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USA 29 AIRFOIL

Cambered · 13% thick · low-to-mid Re
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PROFILEUSA 29 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness13.2% @ 30%c
max camber5.5% @ 40%c
LE radius1.91%c
area upper / chord0.0768
area lower / chord-0.0128
area camber / chord0.0320
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.271-50.37893.3331.02911.671.67920ClAngle 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 0.06917% of chord; maximum error 0.2881%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
133.8
Angle at maximum lift / drag (°)
9
Minimum Cd
0.007038
Maximum Cl
1.516
Angle at maximum Cl (°)
11
Cd at zero lift
0.007181
Cm at zero angle
-0.0956
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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