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AIRCRAFT AND CLASSICCAMBEREDSELIG-DATABASETHICK

USA 35 A

Cambered · 18% thick · low-to-mid Re
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PROFILEUSA 35 A
surfacecamber line
GEOMETRY · AREA METRICS
max thickness18.2% @ 29%c
max camber6.4% @ 39%c
LE radius3.64%c
area upper / chord0.1036
area lower / chord-0.0182
area camber / chord0.0427
TE thickness0.43%c
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Polars

Preliminary
NeuralFoil
-0.008974-50.63543.3331.2811.671.92420ClAngle 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 0.07466% of chord; maximum error 0.3456%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
135.3
Angle at maximum lift / drag (°)
5
Minimum Cd
0.007911
Maximum Cl
1.763
Angle at maximum Cl (°)
10
Cd at zero lift
—
Cm at zero angle
-0.1531
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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