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GIII BL45 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILEGIII BL45 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.4% @ 35%c
max camber0.8% @ 25%c
LE radius1.20%c
area upper / chord0.0401
area lower / chord-0.0329
area camber / chord0.0036
TE thickness0.04%c
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Polars

Preliminary
Combined estimate
-0.7646-50.10813.3330.980811.671.85320ClAngle 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 0.02083% of chord; maximum error 0.1133%.

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
116.5
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006883
Maximum Cl
1.635
Angle at maximum Cl (°)
16
Cd at zero lift
0.006903
Cm at zero angle
0.006516
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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