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CAMBEREDDRELA AGSELIG-DATABASETHIN

AG46c -03f

Cambered · 6% thick · low-to-mid Re
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PROFILEAG46c -03f
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.0% @ 23%c
max camber2.3% @ 42%c
LE radius0.40%c
area upper / chord0.0372
area lower / chord-0.0001
area camber / chord0.0185
TE thickness0.08%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7144-5-0.091823.3330.530811.671.15320ClAngle 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 0.01326% of chord; maximum error 0.06361%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
128
Angle at maximum lift / drag (°)
6
Minimum Cd
0.00561
Maximum Cl
0.9977
Angle at maximum Cl (°)
17
Cd at zero lift
0.005635
Cm at zero angle
-0.02711
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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