Aerodynamic Optimization of an Over-the-Wing-Nacelle-Mount Configuration

Table 2

Range of design parameters for PARSEC airfoil and twist Angles.

Parameter	Min	Max
𝑟le	0.005	0.06
𝑍Te	−0.015	0.015
𝛼Te	−8 deg.	−3 deg.
𝑋up	0.35	0.50
𝑍up	0.06	0.13
𝑍xxup	−1.0	−0.2
𝑋lo	0.35	0.5
𝑍lo	−0.13	−0.06
𝑍xxlo	0.1	1.0
Washout at tip	−4 deg.	4 deg.
Washout at kink	−4 deg.	4 deg.
Incidence angle (root)	0 deg.	8 deg.