A Piper Cub aircraft configuration has been analyzed using the VSAERO code and the aerodynamic characteristics have been obtained at two incidences. Detailed pressure distributions have been computed along wing-body-tail sections. A comparison of lift characteristics with flight data shows reasonable agreement.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    VSAERO Analysis of a Piper Cub Aircraft


    Contributors:
    A. Srivastava (author) / D. Lednicer (author) / I. Gilchrist (author) / J. Saghafi (author)

    Publication date :

    1993


    Size :

    6 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    A VSAERO Analysis of Several Canard Configured Aircraft

    Lednicer, David | SAE Technical Papers | 1988


    A VSAERO Analysis of Several Canard Configured Aircraft - Part 2

    Lednicer, David | SAE Technical Papers | 1989


    Application of VSAERO to internal flows

    NATHMAN, JAMES / FRANK, JOEL | AIAA | 1987



    A VSAERO Method Computation on Half-Model Slat-Flap Configuration

    Djatmiko, B. / Sudira, I. G. N. / Layukallo, T. et al. | British Library Conference Proceedings | 1994