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WACO COOTIE AIRFOIL

Cambered · 8% thick · low-to-mid Re
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PROFILEWACO COOTIE AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.5% @ 30%c
max camber6.3% @ 40%c
LE radius0.79%c
area upper / chord0.0723
area lower / chord0.0125
area camber / chord0.0424
TE thickness0.50%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1033-50.52143.3331.14611.671.77120ClAngle 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 0.06117% of chord; maximum error 0.2532%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
162.5
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006444
Maximum Cl
1.615
Angle at maximum Cl (°)
8
Cd at zero lift
—
Cm at zero angle
-0.1283
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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