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CAMBEREDEPPLERSELIG-DATABASETHIN

E59

Cambered · 6% thick · low-to-mid Re
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PROFILEE59
surfacecamber line
GEOMETRY · AREA METRICS
max thickness5.6% @ 26%c
max camber5.2% @ 53%c
LE radius0.35%c
area upper / chord0.0565
area lower / chord0.0177
area camber / chord0.0371
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
0.1356-50.64913.3331.16311.671.67620ClAngle 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 0.05166% of chord; maximum error 0.2404%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
174.6
Angle at maximum lift / drag (°)
4
Minimum Cd
0.006103
Maximum Cl
1.548
Angle at maximum Cl (°)
6
Cd at zero lift
—
Cm at zero angle
-0.2214
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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