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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 600 AIRFOIL

Cambered · 13% thick · low-to-mid Re
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PROFILEGOE 600 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness13.1% @ 31%c
max camber1.9% @ 49%c
LE radius1.88%c
area upper / chord0.0567
area lower / chord-0.0321
area camber / chord0.0123
TE thickness0.50%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6008-50.2693.3331.13911.672.00820ClAngle 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.

Geometry fit: RMS error 0.05437% of chord; maximum error 0.26%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
128.4
Angle at maximum lift / drag (°)
10
Minimum Cd
0.007406
Maximum Cl
1.791
Angle at maximum Cl (°)
16
Cd at zero lift
0.007426
Cm at zero angle
-0.04657
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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