Airfoils.Pro
database / Eppler / E1214
CAMBEREDEPPLERSELIG-DATABASETHICK

E1214

Cambered · 20% thick · low-to-mid Re
Compare↓ Download
PROFILEE1214
surfacecamber line
GEOMETRY · AREA METRICS
max thickness19.8% @ 24%c
max camber2.1% @ 31%c
LE radius4.33%c
area upper / chord0.0730
area lower / chord-0.0460
area camber / chord0.0135
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5979-50.11163.3330.82111.671.53120ClAngle 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 0.02854% of chord; maximum error 0.1827%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
108.7
Angle at maximum lift / drag (°)
7
Minimum Cd
0.007507
Maximum Cl
1.353
Angle at maximum Cl (°)
20
Cd at zero lift
0.007509
Cm at zero angle
-0.02506
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…