In theory, the most efficient wing shape for transonic and low supersonic speeds is simply a long narrow straight subsonic wing turned at an oblique angle to the flight direction. This theory has been verified by tests at Mach numbers from .6 to 1.4 in supersonic wind tunnel and by comparative studies of transonic transport designs.


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    Titel :

    Aeroelastic characteristics of an oblique wing


    Beteiligte:
    Jones, R. T. (Autor:in) / Nisbet, J. W. (Autor:in)


    Erscheinungsdatum :

    01.02.1976


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aeroelastic stability characteristics of an oblique wing aircraft

    Crittenden, J. B. / Weisshaar, T. A. / Johnson, E. H. et al. | NTRS | 1977


    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

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