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Airfoil database list (N).

NASA/LANGLEY NLF(1)-0215F AIRFOIL to NPL AIRFOIL FROM ARC CP 1372

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(nlf0215f-il) NASA/LANGLEY NLF(1)-0215F AIRFOIL

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NASA/LANGLEY NLF(1)-0215F AIRFOILNASA/Langley/Somers NLF(1)-0215F natural laminar flow airfoil
Max thickness 15% at 37.7% chord
Max camber 4% at 42.3% chord
Source UIUC Airfoil Coordinates Database

(nlf1015-il) NASA NLF1015

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NASA  NLF1015NASA/Langley/Somers-Maughmer NLF(1)-1015 natural laminar flow airfoil
Max thickness 15% at 39.8% chord
Max camber 4.3% at 62.8% chord
Source UIUC Airfoil Coordinates Database

(nlf414f-il) NASA/LANGLEY NLF 0414F AIRFOIL

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NASA/LANGLEY NLF 0414F AIRFOILNASA/Langley/Viken NLF(1)-0414F natural laminar flow airfoil
Max thickness 14.2% at 46.6% chord
Max camber 2.4% at 53.7% chord
Source UIUC Airfoil Coordinates Database

(nlf415-il) NASA/LANGLEY NLF(2)-0415 AIRFOIL

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NASA/LANGLEY NLF(2)-0415 AIRFOILNASA/Langley-DFVLR/Somers(NASA)-Horstmann(DFVLR) NLF(2)-0415 natural laminar flow airfoil
Max thickness 15% at 47.1% chord
Max camber 3% at 71.4% chord
Source UIUC Airfoil Coordinates Database

(nlf416-il) NASA/LANGLEY NLF(1)-0416 AIRFOIL

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NASA/LANGLEY NLF(1)-0416 AIRFOILNASA/Langley/Somers NLF(1)-0416 natural laminar flow airfoil
Max thickness 15.9% at 30.4% chord
Max camber 2.5% at 34.8% chord
Source UIUC Airfoil Coordinates Database

(nlr1t-il) NLR-1T AIRFOIL

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NLR-1T AIRFOILBell/NASA/NLR NLR-1T rotorcraft airfoil
Max thickness 8.7% at 38.3% chord
Max camber 1.3% at 22.3% chord
Source UIUC Airfoil Coordinates Database

(nlr7301-il) NLR-7301 AIRFOIL

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NLR-7301 AIRFOILNLR NLR-7301 transonic airfoil
Max thickness 16.5% at 35% chord
Max camber 1.7% at 75% chord
Source UIUC Airfoil Coordinates Database

(nn7mk20-il) NN7 MK20

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NN7 MK20NN7 MK20 airfoil
Max thickness 16.9% at 37.1% chord
Max camber 3% at 59.8% chord
Source UIUC Airfoil Coordinates Database

(npl9510-il) NPL 9510 AIRFOIL

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NPL 9510 AIRFOILNPL 9510 transonic airfoil
Max thickness 11.1% at 32% chord
Max camber 1.6% at 80% chord
Source UIUC Airfoil Coordinates Database

(npl9615-il) NPL 9615 AIRFOIL

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NPL 9615 AIRFOILNPL 9615 rotorcraft airfoil
Max thickness 11.3% at 34.2% chord
Max camber 1% at 19.8% chord
Source UIUC Airfoil Coordinates Database

(npl9626-il) NPL 9626 AIRFOIL

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NPL 9626 AIRFOILNPL 9626 rotorcraft airfoil
Max thickness 12.1% at 30.9% chord
Max camber 0.7% at 30.9% chord
Source UIUC Airfoil Coordinates Database

(npl9627-il) NPL 9627 AIRFOIL

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NPL 9627 AIRFOILNPL 9627 rotorcraft airfoil
Max thickness 12.2% at 31% chord
Max camber 0.9% at 40.4% chord
Source UIUC Airfoil Coordinates Database

(npl9660-il) NPL 9660 AIRFOIL

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NPL 9660 AIRFOILNPL 9660 rotorcraft airfoil
Max thickness 11.3% at 34.2% chord
Max camber 1% at 19.8% chord
Source UIUC Airfoil Coordinates Database

(nplx-il) NPL AIRFOIL FROM ARC CP 1372

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NPL AIRFOIL FROM ARC CP 1372NPL transonic airfoil FROM ARC CP 1372
Max thickness 10.7% at 35.8% chord
Max camber 1.1% at 73.7% chord
Source UIUC Airfoil Coordinates Database
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