Airfoils.Pro
database / MH series / MH 108 11.98%
CAMBEREDMH SERIESSELIG-DATABASE

MH 108 11.98%

Cambered · 12% thick · low-to-mid Re
Compare↓ Download
PROFILEMH 108 11.98%
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.0% @ 26%c
max camber1.1% @ 21%c
LE radius1.58%c
area upper / chord0.0412
area lower / chord-0.0332
area camber / chord0.0040
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.794-50.094383.3330.982811.671.87120ClAngle 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 0.02199% of chord; maximum error 0.06221%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
118
Angle at maximum lift / drag (°)
11
Minimum Cd
0.00695
Maximum Cl
1.649
Angle at maximum Cl (°)
16
Cd at zero lift
0.006956
Cm at zero angle
0.01859
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…