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

GIIIE

Cambered · 9% thick · low-to-mid Re
Compare↓ Download
PROFILEGIIIE
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.8% @ 45%c
max camber1.2% @ 30%c
LE radius0.85%c
area upper / chord0.0368
area lower / chord-0.0235
area camber / chord0.0067
TE thickness0.04%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7043-50.1653.3331.03411.671.90420ClAngle 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 0.0186% of chord; maximum error 0.1037%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
120.3
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006473
Maximum Cl
1.686
Angle at maximum Cl (°)
16
Cd at zero lift
0.006483
Cm at zero angle
-0.01059
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…