Table 2 Aerodynamic impact of flaps... | Emerald Publishing

Table 2

Aerodynamic impact of flaps deflection on the pitching moment coefficient

Derivative name	Symbol	Value
Front wing pitching moment increment versus front flap deflection	$\frac{\partial C_{M, F}}{\partial δ_{F}}$	0.565 [1/rad]
Rear wing pitching moment increment versus front flap deflection	$\frac{\partial C_{M, R}}{\partial δ_{F}}$	0.274 [1/rad]
Front wing pitching moment increment versus front flap deflection	$\frac{\partial C_{M, R}}{\partial δ_{F}}$	0.033 [1/rad]
Rear wing pitching moment increment versus rear flap deflection	$\frac{\partial C_{M, R}}{\partial δ_{R}}$	−0.692 [1/rad]

Derivative name	Symbol	Value
Front wing pitching moment increment versus front flap deflection	$\frac{\partial C_{M, F}}{\partial δ_{F}}$	0.565 [1/rad]
Rear wing pitching moment increment versus front flap deflection	$\frac{\partial C_{M, R}}{\partial δ_{F}}$	0.274 [1/rad]
Front wing pitching moment increment versus front flap deflection	$\frac{\partial C_{M, R}}{\partial δ_{F}}$	0.033 [1/rad]
Rear wing pitching moment increment versus rear flap deflection	$\frac{\partial C_{M, R}}{\partial δ_{R}}$	−0.692 [1/rad]