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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 235 (SCHUETTE-LANZ)

Cambered · 7% thick · low-to-mid Re
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PROFILEGOE 235 (SCHUETTE-LANZ)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.5% @ 20%c
max camber3.5% @ 39%c
LE radius0.47%c
area upper / chord0.0458
area lower / chord-0.0002
area camber / chord0.0228
TE thickness0.32%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4689-50.4263.3331.32111.672.21620ClAngle 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 0.069% of chord; maximum error 0.3201%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
144.2
Angle at maximum lift / drag (°)
9
Minimum Cd
0.006502
Maximum Cl
1.992
Angle at maximum Cl (°)
16
Cd at zero lift
0.006541
Cm at zero angle
-0.06752
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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