Airfoils.Pro
database / Research / RHODESG34
CAMBEREDRESEARCHSELIG-DATABASE

RHODESG34

Cambered · 14% thick · low-to-mid Re
Compare↓ Download
PROFILERHODESG34
surfacecamber line
GEOMETRY · AREA METRICS
max thickness14.1% @ 30%c
max camber7.0% @ 30%c
LE radius2.18%c
area upper / chord0.0958
area lower / chord0.0007
area camber / chord0.0483
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
0.02436-50.5993.3331.17411.671.74820ClAngle 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 0.06995% of chord; maximum error 0.3305%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
144.9
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006942
Maximum Cl
1.605
Angle at maximum Cl (°)
8
Cd at zero lift
—
Cm at zero angle
-0.09789
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…