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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

8.15: Generating an elliptic Wing

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