An automated transonic design code has been developed which modifies an initial airfoil or wing in order to generate a specified pressure distribution. The design method uses an iterative approach that alternates between a potential-flow analysis and a design algorithm that relates changes in surface pressure to changes in geometry. The analysis code solves an extended small-disturbance potential-flow equation and can model a fuselage, pylons, nacelles, and a winglet in addition to the wing. A two-dimensional option is available for airfoil analysis and design. Several two- and three-dimensional test cases illustrate the capabilities of the design code.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    A transonic-small-disturbance wing design methodology


    Beteiligte:

    Erscheinungsdatum :

    01.03.1988


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Transonic-Small-Disturbance Wing Design Methodology

    P. S. Phillips / E. G. Waggoner / R. L. Campbell | NTIS | 1988




    Coupling of a Wing Inverse Design Code to a Transonic Small Disturbance Flow Solver

    Jones, D. / Fejtek, I. / Leblond, D. et al. | British Library Conference Proceedings | 2001


    Wing flutter calculations with the CAP-TSD unsteady transonic small disturbance program

    Bennett, Robert M. / Batina, John T. / Cunningham, Herbert J. | NTRS | 1988