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CAMBEREDEPPLERSELIG-DATABASETHIN

E61 (5.64%)

Cambered · 6% thick · low-to-mid Re
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PROFILEE61 (5.64%)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness5.7% @ 24%c
max camber6.7% @ 51%c
LE radius0.35%c
area upper / chord0.0665
area lower / chord0.0279
area camber / chord0.0472
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
0.3166-50.84763.3331.37911.671.9120ClAngle 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 0.01583% of chord; maximum error 0.06916%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
185.3
Angle at maximum lift / drag (°)
4
Minimum Cd
0.006394
Maximum Cl
1.777
Angle at maximum Cl (°)
6
Cd at zero lift
—
Cm at zero angle
-0.2598
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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