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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 177 AIRFOIL

Cambered · 8% thick · low-to-mid Re
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PROFILEGOE 177 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.7% @ 20%c
max camber5.1% @ 39%c
LE radius0.65%c
area upper / chord0.0571
area lower / chord0.0084
area camber / chord0.0328
TE thickness0.20%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2379-50.42383.3331.08511.671.74720ClAngle 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 0.05681% of chord; maximum error 0.2324%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
166.1
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006098
Maximum Cl
1.582
Angle at maximum Cl (°)
9
Cd at zero lift
0.006937
Cm at zero angle
-0.1104
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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