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CAMBEREDOTHER FAMILIESSELIG-DATABASETHIN

Eh 1.0/7.0

Cambered · 7% thick · low-to-mid Re
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PROFILEEh 1.0/7.0
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.0% @ 29%c
max camber1.0% @ 26%c
LE radius0.54%c
area upper / chord0.0277
area lower / chord-0.0182
area camber / chord0.0047
TE thickness0.00%c
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Polars

Preliminary
Combined estimate
-0.7246-5-0.12753.3330.469611.671.06720ClAngle 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 0.008982% of chord; maximum error 0.03336%.

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
117.8
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005704
Maximum Cl
0.9174
Angle at maximum Cl (°)
17
Cd at zero lift
0.005708
Cm at zero angle
0.0001777
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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