static-thrust tests of rotor having NACA 63215 A018 airfoil sections with and without vortex generators installed


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Shivers, J.P. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    21 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :