Recently, a singular integral method was developed for solving two-dimensional compressible potential flows. The original formulation limited the applicability to single bodies in a uniform freestream. Currently, modifications are being made so that the flow field around multiple bodies can also be calculated. Because of the unique manner in which the integral equations are formulated, they are especially well-suited for analysis and inverse design calculations of a row of similar airfoils. A brief description of the formulation is given in this paper and some preliminary results are included.

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