Mathematical investigation of factors controlling stability in nose-steered or tail-first airplane by means of simplified formulas for moment coefficient of wing; slope of moment line of wing; moment coefficient of horizontal empennage; including area, chord and angle of attack of wing. From Zeit. fuer Flugtechnik und Motorluftschiffahrt, Dec. 15, 1930, indexed in Engineering Index 1930, p. 67.


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    Title :

    Static longitudinal stability of "Ente" airplanes


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Memorandum


    Contributors:
    Kiel, H.G. (author)


    Publication date :

    1930


    Size :

    27 pages


    Remarks:

    21 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Static longitudinal stability of "Ente" airplanes

    Kiel, Heinrich Georg | NTRS | 1931


    Static longitudinal stability of "Ente" airplanes

    Kiel, Heinrich Georg | TIBKAT | 1931


    Longitudinal stability of airplanes

    Ko¨ / nig, Georg. | Engineering Index Backfile | 1923


    Equalization of moments and static longitudinal stability of airplanes

    Mueller, H. | Engineering Index Backfile | 1929


    Statical longitudinal stability of airplanes

    Warner, Edward P. | Engineering Index Backfile | 1920