AERODYNAM$$C ; FOR NACA $8414$ THE FOLLOWING QUESTIONS WILL BE ANSWERED IN THE ANSYS PROGRAM.PLEASE SEND $$MAGE FORMAT

What to Include in Homework

$1.$ Mesh image.

$2.$ The x$-$y graph containing the lift and drag values $$for each angle we solved $($in the solutions, increase the alpha angle to a suitable value $($e$.$g$.4$ o$)$ degrees and continue until it shows Cl max or post$-$stall values$)$

$3.$ Velocity contours around the wing must be created for all angles. $($Do not forget to equalize the speed scale on the edge of the contour for each angle.$)$

$4.$ Draw Cp graphs for each angle from the X$-$Y plot section.

$5.$ Comment on the relationship between the differences in Cl and Cd values $$at the studied angles and the flow field.