1549312215-Complex_Analysis_for_Mathematics_and_Engineering_5th_edition__Mathews

11 .8 • THE .JOUKOWSKJ AIRFOIL

y

Aoww1 · 111 circulanon. a=I

x

Aoww· 1 111 circulatton. a = 2.2
·na- 2 ·a
Flow wilh circulauo -. t circle w1 'th circulat1on ·
Figure 11 .65 Flows past t he uni

y

Figure 11 .66 Flow w1 'th circulat1on. around C,.

x

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