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NACA 4-DIGITSELIG-DATABASESYMMETRIC

NACA 0011SC

Symmetric · 11% thick · low-to-mid Re
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PROFILENACA 0011SC
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.0% @ 40%c
max camber0.0% @ 0%c
LE radius1.32%c
area upper / chord0.0419
area lower / chord-0.0419
area camber / chord0.0000
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7548-50.097633.3330.950111.671.80320ClAngle 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 0.02154% of chord; maximum error 0.06145%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
121.2
Angle at maximum lift / drag (°)
12
Minimum Cd
0.007277
Maximum Cl
1.589
Angle at maximum Cl (°)
17
Cd at zero lift
0.007277
Cm at zero angle
-3.432e-17
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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