Table 1 Aerodynamic impact of flaps... | Emerald Publishing

Table 1

Aerodynamic impact of flaps deflection on the lift coefficient

Derivative name	Symbol	Value
Front wing lift increment versus front flap deflection	$\frac{\partial C_{L, F}}{\partial δ_{F}}$	0.875 [1/rad]
Rear wing lift increment versus front flap deflection	$\frac{\partial C_{L, R}}{\partial δ_{F}}$	−0.375 [1/rad]
Front wing lift increment versus rear flap deflection	$\frac{\partial C_{L, R}}{\partial δ_{F}}$	0.047 [1/rad]
Rear wing lift increment versus rear flap deflection	$\frac{\partial C_{L, R}}{\partial δ_{R}}$	0.838 [1/rad]

Derivative name	Symbol	Value
Front wing lift increment versus front flap deflection	$\frac{\partial C_{L, F}}{\partial δ_{F}}$	0.875 [1/rad]
Rear wing lift increment versus front flap deflection	$\frac{\partial C_{L, R}}{\partial δ_{F}}$	−0.375 [1/rad]
Front wing lift increment versus rear flap deflection	$\frac{\partial C_{L, R}}{\partial δ_{F}}$	0.047 [1/rad]
Rear wing lift increment versus rear flap deflection	$\frac{\partial C_{L, R}}{\partial δ_{R}}$	0.838 [1/rad]