System of equations for forced vibrations of prismatic shells, contour of which is not deformed, taking into account deplanation of sections, on basis of variational method.


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    Title :

    Self-oscillations of prismatic shells of caisson type aircraft wing in supersonic air flow


    Additional title:

    Avtokolebaniya prizmaticheskikh obolochek tipa kessona kryla samoleta v sverkhzvukovom potoke vozdukha


    Contributors:

    Published in:

    Publication date :

    1961


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Russian


    Keywords :


    AIRCRAFT WING, AIRCRAFT WINGS CAISSON, CENTER WING, SPAR (VERSIONS)

    VISHNYAKOV IGOR NIKOLAEVICH / KAPLUN YAKOV BORISOVICH / SELIVANOV NIKOLAJ PAVLOVICH et al. | European Patent Office | 2019

    Free access

    Oblique-wing supersonic aircraft

    Jones, R. T. | NTRS | 1976


    Single Wing Supersonic Aircraft

    R. T. Jones | NTIS | 1973


    Single Wing Supersonic Aircraft

    R. T. Jones | NTIS | 1974


    CAISSON OF WING DETACHABLE PART

    GOMZIN ALEKSANDR VLADISLAVOVICH / LACHUGIN VLADISLAV ALEKSANDROVICH / SHALYGIN VADIM APOLLONOVICH et al. | European Patent Office | 2019

    Free access