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CAMBEREDDRELA AGSELIG-DATABASETHIN

AG03 (flat aft

Cambered · 6% thick · low-to-mid Re
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PROFILEAG03 (flat aft
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.2% @ 26%c
max camber2.0% @ 32%c
LE radius0.43%c
area upper / chord0.0342
area lower / chord-0.0074
area camber / chord0.0134
TE thickness0.12%c
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Polars

Preliminary
NeuralFoil
-0.5591-50.026943.3330.612911.671.19920ClAngle 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 0.006632% of chord; maximum error 0.02804%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
130.7
Angle at maximum lift / drag (°)
5
Minimum Cd
0.005692
Maximum Cl
1.052
Angle at maximum Cl (°)
7
Cd at zero lift
0.005732
Cm at zero angle
-0.03807
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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