The paper presents a design methodology for supersonic wing Sections with hybrid laminar flow control. The approach is based on coupled Euler/ boundary layer flow simulation and linear stability analysis for transition prediction. The investigations show that combinations of simple pressure distribution shapes can be used to optimize airfoils for maximum extent of laminar flow and hence minimum friction drag.


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    Title :

    Laminar Design for Supersonic Civil Transport


    Contributors:
    A. Traore (author)

    Publication date :

    2001


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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