The progress of two studies which apply nonlinear aerodynamics to supersonic wing design is reviewed. The first study employed a nonlinear potential flow code to design wings for high lift and low drag due to lift by employing a controlled leading-edge expansion in which the crossflow accelerates to supercritical conditions and decelerates through a weak shock. The second study utilized a modified linearized theory code to explore the concept of using 'attainable' leading-edge thrust as a guide for selecting a wing leading-edge shape (planform and radius) for maintaining attached flow and maximizing leading-edge thrust. Experimental and theoretical results obtained during the course of these two studies are discussed.


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    Titel :

    An overview of two nonlinear supersonic wing design studies


    Beteiligte:
    Miller, D. S. (Autor:in) / Pittman, J. L. (Autor:in) / Wood, R. M. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting ; 1983 ; Reno, NV


    Erscheinungsdatum :

    1983-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    An overview of two nonlinear supersonic wing design studies

    MILLER, D. / PITTMAN, J. / WOOD, R. | AIAA | 1983


    Supersonic-Wing Nonlinear Aerodynamics

    Carlson, H. W. / Mack, R. J. | NTRS | 1983



    Warp Design of a Supersonic Wing Using a Nonlinear Optimization Method

    Lei, Zhong / Makino, Yoshikazu / Yoshida, Kenji | AIAA | 2004


    Supersonic 'oblique all wing' airfoil design

    Butler, Matthew Elliott | DSpace@MIT | 1993

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