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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 207 (AVIATIK

Cambered · 9% thick · low-to-mid Re
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PROFILEGOE 207 (AVIATIK
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.8% @ 20%c
max camber6.6% @ 30%c
LE radius0.85%c
area upper / chord0.0699
area lower / chord0.0111
area camber / chord0.0405
TE thickness0.75%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1685-50.52913.3331.22711.671.92420ClAngle 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 0.07069% of chord; maximum error 0.4011%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
157.4
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007054
Maximum Cl
1.75
Angle at maximum Cl (°)
9
Cd at zero lift
—
Cm at zero angle
-0.1117
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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