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CAMBEREDDRELA AGSELIG-DATABASETHIN

AG11

Cambered · 6% thick · low-to-mid Re
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PROFILEAG11
surfacecamber line
GEOMETRY · AREA METRICS
max thickness5.8% @ 26%c
max camber2.3% @ 29%c
LE radius0.37%c
area upper / chord0.0348
area lower / chord-0.0046
area camber / chord0.0151
TE thickness0.23%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5818-50.30263.3331.18711.672.07120ClAngle 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 0.01091% of chord; maximum error 0.04415%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
134
Angle at maximum lift / drag (°)
9
Minimum Cd
0.006249
Maximum Cl
1.85
Angle at maximum Cl (°)
16
Cd at zero lift
0.006292
Cm at zero angle
-0.0348
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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