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BOEING VERTOL V43012-1.58

Cambered · 12% thick · low-to-mid Re
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PROFILEBOEING VERTOL V43012-1.58
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.0% @ 32%c
max camber3.7% @ 15%c
LE radius1.60%c
area upper / chord0.0614
area lower / chord-0.0208
area camber / chord0.0203
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.478-50.15293.3330.783911.671.41520ClAngle 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 0.03651% of chord; maximum error 0.2439%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
131
Angle at maximum lift / drag (°)
6
Minimum Cd
0.00639
Maximum Cl
1.257
Angle at maximum Cl (°)
8
Cd at zero lift
0.006515
Cm at zero angle
-0.02133
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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