Airfoils.Pro
database / Other families / WB13535SM
CAMBEREDOTHER FAMILIESSELIG-DATABASE

WB13535SM

Cambered · 14% thick · low-to-mid Re
Compare↓ Download
PROFILEWB13535SM
surfacecamber line
GEOMETRY · AREA METRICS
max thickness13.6% @ 26%c
max camber3.8% @ 50%c
LE radius2.02%c
area upper / chord0.0681
area lower / chord-0.0195
area camber / chord0.0243
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3567-50.32873.3331.01411.671.720ClAngle of attack (°)
Why this curve

This is a NeuralFoil prediction from the stored profile coordinates and the selected flow condition, with AeroSandbox compressibility corrections. It is not a completed OpenFOAM calculation.

Prediction error has not been calibrated for this condition. No accuracy interval is claimed.

The compressibility correction is a low-fidelity estimate, not a resolved shock or compressible CFD solution.

Geometry fit: RMS error 0.04398% of chord; maximum error 0.2239%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
145
Angle at maximum lift / drag (°)
8
Minimum Cd
0.006685
Maximum Cl
1.528
Angle at maximum Cl (°)
10
Cd at zero lift
0.006726
Cm at zero angle
-0.09221
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…