A computer program for aircraft synthesis using a numerical optimizer was developed to study the application of the joined-wing configuration to transport aircraft. The structural design algorithm included the effects of secondary bending moments to investigate the possibility of tail buckling and to design joined wings resistant to buckling. The structural weight computed using this method was combined with a statistically-based method to obtain realistic estimates of total lifting surface weight and aircraft empty weight. A variety of 'optimum' joined-wing and conventional aircraft designs were compared on the basis of direct operating cost, gross weight, and cruise drag. The most promising joined-wing designs were found to have a joint location at about 70 percent of the wing semispan. The optimum joined-wing transport is shown to save 1.7 percent in direct operating cost and 11 percent in drag for a 2000 nautical mile transport mission.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design synthesis and optimization of joined-wing transports


    Beteiligte:
    Gallman, John W. (Autor:in) / Smith, Stephen C. (Autor:in) / Kroo, Ilan M. (Autor:in)

    Erscheinungsdatum :

    01.09.1990


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Design synthesis and optimization of joined-wing transports

    GALLMAN, JOHN / SMITH, STEPHEN / KROO, ILAN | AIAA | 1990


    Structural Optimization for Joined-Wing Synthesis

    Gallman, J.W. | Online Contents | 1996


    Structural optimization for joined-wing synthesis

    Gallman, John W. / Kroo, Ilan M. | AIAA | 1996


    Structural optimization for joined-wing synthesis

    GALLMAN, JOHN / KROO, ILAN | AIAA | 1992


    Preliminary design optimization of joined-wing aircraft

    Gallman, John W. / Kroo, Ilan M. / Smith, Stephen C. | NTRS | 1990