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CAMBEREDRESEARCHSELIG-DATABASETHICK

RONCZ R1145MS AIRFOIL

Cambered · 19% thick · low-to-mid Re
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PROFILERONCZ R1145MS AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness18.8% @ 35%c
max camber4.4% @ 49%c
LE radius3.89%c
area upper / chord0.0968
area lower / chord-0.0348
area camber / chord0.0310
TE thickness0.31%c
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Polars

Preliminary
Combined estimate
-0.2994-50.35983.3331.01911.671.67820ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 0 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 0.01968% of chord; maximum error 0.07147%.

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

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
107.5
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007629
Maximum Cl
1.513
Angle at maximum Cl (°)
10
Cd at zero lift
0.00763
Cm at zero angle
-0.1019
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…