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BE50 (original)

Cambered · 7% thick · low-to-mid Re
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PROFILEBE50 (original)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.3% @ 25%c
max camber4.8% @ 44%c
LE radius0.58%c
area upper / chord0.0575
area lower / chord0.0119
area camber / chord0.0347
TE thickness0.26%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.154-50.43033.3331.01511.671.59920ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 0 contributing CFD observations. History windows remain observations, not separate solver runs or automatically converged points.

Model uncertainty is conditional on the stated assumptions and has not been calibrated for this condition. It is not a validated accuracy guarantee.

Geometry fit: RMS error 0.03928% of chord; maximum error 0.2152%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10 · Polar model progressive-polar-gp-v2

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
161
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006019
Maximum Cl
1.453
Angle at maximum Cl (°)
7
Cd at zero lift
0.006212
Cm at zero angle
-0.1214
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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