Formula for computing loads that come upon machine as a whole under various conditions of flight. Equations of equilibrium when flying and when alighting with engine shut off; approximate method of calculating loads when turning in horizontal position and when flattening out from vertical dive and looping. How flattening out of flight path is brought about. Loads caused by gusts, spiral glides and spinning. Distribution of load over the planes. Pressure distribution in spiral guide. (See also - vol. 16, nos. 289 and 291, 293, 294, 295, 296 and 297, May 1, 15, 29, June 5, 12, 19 and 26, 1919, pp. 556-559, 589-592, 619-622, 644-647 and 671-673, 32 figs)


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    Title :

    The loads and stresses on aeroplanes


    Additional title:

    Aeronautics


    Contributors:
    Case, John (author)

    Published in:

    Aeronautics ; 17 , n 300


    Publication date :

    1919


    Size :

    3 pages


    Remarks:

    4 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    The loads and stresses on aeroplanes

    Case, John | Engineering Index Backfile | 1920


    The loads and stresses in aeroplanes

    Case, John | Engineering Index Backfile | 1921


    Calculation of stresses in aeroplanes

    Slocum, S.E. | Engineering Index Backfile | 1918


    Loads and calculations of army aeroplanes

    Stelmachowski, Ing. | Engineering Index Backfile | 1921


    Aeroplanes

    Renaud, Paul | Engineering Index Backfile | 1911