Airfoils.Pro
database / Other families / Dayton-Wright 6
CAMBEREDOTHER FAMILIESSELIG-DATABASE

Dayton-Wright 6

Cambered · 14% thick · low-to-mid Re
Compare↓ Download
PROFILEDayton-Wright 6
surfacecamber line
GEOMETRY · AREA METRICS
max thickness13.6% @ 30%c
max camber7.2% @ 30%c
LE radius2.04%c
area upper / chord0.0968
area lower / chord0.0025
area camber / chord0.0496
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.07221-50.53923.3331.15111.671.76220ClAngle 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 0.06652% of chord; maximum error 0.3525%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
130
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006928
Maximum Cl
1.609
Angle at maximum Cl (°)
11
Cd at zero lift
—
Cm at zero angle
-0.08287
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…