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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Aeroelastic stability characteristics of an oblique wing aircraft


    Contributors:

    Conference:

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


    Publication date :

    1977-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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


    Aeroelastic Control of Oblique-Wing Aircraft

    J. J. Burken / G. S. Alag / G. B. Gilyard | NTIS | 1986