Low scale wing tunnel investigation conducted in both straight and yawing flow; curved flow equipment of Langley stability tunnel used for tests.


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    Title :

    Investigation at low speeds of effect of aspect ratio and sweep on static and yawing stability derivatives of untapered wings


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Goodman, A. (author) / Brewer, J.D. (author)


    Publication date :

    1948


    Size :

    34 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :