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CAMBEREDHQ SERIESSELIG-DATABASE

HQ 1.5/10 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILEHQ 1.5/10 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.0% @ 35%c
max camber1.5% @ 50%c
LE radius1.09%c
area upper / chord0.0436
area lower / chord-0.0214
area camber / chord0.0111
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5785-50.27793.3331.13411.671.99120ClAngle 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 0.01455% of chord; maximum error 0.07223%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
129.1
Angle at maximum lift / drag (°)
9
Minimum Cd
0.006619
Maximum Cl
1.777
Angle at maximum Cl (°)
16
Cd at zero lift
0.006625
Cm at zero angle
-0.04564
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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