Airfoils.Pro
database / Eppler / E184 (8.33%)
CAMBEREDEPPLERSELIG-DATABASE

E184 (8.33%)

Cambered · 8% thick · low-to-mid Re
Compare↓ Download
PROFILEE184 (8.33%)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.3% @ 32%c
max camber1.2% @ 36%c
LE radius0.76%c
area upper / chord0.0313
area lower / chord-0.0214
area camber / chord0.0049
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.8342-50.040773.3330.915711.671.79120ClAngle 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.

Geometry fit: RMS error 0.01453% of chord; maximum error 0.07747%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
112.1
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006423
Maximum Cl
1.572
Angle at maximum Cl (°)
16
Cd at zero lift
0.006442
Cm at zero angle
0.02572
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…