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USA 32 AIRFOIL

Cambered · 15% thick · low-to-mid Re
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PROFILEUSA 32 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness14.7% @ 20%c
max camber9.3% @ 40%c
LE radius2.39%c
area upper / chord0.1125
area lower / chord0.0058
area camber / chord0.0592
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
0.1195-50.71033.3331.30111.671.89220ClAngle 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 0.08216% of chord; maximum error 0.2795%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
111.2
Angle at maximum lift / drag (°)
5
Minimum Cd
0.008323
Maximum Cl
1.744
Angle at maximum Cl (°)
11
Cd at zero lift
—
Cm at zero angle
-0.1427
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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