IN the two-dimensional case the configuration shows a wake which forms a discontinuity in the flow, being bounded by contact vortices δγi1 and δγi2 which have as resultant a vortex δγi (FIG. 12). For there to be lift: δγi2<0, δγi1>0, δγi<0. There corresponds to each vortex δγi a vortex on the aerofoil δΓi of the same sign, and in addition a vortex Γ corresponding to the free stream potential, without jet.


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    Title :

    Establishment of Lift on an Aerofoil with a Jet Flap


    Subtitle :

    A Theoretical Note Relating to a Wing with Trailing Edge Jet with Extension to Cover Wings of Finite Span


    Contributors:
    Hirsch, R. (author)


    Publication date :

    1958-01-01


    Size :

    9 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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