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BOEING-VERTOL V23010-1.58 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILEBOEING-VERTOL V23010-1.58 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.2% @ 30%c
max camber1.7% @ 15%c
LE radius1.14%c
area upper / chord0.0428
area lower / chord-0.0246
area camber / chord0.0091
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.686-50.20713.3331.111.671.99320ClAngle 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 0.04216% of chord; maximum error 0.2539%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
126.1
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006542
Maximum Cl
1.77
Angle at maximum Cl (°)
17
Cd at zero lift
0.006543
Cm at zero angle
-0.008478
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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