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Old   September 18, 2004, 07:20
Default A Problem about NURBS
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i want to represent airfoil using NURBS(nonuniform rational B spines).But i have a problem.How can i konw the control points for this curve if i have known the points in pressure and suction side.For example,there 100 points in every side and i want to using eight control point to represent it!
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