Airfoils.Pro
database / Drela AG / AG52
CAMBEREDDRELA AGSELIG-DATABASE

AG52

Cambered · 8% thick · low-to-mid Re
Compare↓ Download
PROFILEAG52
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.4% @ 28%c
max camber1.8% @ 41%c
LE radius0.77%c
area upper / chord0.0400
area lower / chord-0.0155
area camber / chord0.0122
TE thickness0.04%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5703-50.29673.3331.16411.672.03120ClAngle 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 0.008781% of chord; maximum error 0.02797%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
130.9
Angle at maximum lift / drag (°)
9
Minimum Cd
0.006475
Maximum Cl
1.814
Angle at maximum Cl (°)
16
Cd at zero lift
0.006478
Cm at zero angle
-0.04575
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…