Airfoils.Pro
database / MH series / MH 110 10.01%
CAMBEREDMH SERIESSELIG-DATABASE

MH 110 10.01%

Cambered · 10% thick · low-to-mid Re
Compare↓ Download
PROFILEMH 110 10.01%
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.0% @ 24%c
max camber1.1% @ 15%c
LE radius1.10%c
area upper / chord0.0330
area lower / chord-0.0292
area camber / chord0.0019
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.8466-50.048363.3330.943311.671.83820ClAngle 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 0.01603% of chord; maximum error 0.04396%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
113.5
Angle at maximum lift / drag (°)
11
Minimum Cd
0.006649
Maximum Cl
1.615
Angle at maximum Cl (°)
16
Cd at zero lift
0.006664
Cm at zero angle
0.0364
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…