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CLARK W AIRFOIL

Cambered · 11% thick · low-to-mid Re
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PROFILECLARK W AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.2% @ 30%c
max camber3.8% @ 40%c
LE radius1.39%c
area upper / chord0.0635
area lower / chord-0.0156
area camber / chord0.0240
TE thickness0.10%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3561-50.26323.3330.882511.671.50220ClAngle 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 0.05812% of chord; maximum error 0.2747%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
145
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006562
Maximum Cl
1.347
Angle at maximum Cl (°)
8
Cd at zero lift
0.006572
Cm at zero angle
-0.09139
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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