Airfoils
.Pro
Browse
Search
Detail
Compare
⌕ jump to airfoil…
Browse
Search
Detail
Compare
☾
database
/
Other families
/
B707D
CAMBERED
OTHER FAMILIES
SELIG-DATABASE
B707D
Cambered · 9% thick · low-to-mid Re
+ Add to compare
↓ Download
PROFILE
B707D
surface
camber line
BEST-FIT POLAR
Re 102k · M 0.09 · final
6 solved points
M 0.09
(L/D)max
20.4
α @ (L/D)max
2.0°
Cd,min
0.0160
Cl @ Cd,min
0.22
Cd₀ (Cl=0)
0.0204
Cl,max
0.36
α @ Cl,max
2.0°
Cm,0
-0.04
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
▾
max thickness
9.0% @ 40%c
max camber
2.0% @ 30%c
LE radius
0.89%c
area upper / chord
0.0438
area lower / chord
-0.0157
area camber / chord
0.0140
TE thickness
0.00%c
DOWNLOAD COORDINATES
Selig .dat ↓
Lednicer ↓
XFOIL ↓
CSV coords ↓
DXF ↓
Cl–α
Cl–Cd
L/D–α
Cm–α
6 solved points
M 0.09
−
+
fit
-0.3
-0.2
-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 · 6
best-fit
SOLVER WORK
0 conditions · 0 engine jobs
All 0
Attention 0
Solving 0
Re ↑
attention first
recent
Loading solver work…