An analysis of the lift augmentation due to a thin jet of air issuing from a slot along the leading edge of a delta wing is presented. The problem is treated with an extension of the method of Brown and Michael, representing the separated flow on the lee side of the wing by a pair of concentrated vortices and corresponding feeding sheets. It is assumed that the jet is not affected by Coanda forces. The analysis produces qualitative agreement with experiments.


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    Title :

    The lift of sharp-leading-edged delta wings with blowing


    Contributors:

    Publication date :

    1985-12-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :



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