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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 370 AIRFOIL

Cambered · 5% thick · low-to-mid Re
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PROFILEGOE 370 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness4.6% @ 21%c
max camber5.7% @ 40%c
LE radius0.24%c
area upper / chord0.0533
area lower / chord0.0188
area camber / chord0.0360
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.1386-50.45093.3331.0411.671.6320ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 0 contributing CFD observations. History windows remain observations, not separate solver runs or automatically converged points.

Model uncertainty is conditional on the stated assumptions and has not been calibrated for this condition. It is not a validated accuracy guarantee.

Geometry fit: RMS error 0.04752% of chord; maximum error 0.1933%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10 · Polar model progressive-polar-gp-v2

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
167.2
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005896
Maximum Cl
1.483
Angle at maximum Cl (°)
8
Cd at zero lift
—
Cm at zero angle
-0.1294
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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