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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 187 (SCHUETTE-LANZ

Cambered · 8% thick · low-to-mid Re
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PROFILEGOE 187 (SCHUETTE-LANZ
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.3% @ 30%c
max camber4.8% @ 30%c
LE radius0.76%c
area upper / chord0.0602
area lower / chord0.0044
area camber / chord0.0323
TE thickness0.50%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2795-50.36853.3331.01711.671.66520ClAngle 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 0.04827% of chord; maximum error 0.2098%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
155.7
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006813
Maximum Cl
1.503
Angle at maximum Cl (°)
8
Cd at zero lift
0.007774
Cm at zero angle
-0.09149
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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