A method for constructing an airfoil using a specified chord velocity diagram |
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| Authors: | R B Salimov A G Labutkin |
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| Institution: | 1.Kazan State University of Architecture and Building Construction,Kazan,Russia |
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| Abstract: | A problem of determining a shape of the airfoil being streamlined by a potential incompressible inviscid flow is solved by
the successive approximation method using a specified chord velocity diagram. It is shown that a closed airfoil that possesses
a specified chord velocity diagram can be constructed with a sufficient accuracy; if the chord diagram is unsuccessfully specified,
the closed airfoil may prove to be not univalent, that is, physically unrealizable. |
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