Oblique wing aeroelasticity studies are reviewed. The static aeroelastic stability characteristics of oblique wing aircraft, lateral trim requirements for 1-g flight, and the dynamic aeroelastic stability behavior of oblique winged aircraft, primarily flutter, are among the topics studied. The similarities and differences between oblique winged aircraft and conventional, bilaterally symmetric, swept wing aircraft are emphasized.


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    Title :

    An investigation of aeroelastic phenomena associated with an oblique winged aircraft


    Contributors:

    Publication date :

    1976-08-31


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :




    Aeroelastic Control of Oblique-Wing Aircraft

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


    Aeroelastic control of oblique-wing aircraft

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