Abstract
An algorithm has been developed which treats transonic flow over jet-flapped wings of general plan form within a small disturbance framework. The numerical method represents a generalization of the relaxation solutions developed by Bailey and Ballhaus for unblown wings and the authors' previous work for twodimensional jet-flapped airfoils, and it incorporates a new far field which accounts for the vorticity on the jet. Supercritical results presented for a variety of blown planforms indicate repeal of the Kutta condition, as in two dimensions, appreciable spanwise load carryover for partial span blowing, and reduction in lift augmentation due to sweepback. Comparison of lift coefficients with experimental values shows good agreement for various planforms.
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