The advantages of oblique wings have been the subject of numerous theoretical studies, wind tunnel tests, low speed flight models, and finally a low speed manned demonstrator, the AD-1. The specific objectives of the OWRA program are: (1) to establish the necessary technology base required to translate theoretical and experimental results into practical mission oriented designs; (2) to design, fabricate and flight test an oblique wing aircraft throughout a realistic flight envelope, and (3) to develop and validate design and analysis tools for asymmetric aircraft configurations. The preliminary design phase of the project is complete and has resulted in a wing configuration for which construction is ready to be initiated.


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    Titel :

    The oblique-wing research aircraft: A test bed for unsteady aerodynamic and aeroelastic research


    Beteiligte:


    Erscheinungsdatum :

    01.02.1989


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    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


    Aeroelastic control of oblique-wing aircraft

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


    Aeroelastic stability characteristics of an oblique wing aircraft

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