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TsAGI 8% AIRFOIL

Cambered · 8% thick · low-to-mid Re
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PROFILETsAGI 8% AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.9% @ 30%c
max camber1.3% @ 30%c
LE radius0.70%c
area upper / chord0.0339
area lower / chord-0.0208
area camber / chord0.0065
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7076-5-0.1093.3330.489511.671.08820ClAngle 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 0.04098% of chord; maximum error 0.1943%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
113.9
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005919
Maximum Cl
0.9385
Angle at maximum Cl (°)
8
Cd at zero lift
0.005928
Cm at zero angle
0.002757
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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