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Airfoil database list (M).

NACA M3 AIRFOIL to MH 102 16.99%

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(m3-il) NACA M3 AIRFOIL

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NACA M3 AIRFOILNACA/Munk M-3 airfoil
Max thickness 11.9% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(m4-il) NACA M4 AIRFOIL

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NACA M4 AIRFOILNACA/Munk M-4 airfoil
Max thickness 6.3% at 30% chord
Max camber 2.2% at 30% chord
Source UIUC Airfoil Coordinates Database

(m5-il) NACA M5 AIRFOIL

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NACA M5 AIRFOILNACA/Munk M-5 airfoil
Max thickness 8.2% at 30.1% chord
Max camber 2.1% at 30.1% chord
Source UIUC Airfoil Coordinates Database

(m6-il) NACA M6 AIRFOIL

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NACA M6 AIRFOILNACA/Munk M-6 airfoil
Max thickness 12% at 30% chord
Max camber 2.2% at 30% chord
Source UIUC Airfoil Coordinates Database

(m665-il) M6 (65%)

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M6 (65%)NACA/Munk M6 (65%)
Max thickness 7.8% at 30% chord
Max camber 1.4% at 30% chord
Source UIUC Airfoil Coordinates Database

(m685-il) M6 (85%)

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M6 (85%)NACA/Munk M6 (85%)
Max thickness 10.2% at 30% chord
Max camber 1.9% at 30% chord
Source UIUC Airfoil Coordinates Database

(m7-il) NACA M7 AIRFOIL

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NACA M7 AIRFOILNACA/Munk M-7 airfoil
Max thickness 6.2% at 40% chord
Max camber 4.9% at 30% chord
Source UIUC Airfoil Coordinates Database

(m8-il) NACA M8 AIRFOIL

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NACA M8 AIRFOILNACA/Munk M-8 airfoil
Max thickness 11.7% at 15% chord
Max camber 8% at 30% chord
Source UIUC Airfoil Coordinates Database

(m9-il) NACA M9 AIRFOIL

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NACA M9 AIRFOILNACA/Munk M-9 airfoil
Max thickness 10.4% at 15% chord
Max camber 7.2% at 30% chord
Source UIUC Airfoil Coordinates Database

(ma409-il) MA409 (original) (modified line 7)

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MA409 (original) (modified line 7)Michael Achterberg MA409 F1C class free flight airfoil (original)
Max thickness 6.8% at 25% chord
Max camber 3.3% at 50% chord
Source UIUC Airfoil Coordinates Database

(ma409sm-il) MA409 (smoothed)

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MA409 (smoothed)Michael Achterberg MA409 F1C class free flight airfoil (smoothed)
Max thickness 6.7% at 23.8% chord
Max camber 3.3% at 49.3% chord
Source UIUC Airfoil Coordinates Database

(marsden-il) Marsden

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MarsdenMarsden airfoil
Max thickness 27.9% at 31.6% chord
Max camber 7.7% at 37.6% chord
Source UIUC Airfoil Coordinates Database

(marske1-il) MARSKE XM-1D AIRFOIL (F14-3.0)

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MARSKE XM-1D AIRFOIL (F14-3.0)Marske XM-1D airfoil (F14-3.0)
Max thickness 14% at 25.1% chord
Max camber 3% at 25.1% chord
Source UIUC Airfoil Coordinates Database

(marske2-il) MARSKE PIONEER IA AIRFOIL (NACA 23112/43012A HYBRID)

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MARSKE PIONEER IA AIRFOIL (NACA 23112/43012A HYBRID)Marske Pioneer IA airfoil (NACA 23112/43012A hybrid)
Max thickness 12.1% at 25% chord
Max camber 2.7% at 15% chord
Source UIUC Airfoil Coordinates Database

(marske3-il) MARSKE PIONEER IID ROOT AIRFOIL (NACA 431012A/24112 HYBRID)

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MARSKE PIONEER IID ROOT AIRFOIL (NACA 431012A/24112 HYBRID)Marske Pioneer IID root airfoil (NACA 43012A/24112 hybrid)
Max thickness 12.1% at 30% chord
Max camber 2.8% at 15% chord
Source UIUC Airfoil Coordinates Database

(marske4-il) MARSKE PIONEER IID TIP AIRFOIL (NACA 431012A*.833 HYBRID)

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MARSKE PIONEER IID TIP AIRFOIL (NACA 431012A*.833 HYBRID)Marske Pioneer IID tip airfoil (NACA 43012A*.833 hybrid)
Max thickness 10.2% at 20% chord
Max camber 2.8% at 15% chord
Source UIUC Airfoil Coordinates Database

(marske5-il) MARSKE MONARCH AIRFOIL (NACA 43012A)

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MARSKE MONARCH AIRFOIL (NACA 43012A)Marske Monarch airfoil (NACA 43012A)
Max thickness 12.2% at 20% chord
Max camber 3.4% at 15% chord
Source UIUC Airfoil Coordinates Database

(marske7-il) RONCZ LOW DRAG FLYING WING AIRFOIL

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RONCZ LOW DRAG FLYING WING AIRFOILRoncz/Marske-7 low drag flying wing airfoil
Max thickness 12.1% at 42.8% chord
Max camber 2.8% at 39.1% chord
Source UIUC Airfoil Coordinates Database

(mb253515sm-il) MB253515 15.0% smoothed

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MB253515 15.0% smoothedMike Bame MB253515 low Reynolds number airfoil
Max thickness 15% at 35% chord
Max camber 2.5% at 37.5% chord
Source UIUC Airfoil Coordinates Database

(mh102-il) MH 102 16.99%

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MH 102  16.99%Martin Hepperle MH 102 for stall controlled wind turbines (root)
Max thickness 17% at 27.7% chord
Max camber 2.8% at 37.6% chord
Source UIUC Airfoil Coordinates Database
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