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RG 8 AIRFOIL

Cambered · 11% thick · low-to-mid Re
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PROFILERG 8 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.8% @ 32%c
max camber2.2% @ 61%c
LE radius1.28%c
area upper / chord0.0519
area lower / chord-0.0189
area camber / chord0.0165
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3451-50.2423.3330.829211.671.41620ClAngle 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 0.01703% of chord; maximum error 0.08521%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
142.7
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006324
Maximum Cl
1.27
Angle at maximum Cl (°)
7
Cd at zero lift
0.006332
Cm at zero angle
-0.1062
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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