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15: Folder 2D and Display of Curves

This chapter covers the output of the computed curves. The graphics window top left shows the wing, which is actually under construction. The wing is displayed as a flat 2D-object, so that a possible dihedral is not visible.




15.1: Display current Wings
15.2: Display CP, CG and NP
15.3: Display Strength of Circulation (Gamma)
15.4: Display Distribution of Cl
15.5: Display Distribution of Cdi
15.6: Display Distribution of ai
15.7: Display Distribution of Reynolds Number
15.8: Airfoil Cross-Section
15.9: Display Contour of whole Airplane
15.10: Output of Flap Angle
15.11: Positioning the Marking-bar

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