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B-29 TIP AIRFOIL
CAMBERED
OTHER FAMILIES
SELIG-DATABASE
B-29 TIP AIRFOIL
Cambered · 9% thick · low-to-mid Re
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PROFILE
B-29 TIP AIRFOIL
surface
camber line
BEST-FIT POLAR
Re 102k · M 0.09 · final
10 solved points
M 0.09
(L/D)max
17.1
α @ (L/D)max
5.0°
Cd,min
0.0194
Cl @ Cd,min
0.16
Cd₀ (Cl=0)
0.0214
Cl,max
0.58
α @ Cl,max
5.0°
Cm,0
-0.02
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
▾
max thickness
9.0% @ 30%c
max camber
2.2% @ 30%c
LE radius
0.89%c
area upper / chord
0.0410
area lower / chord
-0.0183
area camber / chord
0.0113
TE thickness
0.00%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
-0.4
-0.2
0.0
0.2
0.4
0.6
-4
-2
0
2
4
angle of attack α [deg]
Cl
POLARS
Re 102k · M 0.09 · 10
best-fit
SOLVER WORK
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Solving 0
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