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CAMBEREDDRELA AGSELIG-DATABASE

AG23 XC Bubble

Cambered · 9% thick · low-to-mid Re
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PROFILEAG23 XC Bubble
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.9% @ 27%c
max camber2.2% @ 45%c
LE radius0.87%c
area upper / chord0.0439
area lower / chord-0.0129
area camber / chord0.0155
TE thickness0.10%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4637-50.14263.3330.74911.671.35520ClAngle 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 0.008018% of chord; maximum error 0.02834%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
144
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005948
Maximum Cl
1.204
Angle at maximum Cl (°)
7
Cd at zero lift
0.005965
Cm at zero angle
-0.074
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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