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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 368 AIRFOIL

Cambered · 8% thick · low-to-mid Re
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PROFILEGOE 368 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.7% @ 15%c
max camber3.8% @ 30%c
LE radius0.65%c
area upper / chord0.0462
area lower / chord0.0012
area camber / chord0.0237
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3877-50.28263.3330.952911.671.62320ClAngle 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 0.04698% of chord; maximum error 0.178%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
156.6
Angle at maximum lift / drag (°)
7
Minimum Cd
0.00582
Maximum Cl
1.456
Angle at maximum Cl (°)
9
Cd at zero lift
0.005998
Cm at zero angle
-0.0701
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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