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Aircraft and classic
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B737D
AIRCRAFT AND CLASSIC
CAMBERED
SELIG-DATABASE
B737D
Cambered · 11% thick · low-to-mid Re
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PROFILE
B737D
surface
camber line
BEST-FIT POLAR
Re 102k · M 0.09 · final
7 solved points
M 0.09
(L/D)max
14.0
α @ (L/D)max
4.0°
Cd,min
0.0201
Cl @ Cd,min
0.07
Cd₀ (Cl=0)
0.0209
Cl,max
0.43
α @ Cl,max
4.0°
Cm,0
-0.02
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
▾
max thickness
10.8% @ 40%c
max camber
1.6% @ 21%c
LE radius
1.28%c
area upper / chord
0.0460
area lower / chord
-0.0256
area camber / chord
0.0102
TE thickness
0.16%c
DOWNLOAD COORDINATES
Selig .dat ↓
Lednicer ↓
XFOIL ↓
CSV coords ↓
DXF ↓
Cl–α
Cl–Cd
L/D–α
Cm–α
7 solved points
M 0.09
−
+
fit
-0.3
-0.2
-0.1
0.0
0.1
0.2
0.3
0.4
-5
-4
-3
-2
-1
0
1
2
3
4
angle of attack α [deg]
Cl
POLARS
Re 102k · M 0.09 · 7
best-fit
SOLVER WORK
0 conditions · 0 engine jobs
All 0
Attention 0
Solving 0
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