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Aircraft and classic
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B737B
AIRCRAFT AND CLASSIC
CAMBERED
SELIG-DATABASE
B737B
Cambered · 13% thick · low-to-mid Re
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PROFILE
B737B
surface
camber line
BEST-FIT POLAR
Re 102k · M 0.09 · final
10 solved points
M 0.09
(L/D)max
9.5
α @ (L/D)max
2.0°
Cd,min
0.0185
Cl @ Cd,min
0.03
Cd₀ (Cl=0)
0.0188
Cl,max
0.36
α @ Cl,max
5.5°
Cm,0
-0.00
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
▾
max thickness
12.5% @ 29%c
max camber
1.5% @ 7%c
LE radius
1.73%c
area upper / chord
0.0501
area lower / chord
-0.0319
area camber / chord
0.0091
TE thickness
0.08%c
DOWNLOAD COORDINATES
Selig .dat ↓
Lednicer ↓
XFOIL ↓
CSV coords ↓
DXF ↓
Cl–α
Cl–Cd
L/D–α
Cm–α
10 solved points
M 0.09
−
+
fit
-0.3
-0.2
-0.1
0.0
0.1
0.2
0.3
0.4
-4
-2
0
2
4
6
8
angle of attack α [deg]
Cl
POLARS
Re 102k · M 0.09 · 10
best-fit
SOLVER WORK
0 conditions · 0 engine jobs
All 0
Attention 0
Solving 0
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