Airfoils.Pro
database / Other families / ONERA HOR07 AIRFOIL
CAMBEREDOTHER FAMILIESSELIG-DATABASETHIN

ONERA HOR07 AIRFOIL

Cambered · 7% thick · low-to-mid Re
Compare↓ Download
PROFILEONERA HOR07 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.2% @ 25%c
max camber4.5% @ 40%c
LE radius0.57%c
area upper / chord0.0508
area lower / chord0.0053
area camber / chord0.0280
TE thickness0.98%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2931-50.28813.3330.869311.671.4520ClAngle 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 0.01744% of chord; maximum error 0.07836%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
142.4
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006927
Maximum Cl
1.305
Angle at maximum Cl (°)
7
Cd at zero lift
0.007083
Cm at zero angle
-0.1064
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…