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CAMBEREDEPPLERSELIG-DATABASE

E211 (10.96%)

Cambered · 11% thick · low-to-mid Re
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PROFILEE211 (10.96%)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.9% @ 33%c
max camber2.6% @ 56%c
LE radius1.32%c
area upper / chord0.0548
area lower / chord-0.0165
area camber / chord0.0191
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.33-50.46443.3331.25911.672.05320ClAngle 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 0.01826% of chord; maximum error 0.07693%.

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
134.7
Angle at maximum lift / drag (°)
9
Minimum Cd
0.00693
Maximum Cl
1.855
Angle at maximum Cl (°)
16
Cd at zero lift
0.006933
Cm at zero angle
-0.1083
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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