Airfoils
.Pro
Browse
Search
Detail
Compare
⌕ jump to airfoil…
Browse
Search
Detail
Compare
☾
database
/
Other families
/
20-32C AIRFOIL
CAMBERED
OTHER FAMILIES
SELIG-DATABASE
THIN
20-32C AIRFOIL
Cambered · 8% thick · low-to-mid Re
+ Add to compare
↓ Download
PROFILE
20-32C AIRFOIL
surface
camber line
BEST-FIT POLAR
Re 102k · M 0.09 · provisional
74 solved points
M 0.09
(L/D)max
42.8
α @ (L/D)max
2.5°
Cd,min
0.0200
Cl @ Cd,min
0.83
Cd₀ (Cl=0)
0.0560
Cl,max
1.23
α @ Cl,max
17.5°
Cm,0
-0.02
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
▾
max thickness
8.0% @ 20%c
max camber
6.9% @ 39%c
LE radius
0.70%c
area upper / chord
0.0691
area lower / chord
0.0229
area camber / chord
0.0460
TE thickness
0.32%c
DOWNLOAD COORDINATES
Selig .dat ↓
Lednicer ↓
XFOIL ↓
CSV coords ↓
DXF ↓
Cl–α
Cl–Cd
L/D–α
Cm–α
74 solved points
M 0.09–0.49
−
+
fit
0.0
0.2
0.4
0.6
0.8
1.0
1.2
1.4
0
5
10
15
20
2
2
2
2
2
angle of attack α [deg]
Cl
POLARS
Re 102k · M 0.09 · 24
Re 307k · M 0.26 · 25
Re 566k · M 0.49 · 25
best-fit
alternate stored result · not in best-fit
needs URANS confirmation
post-stall → URANS
SOLVER WORK
0 conditions · 0 engine jobs
All 0
Attention 0
Solving 0
Re ↑
attention first
recent
Loading solver work…