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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 287 AIRFOIL

Cambered · 9% thick · low-to-mid Re
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PROFILEGOE 287 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.9% @ 30%c
max camber4.9% @ 39%c
LE radius0.87%c
area upper / chord0.0600
area lower / chord0.0008
area camber / chord0.0304
TE thickness0.50%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3282-50.3773.3331.08211.671.78720ClAngle 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 0.05479% of chord; maximum error 0.2812%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
155.3
Angle at maximum lift / drag (°)
8
Minimum Cd
0.006385
Maximum Cl
1.611
Angle at maximum Cl (°)
9
Cd at zero lift
0.007649
Cm at zero angle
-0.08395
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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