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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    Titel :

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


    Weitere Titelangaben:

    Nat. Advisory Committee Aeronautics -- Reports


    Beteiligte:
    de France, S.J. (Autor:in) / Burgess, C.P. (Autor:in)


    Erscheinungsdatum :

    1929


    Format / Umfang :

    16 pages


    Anmerkungen:

    16 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    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