Analysis of results obtained in systematic research program concerned with effects of wing sweep, aspect ratio, taper ratio, and dihedral on rolling moment due to sideslip of wing-fuselage configurations up to Mach numbers of about 0.95; new methods and design charts for estimating effects of compressibility and wing geometry on rolling moment due to sideslip.


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    Title :

    Rolling moment due to sideslip of swept wings at subsonic and transonic speeds


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    81 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :