Airfoils.Pro
database / Other families / AMSOIL2
CAMBEREDOTHER FAMILIESSELIG-DATABASE

AMSOIL2

Cambered · 12% thick · low-to-mid Re
Compare↓ Download
PROFILEAMSOIL2
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.8% @ 39%c
max camber1.0% @ 50%c
LE radius1.52%c
area upper / chord0.0477
area lower / chord-0.0348
area camber / chord0.0065
TE thickness0.45%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7053-50.21573.3331.13711.672.05820ClAngle 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 0.02531% of chord; maximum error 0.1007%.

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 (°)
11
Minimum Cd
0.007045
Maximum Cl
1.827
Angle at maximum Cl (°)
16
Cd at zero lift
0.007056
Cm at zero angle
-0.03219
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…