• 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.