Results of investigation by Hoff, Hopf, and writer. Describes method of calculation without any assumption in regard to variation of engine power with altitude and only with assumption that this relation is, in fact, empirically known from measurements taken in altitude tests. Translated from Technische Berichte, vol. 3, no. 7, pp. 267-274.


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    Title :

    Curvilinear flight of airplanes


    Additional title:

    U. S. Nat. Advisory Comm. Aeronautics -- Tech. Notes


    Contributors:


    Publication date :

    1924


    Size :

    21 pages


    Remarks:

    6 Figs. on supp. pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Curvilinear flight of airplanes

    Salkowski, E | NTRS | 1924



    Airplanes in horizontal curvilinear flight

    Kann, H. | Engineering Index Backfile | 1924


    Flight tests on airplanes

    Koppe, H. | Engineering Index Backfile | 1926


    Flight Tests on Airplanes

    Koppe, Heinrich | NTRS | 1926