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database / HQ series / HQ 2.0/10 AIRFOIL
CAMBEREDHQ SERIESSELIG-DATABASE

HQ 2.0/10 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILEHQ 2.0/10 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.0% @ 35%c
max camber2.0% @ 45%c
LE radius1.09%c
area upper / chord0.0473
area lower / chord-0.0178
area camber / chord0.0148
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.4731-50.11873.3330.710411.671.30220ClAngle 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 0.01434% of chord; maximum error 0.07156%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
136.1
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006062
Maximum Cl
1.154
Angle at maximum Cl (°)
7
Cd at zero lift
0.006075
Cm at zero angle
-0.06693
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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