Airfoils.Pro
database / Wortmann FX / FX 63-158 AIRFOIL
CAMBEREDSELIG-DATABASETHICKWORTMANN FX

FX 63-158 AIRFOIL

Cambered · 16% thick · low-to-mid Re
Compare↓ Download
PROFILEFX 63-158 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.8% @ 35%c
max camber3.8% @ 37%c
LE radius2.75%c
area upper / chord0.0778
area lower / chord-0.0196
area camber / chord0.0291
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.03932-50.58413.3331.20811.671.83120ClAngle 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.

The compressibility correction is a low-fidelity estimate, not a resolved shock or compressible CFD solution.

Geometry fit: RMS error 0.0215% of chord; maximum error 0.08595%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
156.3
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007232
Maximum Cl
1.675
Angle at maximum Cl (°)
8
Cd at zero lift
—
Cm at zero angle
-0.1718
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…