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CAMBEREDDRELA AGSELIG-DATABASETHIN

AG19

Cambered · 5% thick · low-to-mid Re
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PROFILEAG19
surfacecamber line
GEOMETRY · AREA METRICS
max thickness5.4% @ 20%c
max camber2.3% @ 43%c
LE radius0.32%c
area upper / chord0.0319
area lower / chord-0.0005
area camber / chord0.0157
TE thickness0.10%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4774-50.086453.3330.650311.671.21420ClAngle 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 0.005472% of chord; maximum error 0.02154%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
140.6
Angle at maximum lift / drag (°)
5
Minimum Cd
0.005545
Maximum Cl
1.073
Angle at maximum Cl (°)
7
Cd at zero lift
0.005608
Cm at zero angle
-0.06151
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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