Two different studies are presented involving a transport category aircraft with an oblique or asymmetrically swept wing. The first study concerns itself with the effect on flutter of changes in certain of the aircraft structural and inertial parameters. The second portion examines the subcritical damping characteristics of a flexible oblique wing aircraft. For this purpose, a recent version of the NASTRAN computer code is used. A comparison is made between the flutter speeds found using the traditional k analysis and the results found from computation of subcritical response using the p-k or 'British' flutter method.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aeroelastic stability characteristics of an oblique wing aircraft


    Beteiligte:
    Crittenden, J. B. (Autor:in) / Weisshaar, T. A. (Autor:in) / Johnson, E. H. (Autor:in) / Rutkowski, M. (Autor:in)

    Kongress:

    Conference on Structures, Structural Dynamics and Materials ; 1977 ; San Diego, CA, US


    Erscheinungsdatum :

    01.01.1977


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Aeroelastic Stability Characteristics of an Oblique-Wing Aircraft

    J. B. Crittenden / T. A. Weishaar / E. H. Johnson et al. | AIAA | 1978


    Aeroelastic stability characteristics of an oblique wing aircraft

    CRITTENDEN, J. / WEISSHAAR, T. / JOHNSON, E. et al. | AIAA | 1977



    Aeroelastic control of oblique-wing aircraft

    Burken, J. J. / Gilyard, G. B. / Alag, G. S. | NTRS | 1986


    Aeroelastic control of oblique-wing aircraft

    Burken, J. J. / Alag, G. S. / Gilyard, G. B. | NTRS | 1986