Airfoils.Pro
database / MH series / MH 46 11.39%
CAMBEREDMH SERIESSELIG-DATABASE

MH 46 11.39%

Cambered · 11% thick · low-to-mid Re
Compare↓ Download
PROFILEMH 46 11.39%
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.3% @ 27%c
max camber1.9% @ 35%c
LE radius1.42%c
area upper / chord0.0417
area lower / chord-0.0250
area camber / chord0.0083
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.8368-5-0.13873.3330.559411.671.25720ClAngle 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 0.02081% of chord; maximum error 0.08822%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
119.7
Angle at maximum lift / drag (°)
7
Minimum Cd
0.00623
Maximum Cl
1.083
Angle at maximum Cl (°)
9
Cd at zero lift
0.006246
Cm at zero angle
0.02915
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…