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CAMBEREDDRELA AGSELIG-DATABASETHIN

AG18

Cambered · 6% thick · low-to-mid Re
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PROFILEAG18
surfacecamber line
GEOMETRY · AREA METRICS
max thickness5.9% @ 21%c
max camber2.2% @ 44%c
LE radius0.38%c
area upper / chord0.0325
area lower / chord-0.0027
area camber / chord0.0149
TE thickness0.09%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4893-50.081473.3330.652211.671.22320ClAngle 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 0.006668% of chord; maximum error 0.02444%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
139.2
Angle at maximum lift / drag (°)
5
Minimum Cd
0.005579
Maximum Cl
1.08
Angle at maximum Cl (°)
7
Cd at zero lift
0.005629
Cm at zero angle
-0.06069
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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