Airfoils.Pro
database / Other families / NPL 9510 AIRFOIL
CAMBEREDOTHER FAMILIESSELIG-DATABASE

NPL 9510 AIRFOIL

Cambered · 11% thick · low-to-mid Re
Compare↓ Download
PROFILENPL 9510 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.1% @ 33%c
max camber1.6% @ 79%c
LE radius1.35%c
area upper / chord0.0376
area lower / chord-0.0345
area camber / chord0.0016
TE thickness0.49%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5889-50.33543.3331.2611.672.18420ClAngle 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 0.02197% of chord; maximum error 0.05934%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
137.4
Angle at maximum lift / drag (°)
10
Minimum Cd
0.007199
Maximum Cl
1.953
Angle at maximum Cl (°)
17
Cd at zero lift
0.00723
Cm at zero angle
-0.09221
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…