Airfoils.Pro
database / Other families / EH 1.0/9.0
CAMBEREDOTHER FAMILIESSELIG-DATABASE

EH 1.0/9.0

Cambered · 9% thick · low-to-mid Re
Compare↓ Download
PROFILEEH 1.0/9.0
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.0% @ 29%c
max camber1.0% @ 26%c
LE radius0.89%c
area upper / chord0.0341
area lower / chord-0.0247
area camber / chord0.0047
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7451-50.13363.3331.01211.671.89120ClAngle 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 0.01136% of chord; maximum error 0.0397%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
120.9
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006543
Maximum Cl
1.671
Angle at maximum Cl (°)
16
Cd at zero lift
0.006554
Cm at zero angle
0.0003429
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…