• Discuss the effects of the flaps on wing parameters such as:

lift curve slope, angle of attack for zero lift coefficient,

pitching moment coefficient, drag coefficient, maximum

lift coefficient, angle of attack of maximum lift coefficient,

etc.

• Discuss how theory (XFOIL) compares (cant compare

directly, Xfoil is 2D, your data is 3D - but can compare

trends).

• Perhaps also tabulate the results for easy comparison. Show

me you understand the results.

•Be focused and to the point. DISCUSS TRENDS.