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USA 50 AIRFOIL

Cambered · 7% thick · low-to-mid Re
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PROFILEUSA 50 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.0% @ 30%c
max camber1.9% @ 40%c
LE radius0.55%c
area upper / chord0.0374
area lower / chord-0.0109
area camber / chord0.0132
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4815-50.084123.3330.649711.671.21520ClAngle 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 0.04273% of chord; maximum error 0.1911%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
133.4
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005816
Maximum Cl
1.074
Angle at maximum Cl (°)
7
Cd at zero lift
0.005838
Cm at zero angle
-0.05628
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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