Mathematical method described; general problem of tail design; effects of flaps on factors involved; manner in which flaps change requirements upon which minimum horizontal tail area is based.


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    Title :

    Notes on calculation of minimum horizontal tail surface for airplanes equipped with wing flaps


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:
    Soule, H.A. (author)


    Publication date :

    1937


    Size :

    19 pages


    Remarks:

    6 Supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English