Investigation made in Langley stability tunnel; all wings had aspect ratios of 2.61 and had NACA 0012 airfoil sections normal to quarter-chord lines; taper ratios of 1.00, 0.50, and 0.25 investigated; experimental results compared with available theory.


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    Title :

    Effect of taper ratio on low-speed static and yawing stability derivatives of 45° sweptback wings with aspect ratio of 2.61


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Letko, W. (author) / Cowan, J.W. (author)


    Publication date :

    1948


    Size :

    20 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :