To outline a transonic wing design problem by applying real coded genetic algorithm (GA) and dynamic mesh technique to reduce the optimization time and cost.

    Design/methodology/approach

    Dynamic mesh technique was used in the design of a transonic wing by matching it with heuristic algorithms.

    Findings

    It is observed that the drag coefficient can be reduced by 25 percent. While this has been done, the lift coefficient is tried to be close to the design value determined at the beginning as a design constraint.

    Originality/value

    It is the first time that the dynamic mesh technique is used for regenerating the mesh structures of the new population members in the GA.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Dynamic mesh and heuristic algorithms for the design of a transonic wing


    Contributors:


    Publication date :

    2006-01-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English