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K3311 (original)

Cambered · 11% thick · low-to-mid Re
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PROFILEK3311 (original)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.0% @ 30%c
max camber3.3% @ 40%c
LE radius1.33%c
area upper / chord0.0580
area lower / chord-0.0133
area camber / chord0.0224
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.362-50.26183.3330.885711.671.5120ClAngle 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.

The compressibility correction is a low-fidelity estimate, not a resolved shock or compressible CFD solution.

Geometry fit: RMS error 0.0365% of chord; maximum error 0.2201%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
145.1
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006269
Maximum Cl
1.354
Angle at maximum Cl (°)
8
Cd at zero lift
0.006283
Cm at zero angle
-0.08653
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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