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BOE106

Cambered · 13% thick · low-to-mid Re
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PROFILEBOE106
surfacecamber line
GEOMETRY · AREA METRICS
max thickness13.1% @ 30%c
max camber3.3% @ 40%c
LE radius1.88%c
area upper / chord0.0663
area lower / chord-0.0224
area camber / chord0.0219
TE thickness0.04%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4158-50.21963.3330.855111.671.49120ClAngle 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 0.05527% of chord; maximum error 0.2782%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
138.6
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006696
Maximum Cl
1.332
Angle at maximum Cl (°)
8
Cd at zero lift
0.006696
Cm at zero angle
-0.06821
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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