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