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CAMBEREDDRELA AGSELIG-DATABASETHIN

AG54

Cambered · 8% thick · low-to-mid Re
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PROFILEAG54
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.5% @ 26%c
max camber1.9% @ 38%c
LE radius0.63%c
area upper / chord0.0372
area lower / chord-0.0116
area camber / chord0.0128
TE thickness0.07%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5397-50.053113.3330.64611.671.23920ClAngle 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 0.00801% of chord; maximum error 0.0265%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
133.7
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005791
Maximum Cl
1.091
Angle at maximum Cl (°)
7
Cd at zero lift
0.005799
Cm at zero angle
-0.04858
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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