Calculation results for 11 different finite span wings are presented. Calculations were made by a combination of a numerical solution of lifting line theory with a technique developed to evaluate nonlinear section lift data. Aerodynamic coefficients for these wings are compared to the research results of other authors and to experimental data. First Published Online: 14 Oct 2010


    Access

    Download


    Export, share and cite



    Title :

    Analysis of calculation results of lift and drag forces for several wings using nonlinear section data


    Contributors:


    Publication date :

    2005




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




    "Section Lift and Drag Measurements on Wings at Low Reynolds Number"

    Lamontagne, L. / Deslauriers, M. / Dumas, G. et al. | British Library Conference Proceedings | 1999


    On the lift and drag of wings

    Lee, J.G. | Engineering Index Backfile | 1931




    Lift and Drag Characteristics of Rotary and Flapping Wings

    Ellington, C. P. / Usherwood, J. R. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2002