Airfoils.Pro
database / Gottingen / GOE 802 B
CAMBEREDGOTTINGENSELIG-DATABASE

GOE 802 B

Cambered · 10% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 802 B
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.8% @ 30%c
max camber6.2% @ 39%c
LE radius1.06%c
area upper / chord0.0760
area lower / chord0.0083
area camber / chord0.0422
TE thickness0.40%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.07479-50.60453.3331.28411.671.96320ClAngle 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 0.2892% of chord; maximum error 0.907%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
170.8
Angle at maximum lift / drag (°)
7
Minimum Cd
0.007731
Maximum Cl
1.793
Angle at maximum Cl (°)
9
Cd at zero lift
—
Cm at zero angle
-0.154
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…