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database / HQ series / HQ 3.0/10 AIRFOIL
CAMBEREDHQ SERIESSELIG-DATABASE

HQ 3.0/10 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILEHQ 3.0/10 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.0% @ 35%c
max camber3.0% @ 50%c
LE radius1.10%c
area upper / chord0.0546
area lower / chord-0.0104
area camber / chord0.0221
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.3207-50.26923.3330.859211.671.44920ClAngle 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 0.0151% of chord; maximum error 0.06958%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
148.9
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006126
Maximum Cl
1.302
Angle at maximum Cl (°)
7
Cd at zero lift
0.006173
Cm at zero angle
-0.09982
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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