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

GIIIJ

Cambered · 8% thick · low-to-mid Re
Compare↓ Download
PROFILEGIIIJ
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.5% @ 35%c
max camber1.4% @ 26%c
LE radius0.79%c
area upper / chord0.0381
area lower / chord-0.0208
area camber / chord0.0087
TE thickness0.04%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6744-50.21123.3331.09711.671.98220ClAngle 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 0.0242% of chord; maximum error 0.1149%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
130.6
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006411
Maximum Cl
1.761
Angle at maximum Cl (°)
16
Cd at zero lift
0.006414
Cm at zero angle
-0.01734
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…