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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 795 AIRFOIL

Cambered · 8% thick · low-to-mid Re
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PROFILEGOE 795 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.0% @ 31%c
max camber2.4% @ 43%c
LE radius0.71%c
area upper / chord0.0445
area lower / chord-0.0123
area camber / chord0.0161
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4696-50.10983.3330.689111.671.26820ClAngle 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 0.01386% of chord; maximum error 0.04891%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
135.7
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005991
Maximum Cl
1.124
Angle at maximum Cl (°)
7
Cd at zero lift
0.006007
Cm at zero angle
-0.06382
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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