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NASA SC(2)-0503 AIRFOIL

Symmetric · 3% thick · low-to-mid Re
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PROFILENASA SC(2)-0503 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness3.0% @ 33%c
max camber-0.7% @ 100%c
LE radius0.10%c
area upper / chord0.0105
area lower / chord-0.0100
area camber / chord0.0003
TE thickness0.24%c
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Polars

Preliminary
NeuralFoil
-0.5292-50.077973.3330.685111.671.29220ClAngle 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 0.005151% of chord; maximum error 0.03185%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
94.49
Angle at maximum lift / drag (°)
4
Minimum Cd
0.005539
Maximum Cl
1.141
Angle at maximum Cl (°)
17
Cd at zero lift
0.005564
Cm at zero angle
-0.05795
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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