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CAMBEREDDRELA AGSELIG-DATABASETHIN

AG09

Cambered · 5% thick · low-to-mid Re
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PROFILEAG09
surfacecamber line
GEOMETRY · AREA METRICS
max thickness4.9% @ 18%c
max camber1.9% @ 33%c
LE radius0.26%c
area upper / chord0.0276
area lower / chord-0.0037
area camber / chord0.0119
TE thickness0.20%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6193-50.25363.3331.12711.671.99920ClAngle 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 0.003889% of chord; maximum error 0.021%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
130.2
Angle at maximum lift / drag (°)
9
Minimum Cd
0.006067
Maximum Cl
1.781
Angle at maximum Cl (°)
16
Cd at zero lift
0.00609
Cm at zero angle
-0.03274
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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