Term aeroelasticity covers phenomena in which three types of forces are acting on airframe, influencing its behavior; they are aerodynamic, inertia, and elastic forces; problems of static aeroelasticity and philosophy of solution employed; mathematical relations, structural, and aerodynamic simulation are discussed; details of computer design which incorporates control console, static elastic section, and aerodynamic section; results of symmetrical static aeroelastic analysis obtained from computer are presented.


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    Titel :

    Solution of static aeroelastic problems by means of direct analog computer


    Weitere Titelangaben:

    AIAA -- Simulation Aerospace Flight Conference -- Tech Papers


    Beteiligte:
    Dixon, W.J. (Autor:in)

    Kongress:

    AIAA Meeting -- Simulation for Aerospace Flight Conference ; 1963 Stability



    Erscheinungsdatum :

    1963


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Integrated solution for computational static aeroelastic problems

    Karpel, Mordechay / Yaniv, Sara / Livshits, David | AIAA | 1996


    Integrated Solution for Conceptual Static Aeroelastic Problems

    Karpel, M. / Yaniv, S. / Livshits, D. et al. | British Library Conference Proceedings | 1996


    Static aeroelastic program

    Roskam, J. | NTRS | 1975


    Static Aeroelastic Considerations

    Lomax, Ted L. | AIAA | 1996