Airfoils.Pro
database / Drela AG / AG35
CAMBEREDDRELA AGSELIG-DATABASE

AG35

Cambered · 9% thick · low-to-mid Re
Compare↓ Download
PROFILEAG35
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.7% @ 28%c
max camber4.4% @ 26%c
LE radius0.84%c
area upper / chord0.0596
area lower / chord0.0013
area camber / chord0.0304
TE thickness0.25%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2978-50.23963.3330.777111.671.31520ClAngle 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.

The compressibility correction is a low-fidelity estimate, not a resolved shock or compressible CFD solution.

Geometry fit: RMS error 0.01367% of chord; maximum error 0.06359%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
137.7
Angle at maximum lift / drag (°)
4
Minimum Cd
0.006047
Maximum Cl
1.18
Angle at maximum Cl (°)
6
Cd at zero lift
0.006055
Cm at zero angle
-0.05401
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…