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CAMBEREDDRELA AGSELIG-DATABASE

AG24 Bubble Dancer

Cambered · 8% thick · low-to-mid Re
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PROFILEAG24 Bubble Dancer
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.4% @ 26%c
max camber2.2% @ 45%c
LE radius0.78%c
area upper / chord0.0422
area lower / chord-0.0110
area camber / chord0.0156
TE thickness0.10%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4623-50.14043.3330.743211.671.34620ClAngle 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 0.008019% of chord; maximum error 0.02928%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
143.4
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005887
Maximum Cl
1.195
Angle at maximum Cl (°)
7
Cd at zero lift
0.005908
Cm at zero angle
-0.0737
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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