Airfoils.Pro
database / Research / RG15A111
CAMBEREDRESEARCHSELIG-DATABASE

RG15A111

Cambered · 11% thick · low-to-mid Re
Compare↓ Download
PROFILERG15A111
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.0% @ 31%c
max camber1.8% @ 39%c
LE radius1.33%c
area upper / chord0.0500
area lower / chord-0.0232
area camber / chord0.0134
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4662-50.12443.3330.715111.671.30620ClAngle 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 0.0178% of chord; maximum error 0.0942%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
134.4
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006322
Maximum Cl
1.158
Angle at maximum Cl (°)
7
Cd at zero lift
0.006323
Cm at zero angle
-0.06902
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…