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Airfoil database list (M).

MH 104 15.28% to MH 23 8%

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(mh104-il) MH 104 15.28%

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MH 104  15.28%Martin Hepperle MH 104 for stall controlled wind turbines
Max thickness 15.2% at 26.4% chord
Max camber 1.9% at 31.1% chord
Source UIUC Airfoil Coordinates Database

(mh106-il) MH 106 13.07%

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MH 106  13.07%Martin Hepperle MH 106 for stall controlled wind turbines
Max thickness 13.1% at 27.4% chord
Max camber 0.9% at 27.4% chord
Source UIUC Airfoil Coordinates Database

(mh108-il) MH 108 11.98%

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MH 108  11.98%Martin Hepperle MH 108 for stall controlled wind turbines
Max thickness 11.9% at 22.8% chord
Max camber 1% at 22.8% chord
Source UIUC Airfoil Coordinates Database

(mh110-il) MH 110 10.01%

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MH 110  10.01%Martin Hepperle MH 110 for stall controlled wind turbines (tip)
Max thickness 10% at 23.9% chord
Max camber 1% at 15.8% chord
Source UIUC Airfoil Coordinates Database

(mh112-il) MH 112 Airfoil

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MH 112  AirfoilMartin Hepperle MH 112 for a propeller for ultralight (root)
Max thickness 16.2% at 31.8% chord
Max camber 6.7% at 48.5% chord
Source UIUC Airfoil Coordinates Database

(mh113-il) MH 113 14.62%

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MH 113  14.62%Martin Hepperle MH 113 for a propeller for ultralight
Max thickness 14.7% at 29.7% chord
Max camber 6.4% at 47.7% chord
Source UIUC Airfoil Coordinates Database

(mh114-il) MH 114 13.02%

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MH 114  13.02%Martin Hepperle MH 114 for a propeller for ultralight
Max thickness 13% at 28.1% chord
Max camber 6.4% at 50% chord
Source UIUC Airfoil Coordinates Database

(mh115-il) MH 115 11.06%

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MH 115  11.06%Martin Hepperle MH 115 for a propeller for ultralight
Max thickness 11.1% at 29.8% chord
Max camber 5.5% at 46% chord
Source UIUC Airfoil Coordinates Database

(mh116-il) MH 116 9.84%

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MH 116  9.84%Martin Hepperle MH 116 for a propeller for ultralight
Max thickness 9.9% at 32.4% chord
Max camber 4.1% at 46.4% chord
Source UIUC Airfoil Coordinates Database

(mh117-il) MH 117 9.8%

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MH 117  9.8%Martin Hepperle MH 117 for a propeller for ultralight (tip)
Max thickness 9.8% at 29.1% chord
Max camber 2.7% at 44.6% chord
Source UIUC Airfoil Coordinates Database

(mh120-il) MH 120 11.57%

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MH 120  11.57%Martin Hepperle MH 120 for tip section of a propeller
Max thickness 11.6% at 34.7% chord
Max camber 2.2% at 44.2% chord
Source UIUC Airfoil Coordinates Database

(mh121-il) MH 121 8.76%

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MH 121  8.76%Martin Hepperle MH 121 for tip section of a propeller
Max thickness 8.8% at 37.9% chord
Max camber 3% at 62.2% chord
Source UIUC Airfoil Coordinates Database

(mh122-il) MH 122 9.32%

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MH 122  9.32%Martin Hepperle MH 122 for tip section of a propeller
Max thickness 9.3% at 37.6% chord
Max camber 3.4% at 64.3% chord
Source UIUC Airfoil Coordinates Database

(mh150-il) MH 150 23.89%

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MH 150  23.89%Martin Hepperle MH 150 for marine ruddershaft for torque reduction (schottel units)
Max thickness 23.9% at 27.2% chord
Max camber 4.5% at 53.8% chord
Source UIUC Airfoil Coordinates Database

(mh18-il) MH 18 11.16%

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MH 18  11.16%Martin Hepperle MH 18 for F3D Pylon Racing
Max thickness 11.1% at 36.8% chord
Max camber 2.7% at 42.1% chord
Source UIUC Airfoil Coordinates Database

(mh20-il) MH 20 9.01%

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MH 20  9.01%Martin Hepperle MH 20 for F3D Pylon Racing
Max thickness 9% at 32.2% chord
Max camber 1.9% at 37.3% chord
Source UIUC Airfoil Coordinates Database

(mh200-il) MH 200 12.97%

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MH 200  12.97%Martin Hepperle MH 200 for a canard airplane (main wing)
Max thickness 13% at 39.5% chord
Max camber 2.1% at 49.8% chord
Source UIUC Airfoil Coordinates Database

(mh201-il) MH 201 13.08%

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MH 201  13.08%Martin Hepperle MH 201 for a canard airplane (canard)
Max thickness 13% at 38.1% chord
Max camber 2.5% at 48.3% chord
Source UIUC Airfoil Coordinates Database

(mh22-il) MH 22 7.2%

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MH 22  7.2%Martin Hepperle MH 22 for F3D Pylon Racing
Max thickness 7.2% at 27% chord
Max camber 1.8% at 37% chord
Source UIUC Airfoil Coordinates Database

(mh23-il) MH 23 8%

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MH 23  8%Martin Hepperle MH 23 for F3D Pylon Racing (extended laminar flow)
Max thickness 8% at 37.5% chord
Max camber 1.2% at 42.7% chord
Source UIUC Airfoil Coordinates Database
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