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CAMBEREDDRELA AGSELIG-DATABASETHIN

AG04

Cambered · 6% thick · low-to-mid Re
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PROFILEAG04
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.4% @ 22%c
max camber1.8% @ 39%c
LE radius0.45%c
area upper / chord0.0319
area lower / chord-0.0085
area camber / chord0.0117
TE thickness0.13%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.6156-50.2673.3331.1511.672.03220ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 0 contributing CFD observations. History windows remain observations, not separate solver runs or automatically converged points.

Model uncertainty is conditional on the stated assumptions and has not been calibrated for this condition. It is not a validated accuracy guarantee.

Geometry fit: RMS error 0.0084% of chord; maximum error 0.02924%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10 · Polar model progressive-polar-gp-v2

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
132.3
Angle at maximum lift / drag (°)
9
Minimum Cd
0.006178
Maximum Cl
1.812
Angle at maximum Cl (°)
16
Cd at zero lift
0.00618
Cm at zero angle
-0.03587
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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