Investigation to determine wing surface pressures and aerodynamic loading associated with deflection of flap; data are presented for flap angles to 16° at Mach of 0.60 to 0.90 with R of 3.2 million and at Mach of 0.25 with R of 15.0 million.


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    Title :

    Effects of inverse-taper leading-edge flap on aerodynamic loading characteristics of 45° sweptback wing at Mach numbers to 0.90


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1959


    Size :

    108 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :