Mar. 9 no. 10 pp 266-269: Longitudinal stability and controllability. Mar. 16 no. 11 pp. 296-297: Tailplane and elevator. Mar. 23 no. 12 pp. 320-322: Summary of longitudinal stability. Appendices giving method of calculation and sample calculations in nos. 13, 14, 15, and 16, Mar. 30, Apr. 6, 13, and 20, 1925, pp. 347-348, 380-381, 411-412, and 436-438, 3 figs, and continuation of article in nos. 17, 18, 19, 20, and 21, Apr. 27, May 4, 11, 18, and 25, 1925, pp. 462-463, 488-490, 521-522, 545-546, and 574-575, 16 figs. Apr. 27: Elements of lateral stability. May 4: Effect of various wing arrangements. May 11: Effect of combined roll and yaw. May 18: Actual airplanes and the tail spin. May 25: Stability in roll and yaw.


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    Title :

    Stability and controllability of airplanes


    Additional title:

    Aviation


    Contributors:

    Published in:

    Aviation ; 18 , n 10-21


    Publication date :

    1925


    Remarks:

    6 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




    Controllability and maneuverability of airplanes

    Norton, F.H. / Brown, W.G. | Engineering Index Backfile | 1922


    Controllability and maneuverability of airplanes

    Norton, F. H. / Brown, W. G. | TIBKAT | 1921


    Controllability and Maneuverability of Airplanes

    Norton, F H / Brown, W G | NTRS | 1923