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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 599 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILEGOE 599 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.0% @ 30%c
max camber1.5% @ 59%c
LE radius1.10%c
area upper / chord0.0449
area lower / chord-0.0244
area camber / chord0.0103
TE thickness0.35%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5773-50.29143.3331.1611.672.02920ClAngle 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 0.05056% of chord; maximum error 0.2387%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
131.8
Angle at maximum lift / drag (°)
10
Minimum Cd
0.00696
Maximum Cl
1.812
Angle at maximum Cl (°)
16
Cd at zero lift
0.006964
Cm at zero angle
-0.0555
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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