No. 325: Data on actual aerodynamic forces and resulting stresses and bending moments in hull of U.S.S. Los Angeles, during severe still-air maneuvers, and in straight flight during rough air; maximum stresses within limits provided in accepted practice; flight in rough air produced forces and stresses about twice as great as most severe still-air maneuvers; transverse aerodynamic forces on hull proper small and irregular; coefficients of tail-surface forces and hull bending moments.


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    Title :

    Speed and deceleration trials of U.S.S. Los Angeles


    Additional title:

    Nat. Advisory Committee Aeronautics -- Reports


    Contributors:


    Publication date :

    1929


    Size :

    16 pages


    Remarks:

    16 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Speed and deceleration trials of U.S.S. Los Angeles

    DeFrance, S. J. / Burgess, C. P. | TIBKAT | 1929


    Speed and deceleration trials of U.S.S. Los Angeles

    de France, S.J. / Burgess, C.P. | Engineering Index Backfile | 1929


    Flight tests on U.S.S. Los Angeles

    de France, S.J. | Engineering Index Backfile | 1929