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ONERA HOR12 AIRFOIL

Cambered · 12% thick · low-to-mid Re
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PROFILEONERA HOR12 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.9% @ 23%c
max camber3.9% @ 48%c
LE radius1.57%c
area upper / chord0.0615
area lower / chord-0.0109
area camber / chord0.0253
TE thickness0.91%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2824-50.34843.3330.979211.671.6120ClAngle 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 0.01231% of chord; maximum error 0.06123%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
144.6
Angle at maximum lift / drag (°)
6
Minimum Cd
0.00716
Maximum Cl
1.452
Angle at maximum Cl (°)
7
Cd at zero lift
0.007171
Cm at zero angle
-0.1253
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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