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Airfoil database list (M).

NACA-M1 AIRFOIL to NACA M27 AIRFOIL

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(m1-il) NACA-M1 AIRFOIL

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NACA-M1 AIRFOILNACA/Munk M-1 airfoil
Max thickness 6.2% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(m10-il) NACA M10 AIRFOIL

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NACA M10 AIRFOILNACA/Munk M-10 airfoil
Max thickness 6.2% at 30% chord
Max camber 1.9% at 30% chord
Source UIUC Airfoil Coordinates Database

(m11-il) NACA M11 AIRFOIL

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NACA M11 AIRFOILNACA/Munk M-11 airfoil
Max thickness 8.2% at 30% chord
Max camber 1.9% at 30% chord
Source UIUC Airfoil Coordinates Database

(m12-il) NACA M12 AIRFOIL

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NACA M12 AIRFOILNACA/Munk M-12 airfoil
Max thickness 11.9% at 30% chord
Max camber 2% at 30% chord
Source UIUC Airfoil Coordinates Database

(m13-il) NACA M13 AIRFOIL

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NACA M13 AIRFOILNACA/Munk M-13 airfoil
Max thickness 6.2% at 30% chord
Max camber 3.8% at 30% chord
Source UIUC Airfoil Coordinates Database

(m14-il) NACA M14 AIRFOIL

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NACA M14 AIRFOILNACA/Munk M-14 airfoil
Max thickness 8.1% at 30% chord
Max camber 3.9% at 30% chord
Source UIUC Airfoil Coordinates Database

(m15-il) NACA M15 AIRFOIL

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NACA M15 AIRFOILNACA/Munk M-15 airfoil
Max thickness 12% at 30% chord
Max camber 3.8% at 30% chord
Source UIUC Airfoil Coordinates Database

(m16-il) NACA M16 AIRFOIL

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NACA M16 AIRFOILNACA/Munk M-16 airfoil
Max thickness 6.2% at 30% chord
Max camber 4.1% at 30% chord
Source UIUC Airfoil Coordinates Database

(m17-il) NACA M17 AIRFOIL

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NACA M17 AIRFOILNACA/Munk M-17 airfoil
Max thickness 8.1% at 40% chord
Max camber 4.1% at 30% chord
Source UIUC Airfoil Coordinates Database

(m18-il) NACA M18 AIRFOIL

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NACA M18 AIRFOILNACA/Munk M-18 airfoil
Max thickness 12% at 30% chord
Max camber 4.1% at 30% chord
Source UIUC Airfoil Coordinates Database

(m19-il) NACA M19 AIRFOIL

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NACA M19 AIRFOILNACA/Munk M-19 airfoil
Max thickness 6.2% at 30% chord
Max camber 6% at 30% chord
Source UIUC Airfoil Coordinates Database

(m2-il) NACA M2 AIRFOIL

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NACA M2 AIRFOILNACA/Munk M-2 airfoil
Max thickness 8% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(m20-il) NACA M20 AIRFOIL

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NACA M20 AIRFOILNACA/Munk M-20 airfoil
Max thickness 8.2% at 30% chord
Max camber 6.1% at 30% chord
Source UIUC Airfoil Coordinates Database

(m21-il) NACA M21 AIRFOIL

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NACA M21 AIRFOILNACA/Munk M-21 airfoil
Max thickness 12% at 30% chord
Max camber 6% at 30% chord
Source UIUC Airfoil Coordinates Database

(m22-il) NACA M22 AIRFOIL

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NACA M22 AIRFOILNACA/Munk M-22 airfoil
Max thickness 6.3% at 30% chord
Max camber 6.3% at 30% chord
Source UIUC Airfoil Coordinates Database

(m23-il) NACA M23 AIRFOIL

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NACA M23 AIRFOILNACA/Munk M-23 airfoil
Max thickness 8.1% at 30.1% chord
Max camber 6.4% at 30.1% chord
Source UIUC Airfoil Coordinates Database

(m24-il) NACA M24 AIRFOIL

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NACA M24 AIRFOILNACA/Munk M-24 airfoil
Max thickness 12% at 30.1% chord
Max camber 6.3% at 30.1% chord
Source UIUC Airfoil Coordinates Database

(m25-il) NACA M25 AIRFOIL

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NACA M25 AIRFOILNACA/Munk M-25 airfoil
Max thickness 6.3% at 30% chord
Max camber 8.2% at 30% chord
Source UIUC Airfoil Coordinates Database

(m26-il) NACA M26 AIRFOIL

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NACA M26 AIRFOILNACA/Munk M-26 airfoil
Max thickness 8.3% at 40% chord
Max camber 8.3% at 30% chord
Source UIUC Airfoil Coordinates Database

(m27-il) NACA M27 AIRFOIL

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NACA M27 AIRFOILNACA/Munk M-27 airfoil
Max thickness 12% at 30.1% chord
Max camber 8.4% at 30.1% chord
Source UIUC Airfoil Coordinates Database
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