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CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 692 AIRFOIL

Cambered · 16% thick · low-to-mid Re
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PROFILEGOE 692 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness16.1% @ 30%c
max camber5.1% @ 40%c
LE radius2.86%c
area upper / chord0.0909
area lower / chord-0.0222
area camber / chord0.0343
TE thickness0.50%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1791-50.51233.3331.20411.671.89520ClAngle 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 0.06521% of chord; maximum error 0.3151%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
141
Angle at maximum lift / drag (°)
7
Minimum Cd
0.00732
Maximum Cl
1.722
Angle at maximum Cl (°)
10
Cd at zero lift
0.007516
Cm at zero angle
-0.1387
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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