Aerodynamic Shape Design and Validation of an Advanced High-Lift Device for a Regional Aircraft with Morphing Droop Nose

Table 1

Flight conditions considered for NLF wing design.

	Mach number	Altitude (ft)	Reynolds (10^6)	(wing + body)
Cruise (1)	0.52	20 000	17.33	0.50
Climb (2)	0.45	20 000	15.00	0.67
Low speed (3)	0.197	0	11.80