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AIRCRAFT AND CLASSICCAMBEREDSELIG-DATABASE

HOBIESMO1.DAT

Cambered · 9% thick · low-to-mid Re
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PROFILEHOBIESMO1.DAT
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.6% @ 25%c
max camber4.0% @ 45%c
LE radius0.81%c
area upper / chord0.0533
area lower / chord-0.0007
area camber / chord0.0263
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2699-50.33153.3330.932811.671.53420ClAngle 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 0.02312% of chord; maximum error 0.1216%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
158.6
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005972
Maximum Cl
1.384
Angle at maximum Cl (°)
8
Cd at zero lift
0.006021
Cm at zero angle
-0.112
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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