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CAMBEREDDRELA AGSELIG-DATABASETHIN

AG14

Cambered · 5% thick · low-to-mid Re
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PROFILEAG14
surfacecamber line
GEOMETRY · AREA METRICS
max thickness5.4% @ 20%c
max camber2.1% @ 40%c
LE radius0.32%c
area upper / chord0.0304
area lower / chord-0.0013
area camber / chord0.0146
TE thickness0.10%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5006-50.068383.3330.637411.671.20620ClAngle 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 0.005836% of chord; maximum error 0.0243%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
138.3
Angle at maximum lift / drag (°)
5
Minimum Cd
0.005527
Maximum Cl
1.064
Angle at maximum Cl (°)
7
Cd at zero lift
0.005579
Cm at zero angle
-0.0566
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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