Airfoils.Pro
database / Other families / DF102
CAMBEREDOTHER FAMILIESSELIG-DATABASE

DF102

Cambered · 11% thick · low-to-mid Re
Compare↓ Download
PROFILEDF102
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.0% @ 29%c
max camber2.3% @ 43%c
LE radius1.33%c
area upper / chord0.0527
area lower / chord-0.0216
area camber / chord0.0156
TE thickness0.01%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5011-50.10713.3330.715211.671.32320ClAngle 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 0.02122% of chord; maximum error 0.1238%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
135.2
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006388
Maximum Cl
1.171
Angle at maximum Cl (°)
8
Cd at zero lift
0.006396
Cm at zero angle
-0.05377
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…