Airfoils.Pro
database / MH series / MH 126 25.0%
CAMBEREDMH SERIESSELIG-DATABASETHICK

MH 126 25.0%

Cambered · 25% thick · low-to-mid Re
Compare↓ Download
PROFILEMH 126 25.0%
surfacecamber line
GEOMETRY · AREA METRICS
max thickness25.0% @ 36%c
max camber7.8% @ 45%c
LE radius6.91%c
area upper / chord0.1345
area lower / chord-0.0323
area camber / chord0.0511
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
0.04801-50.62843.3331.20911.671.78920ClAngle 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 0.03041% of chord; maximum error 0.1248%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
50.73
Angle at maximum lift / drag (°)
1
Minimum Cd
0.009356
Maximum Cl
1.644
Angle at maximum Cl (°)
16
Cd at zero lift
—
Cm at zero angle
-0.1387
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…