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CAMBEREDEPPLERSELIG-DATABASE

E226 (10.19%)

Cambered · 10% thick · low-to-mid Re
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PROFILEE226 (10.19%)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.2% @ 29%c
max camber1.0% @ 43%c
LE radius1.14%c
area upper / chord0.0400
area lower / chord-0.0267
area camber / chord0.0066
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6658-5-0.044393.3330.57711.671.19820ClAngle 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 0.0184% of chord; maximum error 0.08613%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
120.3
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006217
Maximum Cl
1.043
Angle at maximum Cl (°)
8
Cd at zero lift
0.006217
Cm at zero angle
-0.02509
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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