Airfoils
.Pro
Browse
Search
Detail
Compare
⌕ jump to airfoil…
Browse
Search
Detail
Compare
☾
database
/
Other families
/
BOE106
CAMBERED
OTHER FAMILIES
SELIG-DATABASE
BOE106
Cambered · 13% thick · low-to-mid Re
+ Add to compare
↓ Download
PROFILE
BOE106
surface
camber line
BEST-FIT POLAR
Re 102k · M 0.09 · final
5 solved points
M 0.09
(L/D)max
19.7
α @ (L/D)max
2.0°
Cd,min
0.0187
Cl @ Cd,min
0.29
Cd₀ (Cl=0)
0.0352
Cl,max
0.43
α @ Cl,max
2.0°
Cm,0
-0.04
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
▾
max thickness
13.1% @ 30%c
max camber
3.3% @ 40%c
LE radius
1.88%c
area upper / chord
0.0663
area lower / chord
-0.0224
area camber / chord
0.0219
TE thickness
0.04%c
DOWNLOAD COORDINATES
Selig .dat ↓
Lednicer ↓
XFOIL ↓
CSV coords ↓
DXF ↓
Cl–α
Cl–Cd
L/D–α
Cm–α
5 solved points
M 0.09
−
+
fit
-0.1
0.0
0.1
0.2
0.3
0.4
-5
-4
-3
-2
-1
0
1
2
angle of attack α [deg]
Cl
POLARS
Re 102k · M 0.09 · 5
best-fit
SOLVER WORK
0 conditions · 0 engine jobs
All 0
Attention 0
Solving 0
Re ↑
attention first
recent
Loading solver work…