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Airfoil database list (V).

BOEING VERTOL V13006-.7 AIRFOIL to BOEING-VERTOL VR-9 AIRFOIL

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(v13006-il) BOEING VERTOL V13006-.7 AIRFOIL

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BOEING VERTOL V13006-.7 AIRFOILBoeing-Vertol V13006-.7 rotorcraft airfoil
Max thickness 6% at 30.2% chord
Max camber 0.9% at 20.2% chord
Source UIUC Airfoil Coordinates Database

(v13009-il) BOEING VERTOL V(1.95)3009-1.25 AIRFOIL

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BOEING VERTOL V(1.95)3009-1.25 AIRFOILBoeing-Vertol V(1.9)3006-1.25 rotorcraft airfoil
Max thickness 9% at 30.1% chord
Max camber 1.3% at 20.1% chord
Source UIUC Airfoil Coordinates Database

(v23010-il) BOEING-VERTOL V23010-1.58 AIRFOIL

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BOEING-VERTOL V23010-1.58 AIRFOILBoeing-Vertol V23010-1.58 rotorcraft airfoil
Max thickness 10.2% at 30% chord
Max camber 1.8% at 15% chord
Source UIUC Airfoil Coordinates Database

(v43012-il) BOEING VERTOL V43012-1.58 AIRFOIL

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BOEING VERTOL V43012-1.58 AIRFOILBoeing-Vertol V43012-1.58 rotorcraft airfoil
Max thickness 12% at 32% chord
Max camber 3.7% at 15% chord
Source UIUC Airfoil Coordinates Database

(v43015-il) BOEING VERTOL V43015-2.48 AIRFOIL

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BOEING VERTOL V43015-2.48 AIRFOILBoeing-Vertol V43015-2.48 rotorcraft airfoil
Max thickness 15% at 30% chord
Max camber 3.7% at 15% chord
Source UIUC Airfoil Coordinates Database

(vr1-il) BOEING-VERTOL VR-1 AIRFOIL

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BOEING-VERTOL VR-1 AIRFOILBoeing-Vertol VR-1 rotorcraft airfoil
Max thickness 11% at 35.3% chord
Max camber 1.5% at 43.3% chord
Source UIUC Airfoil Coordinates Database

(vr11x-il) BOEING-VERTOL VR-11X AIRFOIL

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BOEING-VERTOL VR-11X AIRFOILBoeing-Vertol/NASA/Dadone VR-11X transonic rotorcraft airfoil
Max thickness 11% at 40% chord
Max camber 2.4% at 25% chord
Source UIUC Airfoil Coordinates Database

(vr12-il) BOEING-VERTOL VR-12 AIRFOIL

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BOEING-VERTOL VR-12 AIRFOILBoeing-Vertol/Dadone VR-12 rotorcraft airfoil
Max thickness 10.6% at 35% chord
Max camber 2.3% at 20% chord
Source UIUC Airfoil Coordinates Database

(vr13-il) BOEING-VERTOL VR-13 AIRFOIL

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BOEING-VERTOL VR-13 AIRFOILBoeing-Vertol/Dadone VR-13 rotorcraft airfoil
Max thickness 9.5% at 35% chord
Max camber 2% at 20% chord
Source UIUC Airfoil Coordinates Database

(vr14-il) BOEING-VERTOL VR-14 AIRFOIL

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BOEING-VERTOL VR-14 AIRFOILBoeing-Vertol/Dadone VR-14 rotorcraft airfoil
Max thickness 8% at 35% chord
Max camber 1.7% at 20% chord
Source UIUC Airfoil Coordinates Database

(vr15-il) BOEING-VERTOL VR-15 AIRFOIL

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BOEING-VERTOL VR-15 AIRFOILBoeing-Vertol/Dadone VR-15 transonic rotorcraft airfoil
Max thickness 8% at 35% chord
Max camber 1.3% at 20% chord
Source UIUC Airfoil Coordinates Database

(vr5-il) BOEING-VERTOL VR-5 AIRFOIL

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BOEING-VERTOL VR-5 AIRFOILBoeing-Vertol VR-5 rotorcraft airfoil
Max thickness 12% at 35% chord
Max camber 3.4% at 35% chord
Source UIUC Airfoil Coordinates Database

(vr7-il) BOEING-VERTOL VR-7 AIRFOIL

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BOEING-VERTOL VR-7 AIRFOILBoeing-Vertol VR-7 rotorcraft airfoil
Max thickness 12% at 33% chord
Max camber 3.1% at 33% chord
Source UIUC Airfoil Coordinates Database

(vr7b-il) BOEING-VERTOL VR-7 AIRFOIL WITH TAB

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BOEING-VERTOL VR-7 AIRFOIL WITH TABBoeing-Vertol VR-7 rotorcraft airfoil with tab
Max thickness 12% at 33% chord
Max camber 3% at 29% chord
Source UIUC Airfoil Coordinates Database

(vr8-il) BOEING-VERTOL VR-8 AIRFOIL

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BOEING-VERTOL VR-8 AIRFOILBoeing-Vertol VR-8 rotorcraft airfoil
Max thickness 8.2% at 35% chord
Max camber 1.3% at 35% chord
Source UIUC Airfoil Coordinates Database

(vr8b-il) BOEING-VERTOL VR-8 AIRFOIL WITH TAB

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BOEING-VERTOL VR-8 AIRFOIL WITH TABBoeing-Vertol VR-8 rotorcraft airfoil with tab
Max thickness 8.2% at 35% chord
Max camber 1.2% at 35% chord
Source UIUC Airfoil Coordinates Database

(vr9-il) BOEING-VERTOL VR-9 AIRFOIL

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BOEING-VERTOL VR-9 AIRFOILBoeing-Vertol VR-9 rotorcraft airfoil
Max thickness 6.1% at 35% chord
Max camber 0.3% at 35% chord
Source UIUC Airfoil Coordinates Database
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