Airfoils
.Pro
Browse
Search
Detail
Compare
⌕ jump to airfoil…
Browse
Search
Detail
Compare
☾
database
/
Other families
/
AVISTAR
CAMBERED
OTHER FAMILIES
SELIG-DATABASE
AVISTAR
Cambered · 15% thick · low-to-mid Re
+ Add to compare
↓ Download
PROFILE
AVISTAR
surface
camber line
BEST-FIT POLAR
Re 102k · M 0.09 · final
13 solved points
M 0.09
(L/D)max
0.9
α @ (L/D)max
7.0°
Cd,min
0.0285
Cl @ Cd,min
-0.27
Cd₀ (Cl=0)
0.0504
Cl,max
0.05
α @ Cl,max
7.0°
Cm,0
0.06
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
▾
max thickness
14.5% @ 35%c
max camber
2.2% @ 38%c
LE radius
2.32%c
area upper / chord
0.0629
area lower / chord
-0.0358
area camber / chord
0.0135
TE thickness
0.32%c
DOWNLOAD COORDINATES
Selig .dat ↓
Lednicer ↓
XFOIL ↓
CSV coords ↓
DXF ↓
Cl–α
Cl–Cd
L/D–α
Cm–α
13 solved points
M 0.09
−
+
fit
-0.3
-0.3
-0.2
-0.2
-0.1
-0.1
0.0
0.0
-4
-2
0
2
4
6
angle of attack α [deg]
Cl
POLARS
Re 102k · M 0.09 · 13
best-fit
SOLVER WORK
0 conditions · 0 engine jobs
All 0
Attention 0
Solving 0
Re ↑
attention first
recent
Loading solver work…