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TsAGI 12% AIRFOIL

Cambered · 12% thick · low-to-mid Re
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PROFILETsAGI 12% AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.9% @ 30%c
max camber2.0% @ 30%c
LE radius1.56%c
area upper / chord0.0508
area lower / chord-0.0313
area camber / chord0.0098
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.6842-5-0.050023.3330.584111.671.21820ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 1 contributing CFD observations. History windows remain observations, not separate solver runs or automatically converged points.

Model uncertainty is conditional on the stated assumptions and has not been calibrated for this condition. It is not a validated accuracy guarantee.

Geometry fit: RMS error 0.05337% of chord; maximum error 0.252%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10 · Polar model progressive-polar-gp-v2

  • · Converged

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
78.6
Angle at maximum lift / drag (°)
7
Minimum Cd
0.009649
Maximum Cl
1.06
Angle at maximum Cl (°)
9
Cd at zero lift
0.009673
Cm at zero angle
0.003525
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…