Airfoils.Pro
database / MH series / MH 18 11.16%
CAMBEREDMH SERIESSELIG-DATABASE

MH 18 11.16%

Cambered · 11% thick · low-to-mid Re
Compare↓ Download
PROFILEMH 18 11.16%
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.1% @ 34%c
max camber2.8% @ 38%c
LE radius1.37%c
area upper / chord0.0535
area lower / chord-0.0208
area camber / chord0.0164
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6419-50.030933.3330.703711.671.37720ClAngle 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 0.01869% of chord; maximum error 0.06303%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
129.4
Angle at maximum lift / drag (°)
7
Minimum Cd
0.0063
Maximum Cl
1.208
Angle at maximum Cl (°)
9
Cd at zero lift
0.006301
Cm at zero angle
-0.01297
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…