Airfoils.Pro
database / Gottingen / GOE 238 (HANSA-BRANDENBURG)
CAMBEREDGOTTINGENSELIG-DATABASE

GOE 238 (HANSA-BRANDENBURG)

Cambered · 10% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 238 (HANSA-BRANDENBURG)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.8% @ 30%c
max camber5.5% @ 30%c
LE radius1.06%c
area upper / chord0.0640
area lower / chord0.0009
area camber / chord0.0325
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2361-50.39123.3331.01811.671.64620ClAngle 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 0.07321% of chord; maximum error 0.3365%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
156.9
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006321
Maximum Cl
1.489
Angle at maximum Cl (°)
8
Cd at zero lift
0.01245
Cm at zero angle
-0.08237
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…