Airfoils.Pro
database / Eppler / E193 (10.22%)
CAMBEREDEPPLERSELIG-DATABASE

E193 (10.22%)

Cambered · 10% thick · low-to-mid Re
Compare↓ Download
PROFILEE193 (10.22%)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.2% @ 31%c
max camber3.6% @ 40%c
LE radius1.15%c
area upper / chord0.0562
area lower / chord-0.0101
area camber / chord0.0230
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3641-50.26233.3330.888711.671.51520ClAngle 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 0.01784% of chord; maximum error 0.07594%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
146
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006177
Maximum Cl
1.358
Angle at maximum Cl (°)
8
Cd at zero lift
0.006185
Cm at zero angle
-0.08633
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…