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W1011

Symmetric · 11% thick · low-to-mid Re
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PROFILEW1011
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.0% @ 26%c
max camber0.1% @ 0%c
LE radius1.33%c
area upper / chord0.0352
area lower / chord-0.0352
area camber / chord0.0000
TE thickness0.16%c
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Polars

Preliminary
NeuralFoil
-0.8201-50.10873.3331.03811.671.96620ClAngle 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.

Geometry fit: RMS error 0.0133% of chord; maximum error 0.03755%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
126.1
Angle at maximum lift / drag (°)
11
Minimum Cd
0.006869
Maximum Cl
1.734
Angle at maximum Cl (°)
17
Cd at zero lift
0.006869
Cm at zero angle
-0.0001856
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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