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CAMBEREDHQ SERIESSELIG-DATABASE

HQ 1.0/10 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILEHQ 1.0/10 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.0% @ 35%c
max camber1.0% @ 50%c
LE radius1.09%c
area upper / chord0.0399
area lower / chord-0.0251
area camber / chord0.0074
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.6516-50.21793.3331.08711.671.95720ClAngle 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.

Geometry fit: RMS error 0.01463% of chord; maximum error 0.06712%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
125.5
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006636
Maximum Cl
1.74
Angle at maximum Cl (°)
16
Cd at zero lift
0.00664
Cm at zero angle
-0.03044
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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