The procedure for wing aerodynamic design based on the algorithm of simultaneous multiregime optimization of cruise and low-speed performance is considered. The method is based on the combination of fast direct methods for subsonic and transonic wing analysis, geometry variation module and the optimization procedure. The description of all the components and examples of practical application of the developed technique for design of the conventional medium-haul airplane wing and the ‘Flying Wing’ configuration are presented.


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    Title :

    Multi-objective optimization procedure for the wing design at cruise and low-speed conditions


    Contributors:


    Publication date :

    2013-02-01


    Size :

    12 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown





    MULTIOBJECTIVE OPTIMIZATION PROCEDURE FOR THE WING DESIGN AT CRUISE AND LOW-SPEED CONDITIONS

    Gubanova, M.A. / International Council of the Aeronautical Sciences; Optimage Ltd | British Library Conference Proceedings | 2010


    Multiobjective Optimization Procedure for the Wing Cruise and High-Lift Aerodynamic Characteristics Matching

    Gubanova, M. / Bolsunovsky, A. / Buzoverya, N. | British Library Conference Proceedings | 2007