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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 374 AIRFOIL

Cambered · 6% thick · low-to-mid Re
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PROFILEGOE 374 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.5% @ 30%c
max camber4.5% @ 30%c
LE radius0.46%c
area upper / chord0.0515
area lower / chord0.0079
area camber / chord0.0297
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2849-50.33683.3330.958611.671.5820ClAngle 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 0.0503% of chord; maximum error 0.2948%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
162.2
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006005
Maximum Cl
1.425
Angle at maximum Cl (°)
8
Cd at zero lift
0.006952
Cm at zero angle
-0.08003
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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