A method has been developed for designing airfoils and wings at transonic speeds. It utilizes a hybrid design algorithm in an iterative predictor/corrector approach, alternating between an analysis code and a design module. This method has been successfully applied to a variety of airfoil and wing design problems, including both transport and highly-swept fighter wing configurations. An efficient approach to viscous airfoil design and the effect of including static aeroelastic deflections in the wing design process are also illustrated.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Design of Transonic Airfoils and Wings Using a Hybrid Design Algorithm


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Aerospace Technology Conference and Exposition ; 1987



    Publication date :

    1987-10-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Design of transonic airfoils and wings using a hybrid design algorithm

    Campbell, Richard L. / Smith, Leigh A. | NTRS | 1987


    Transonic Airfoils and Wings Design Using Inverse and Direct Methods

    Zhang, Mengmeng / Rizzi, Arthur W. / Nangia, R K. | AIAA | 2015


    Hybrid Feedback Design for Subsonic and Transonic Airfoils and Wings (AIAA 2014-0414)

    Zhang, M. / Wang, C. / Rizzi, A.W. et al. | British Library Conference Proceedings | 2014


    Transonic flow theory of airfoils and wings

    Garabedian, P. R. | NTRS | 1976


    Airfoils and Wings in Transonic Ground Effect

    Doig, Graham / Barber, Tracie / Leonardi, Eddie et al. | AIAA | 2008