Question: Write Matlab code solving the Monoplane equation given the variables - Angle of attack at root - Angle of zero lift - Taper Ratio -

Write Matlab code solving the Monoplane equation given the variables

- Angle of attack at root

- Angle of zero lift

- Taper Ratio

- Aspect Ratio

- Washout

- Number of terms in the fourier series for circulation distribution

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