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BOEING-VERTOL VR-9 AIRFOIL

Symmetric · 6% thick · low-to-mid Re
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PROFILEBOEING-VERTOL VR-9 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.1% @ 35%c
max camber0.3% @ 35%c
LE radius0.40%c
area upper / chord0.0215
area lower / chord-0.0175
area camber / chord0.0020
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.7415-50.082693.3330.906911.671.73120ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 0 contributing CFD observations. History windows remain observations, not separate solver runs or automatically converged points.

Model uncertainty is conditional on the stated assumptions and has not been calibrated for this condition. It is not a validated accuracy guarantee.

Geometry fit: RMS error 0.0137% of chord; maximum error 0.08726%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10 · Polar model progressive-polar-gp-v2

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
105.6
Angle at maximum lift / drag (°)
8
Minimum Cd
0.006107
Maximum Cl
1.525
Angle at maximum Cl (°)
15
Cd at zero lift
0.006107
Cm at zero angle
-0.004922
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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