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CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 382 AIRFOIL

Cambered · 20% thick · low-to-mid Re
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PROFILEGOE 382 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness20.0% @ 29%c
max camber6.0% @ 38%c
LE radius4.42%c
area upper / chord0.1062
area lower / chord-0.0271
area camber / chord0.0395
TE thickness0.21%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.124-50.53393.3331.19211.671.84920ClAngle 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 0.0798% of chord; maximum error 0.4226%.

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
117.3
Angle at maximum lift / drag (°)
5
Minimum Cd
0.007759
Maximum Cl
1.685
Angle at maximum Cl (°)
11
Cd at zero lift
—
Cm at zero angle
-0.1139
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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