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CAMBEREDHQ SERIESSELIG-DATABASETHIN

HQ 1.0/8 AIRFOIL

Cambered · 8% thick · low-to-mid Re
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PROFILEHQ 1.0/8 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.0% @ 35%c
max camber1.0% @ 50%c
LE radius0.70%c
area upper / chord0.0334
area lower / chord-0.0186
area camber / chord0.0074
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.6474-50.21623.3331.0811.671.94420ClAngle 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 0.0129% of chord; maximum error 0.06391%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
123.1
Angle at maximum lift / drag (°)
9
Minimum Cd
0.006341
Maximum Cl
1.728
Angle at maximum Cl (°)
16
Cd at zero lift
0.006347
Cm at zero angle
-0.03079
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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