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SIKORSKY DBLN-526 AIRFOIL

Cambered · 26% thick · low-to-mid Re
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PROFILESIKORSKY DBLN-526 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness26.0% @ 50%c
max camber4.0% @ 50%c
LE radius7.44%c
area upper / chord0.1295
area lower / chord-0.0702
area camber / chord0.0296
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.5934-50.086453.3330.766311.671.44620ClAngle 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 0.136% of chord; maximum error 0.4494%.

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
37.6
Angle at maximum lift / drag (°)
11
Minimum Cd
0.01374
Maximum Cl
1.276
Angle at maximum Cl (°)
16
Cd at zero lift
0.01474
Cm at zero angle
0.006274
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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