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BACNLF

Cambered · 10% thick · low-to-mid Re
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PROFILEBACNLF
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.1% @ 43%c
max camber1.4% @ 74%c
LE radius1.12%c
area upper / chord0.0413
area lower / chord-0.0273
area camber / chord0.0070
TE thickness0.24%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5325-50.040143.3330.612811.671.18520ClAngle 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 0.0154% of chord; maximum error 0.14%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
123.6
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006312
Maximum Cl
1.042
Angle at maximum Cl (°)
7
Cd at zero lift
0.006318
Cm at zero angle
-0.07692
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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