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database / HQ series / HQ 2.1/9.5 AIRFOIL
CAMBEREDHQ SERIESSELIG-DATABASE

HQ 2.1/9.5 AIRFOIL

Cambered · 9% thick · low-to-mid Re
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PROFILEHQ 2.1/9.5 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.5% @ 35%c
max camber2.1% @ 55%c
LE radius0.99%c
area upper / chord0.0467
area lower / chord-0.0156
area camber / chord0.0156
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4808-50.37583.3331.23211.672.08920ClAngle 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 0.02167% of chord; maximum error 0.1098%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
138.4
Angle at maximum lift / drag (°)
9
Minimum Cd
0.006533
Maximum Cl
1.875
Angle at maximum Cl (°)
16
Cd at zero lift
0.00654
Cm at zero angle
-0.07093
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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