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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 462 AIRFOIL

Cambered · 11% thick · low-to-mid Re
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PROFILEGOE 462 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.0% @ 10%c
max camber13.4% @ 30%c
LE radius1.32%c
area upper / chord0.1006
area lower / chord0.0641
area camber / chord0.0823
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
0.1903-50.94573.3331.70111.672.45620ClAngle 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 0.1085% of chord; maximum error 0.4516%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
145.7
Angle at maximum lift / drag (°)
6
Minimum Cd
0.01241
Maximum Cl
2.268
Angle at maximum Cl (°)
12
Cd at zero lift
—
Cm at zero angle
-0.2049
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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