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BOEING VERTOL V13006-.7

Cambered · 6% thick · low-to-mid Re
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PROFILEBOEING VERTOL V13006-.7
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.0% @ 30%c
max camber0.9% @ 20%c
LE radius0.39%c
area upper / chord0.0257
area lower / chord-0.0155
area camber / chord0.0051
TE thickness0.12%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.735-50.15593.3331.04711.671.93820ClAngle 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.

Geometry fit: RMS error 0.02211% of chord; maximum error 0.07538%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
125.7
Angle at maximum lift / drag (°)
9
Minimum Cd
0.006101
Maximum Cl
1.715
Angle at maximum Cl (°)
17
Cd at zero lift
0.006112
Cm at zero angle
-0.007533
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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