Shortcoming of conventional method of calculating lift distribution and stability; comparison of gliding and power flight; attempt to eliminate errors in preliminary calculation by assumption of distribution of lift distribution; explanation of great differences found in flight with and without propeller slipstream.


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    Title :

    Lift distribution and longitudinal stability of an airplane


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Memo


    Contributors:
    Topfer, C. (author)


    Publication date :

    1931


    Size :

    7 pages


    Remarks:

    4 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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