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CAMBEREDDRELA AGSELIG-DATABASETHIN

AG55

Cambered · 7% thick · low-to-mid Re
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PROFILEAG55
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.6% @ 25%c
max camber2.0% @ 36%c
LE radius0.48%c
area upper / chord0.0343
area lower / chord-0.0074
area camber / chord0.0135
TE thickness0.10%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5385-50.048713.3330.635911.671.22320ClAngle 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 0.005043% of chord; maximum error 0.01751%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
133.8
Angle at maximum lift / drag (°)
5
Minimum Cd
0.00567
Maximum Cl
1.076
Angle at maximum Cl (°)
7
Cd at zero lift
0.0057
Cm at zero angle
-0.04632
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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