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CH10 (smoothed)

Cambered · 13% thick · low-to-mid Re
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PROFILECH10 (smoothed)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.8% @ 31%c
max camber10.2% @ 49%c
LE radius1.82%c
area upper / chord0.1111
area lower / chord0.0273
area camber / chord0.0692
TE thickness0.01%c
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Polars

Preliminary
NeuralFoil
0.6507-51.2373.3331.82411.672.4120ClAngle 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 0.0174% of chord; maximum error 0.04684%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
153.8
Angle at maximum lift / drag (°)
1
Minimum Cd
0.007777
Maximum Cl
2.264
Angle at maximum Cl (°)
11
Cd at zero lift
—
Cm at zero angle
-0.3243
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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