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CAMBEREDDRELA AGSELIG-DATABASETHIN

AG08

Cambered · 6% thick · low-to-mid Re
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PROFILEAG08
surfacecamber line
GEOMETRY · AREA METRICS
max thickness5.8% @ 21%c
max camber1.8% @ 39%c
LE radius0.37%c
area upper / chord0.0305
area lower / chord-0.0065
area camber / chord0.0120
TE thickness0.16%c
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Polars

Preliminary
NeuralFoil
-0.6045-50.27393.3331.15211.672.03120ClAngle 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.

Geometry fit: RMS error 0.005403% of chord; maximum error 0.01859%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
132.7
Angle at maximum lift / drag (°)
9
Minimum Cd
0.006128
Maximum Cl
1.811
Angle at maximum Cl (°)
16
Cd at zero lift
0.006137
Cm at zero angle
-0.03908
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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