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HAM-STD HS1-712 AIRFOIL

Cambered · 12% thick · low-to-mid Re
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PROFILEHAM-STD HS1-712 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.0% @ 36%c
max camber4.8% @ 44%c
LE radius1.58%c
area upper / chord0.0794
area lower / chord-0.0123
area camber / chord0.0336
TE thickness1.79%c
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Polars

Preliminary
Combined estimate
0.03366-50.64573.3331.25811.671.8720ClAngle 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 0.01895% of chord; maximum error 0.08004%.

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
150.5
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007719
Maximum Cl
1.717
Angle at maximum Cl (°)
7
Cd at zero lift
—
Cm at zero angle
-0.1918
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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