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DAE-31 AIRFOIL

Cambered · 11% thick · low-to-mid Re
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PROFILEDAE-31 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.1% @ 29%c
max camber6.7% @ 45%c
LE radius1.35%c
area upper / chord0.0816
area lower / chord0.0084
area camber / chord0.0450
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.0004774-50.65663.3331.31411.671.97120ClAngle 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 0.01734% of chord; maximum error 0.07082%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
163.5
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006671
Maximum Cl
1.807
Angle at maximum Cl (°)
9
Cd at zero lift
—
Cm at zero angle
-0.1748
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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