26. The surface of many airfoils can be described with an equation of the form where t...
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26. The surface of many airfoils can be described with an equation of the form where t is the maximum thickness as a fraction of the chord length c (e.g.,
). Given that m and m, the following values for y have been measured for a particular airfoil:
Determine the constants , and . (Write a system of five equations and five unknowns, and use MATLAB to solve the equations.)
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