Data show that CLmax may vary by as much as 14% depending on altitude and wing loading at which tests are made, position or motion of propeller, and rate at which angle of attack is changing when maximum lift coefficient is obtained.


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    Title :

    Flight tests of airplane showing dependence of maximum lift coefficient on test conditions


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Soule, H.A. (author) / Hootman, J.A. (author)


    Publication date :

    1937


    Size :

    12 pages


    Remarks:

    3 Supp plates, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :