Abstract
T authors appreciate the interest shown in their work by Prof. Squire. We had, in fact, already tried his suggestion of recasting the expression for i/^ (an unnumbered equation on p. 245 of Ref. 1) into an equivalent form. Figure 1 shows the result of making the suggested change in the expression for \I/ij for an airfoil-type axisymmetric body of fineness ratio = 2.91. The figure shows that the exact solution and the solution obtained by linearly varying axial singularities are essentially the same. The results computed by the expression
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