8: Folder Wing / Input field Wing Root
In this context root means the middle of the wing (root airfoil). Main function
of this input field is creating new wings and their positioning relative to the
airplane's zero-point.
8.1: Creating a new Wing
8.2: Input Designation of
Wing
8.3: Positioning the Wing
8.4: Number of Panels X
8.5: Distribution of Panels
in X-direction
8.5.1: Optimization of
Airfoil Zero-Coefficients
8.5.2: Input Resolution
of Panels in Solid modelling
8.6: Input of Chord line
8.7: Input Mass of Wing
8.8: Input Angle of
Incident
8.9: Select Root-Airfoil
8.10: Select actual Wing
8.11: Copy a Wing
8.12: Import Flying Wing
FLG-File
8.13: Delete current Wing
8.14: Input Angle for
Geometric Twist