Report - Wing Design of SMR-2020
All outputs of the program 'wing_design' were created with version 3.0.0

Data

General parameters
parametersymbolunitvalue
Reference areaSrefm2122.02
Mean aero. chordMACm4.16
Spanbm35.45
Aspect ratioAR110.30
Taper ratioλ10.17
Section parameters
parametersymbolunitS00S01S02S03
Dimensionless half spanη10.000.110.301.00
Spanwise coordinateym0.001.985.3217.73
Chordcm6.126.124.091.04
Sweep leading edgeφLE°0.0033.5029.7329.73
Sweep quarter chordφ25°0.0027.0027.0027.00
Sweep Trailing edgeφTE°0.003.0018.0118.01
Dihedralν°0.005.005.005.00
Twist angleε°0.000.000.000.00
Thickness ratiot/c%15.0015.0013.708.88
Airfoil--F15_15F15_15F15_15F15_15
Spar parameters
front_sparη [1]x/c [%]
from0.000.20
to1.000.20
rear_spar η [1]x/c [%]
from0.000.60
to1.000.60
Leading edge control devices
Deviceηfromx/cfrom,startx/cfrom,endηtox/cto,startx/cto,end
slat0.110.000.200.290.000.20
slat0.310.000.200.950.000.20
Trailing edge control devices
Deviceηfromx/cfrom,startx/cfrom,endηtox/cto,startx/cto,end
flap_fowler0.110.751.000.300.751.00
flap_fowler0.300.751.000.780.751.00
aileron0.800.701.000.980.701.00
Other control devices
Deviceηfromx/cfrom,startx/cfrom,endηtox/cto,startx/cto,end
spoiler_ground0.200.700.850.290.700.85
spoiler_air0.310.700.850.420.700.85
spoiler_air0.420.700.850.530.700.85
spoiler_air0.530.700.850.650.700.85
spoiler_air0.650.700.850.760.700.85
Mass and CoG
MassCoGxCoGyCoGz
8860.09kg15.72m0.00m-0.63m

Plots

Geometry

Airfoils

Thickness & Geometric Twist