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HAM-STD HS1-708 AIRFOIL

Cambered · 8% thick · low-to-mid Re
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PROFILEHAM-STD HS1-708 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.9% @ 22%c
max camber4.9% @ 44%c
LE radius0.69%c
area upper / chord0.0617
area lower / chord0.0026
area camber / chord0.0321
TE thickness0.65%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.0504-50.52223.3331.09511.671.66720ClAngle 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 0.009266% of chord; maximum error 0.03142%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
163
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006543
Maximum Cl
1.524
Angle at maximum Cl (°)
7
Cd at zero lift
—
Cm at zero angle
-0.1627
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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