4.2.2 Aerodynamic sensitivity definition
All maps’ points are percentual variations with respect to the aerodynamic datum point (shown in par.4.2.1).
So, if the datum point is:
= 100%
= 100%
= 40%
A variation of (e.g.) -15% of all the coefficients will bring to:
= 100% * (100%-15%) = 85%
= 100% * (100%-15%) = 85%
= 40% * (100%-15%) = 34%
4.3 FRONT WING SETTING
Front flap angle is adjustable with shims:
• 16 14 04 035 FW adjuster 3°
• 16 14 04 015 FW adjuster 5°
• 16 14 04 032 FW adjuster 7°
On the Front Wing it is allowed the use of the homologated gurney flaps:
• 16 14 04 023 (LH side)
• 16 14 04 024 (RH side)
4.4 REAR WING SETTING
Rear wing angle in the following tables is the angle between the tangent on the upper side of the rear wing
(without gurney flap) and the reference plane:
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