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DAE-11 AIRFOIL

Cambered · 13% thick · low-to-mid Re
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PROFILEDAE-11 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.8% @ 33%c
max camber6.6% @ 44%c
LE radius1.81%c
area upper / chord0.0829
area lower / chord0.0019
area camber / chord0.0424
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.08283-50.60583.3331.29411.671.98320ClAngle 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 0.009337% of chord; maximum error 0.03254%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
157.7
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006581
Maximum Cl
1.811
Angle at maximum Cl (°)
9
Cd at zero lift
—
Cm at zero angle
-0.1442
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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