Pointed wing of aspect ratio 4 was modified by clipping small portions off wing tips to form wings with aspect ratios of 3.50, 3.25, and 3.00; first one was extensively tested as complete model with various horizontal-and vertical-tail combinations.


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    Title :

    Static longitudinal characteristics at high subsonic speeds of complete airplane model with highly tapered wing having 0.80 chord line unswept and with several tail configurations


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    57 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :