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Airfoil database list (F).

FX 66-17AII-182 AIRFOIL to FX 71-L-150/20 AIRFOIL

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(fx6617a2-il) FX 66-17AII-182 AIRFOIL

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FX 66-17AII-182 AIRFOILWortmann FX 66-17AII-182 airfoil
Max thickness 18.2% at 33.9% chord
Max camber 3.8% at 37.1% chord
Source UIUC Airfoil Coordinates Database

(fx6617ai-il) WORTMANN FX 66-17AII-182 AIRFOIL (AS TESTED AT NASA)

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WORTMANN FX 66-17AII-182 AIRFOIL (AS TESTED AT NASA)Wortmann FX 66-17AII-182 airfoil (as tested at NASA)
Max thickness 18.8% at 35.3% chord
Max camber 3.7% at 40.2% chord
Source UIUC Airfoil Coordinates Database

(fx66182-il) FX 66-182 AIRFOIL

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FX 66-182 AIRFOILWortmann FX 66-182 airfoil
Max thickness 18.2% at 33.9% chord
Max camber 3.8% at 37.1% chord
Source UIUC Airfoil Coordinates Database

(fx66196v-il) FX 66-S-196 V1 AIRFOIL

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FX 66-S-196 V1 AIRFOILWortmann FX 66-S-196 V1 airfoil
Max thickness 19.6% at 37.1% chord
Max camber 4% at 46.7% chord
Source UIUC Airfoil Coordinates Database

(fx66a175-il) WORTMANN FX 66-17A-175 AIRFOIL

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WORTMANN FX 66-17A-175 AIRFOILWortmann FX 66-17A-175 airfoil
Max thickness 17.5% at 33.9% chord
Max camber 4.2% at 40.2% chord
Source UIUC Airfoil Coordinates Database

(fx66h60-il) FX 66-H-60

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FX 66-H-60Wortmann FX 66-H-60 airfoil
Max thickness 6% at 22.2% chord
Max camber 1.7% at 17% chord
Source UIUC Airfoil Coordinates Database

(fx66h80-il) FX 66-H-80

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FX 66-H-80Wortmann FX 66-H-80 airfoil
Max thickness 8% at 27.9% chord
Max camber 2.5% at 25% chord
Source UIUC Airfoil Coordinates Database

(fx66s161-il) FX 66-S-161 AIRFOIL

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FX 66-S-161 AIRFOILWortmann FX 66-S-161 airfoil
Max thickness 16.1% at 33.9% chord
Max camber 3.9% at 43.5% chord
Source UIUC Airfoil Coordinates Database

(fx66s171-il) FX 66-S-171 AIRFOIL

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FX 66-S-171 AIRFOILWortmann FX 66-S-171 airfoil
Max thickness 17.1% at 33.9% chord
Max camber 3.9% at 43.5% chord
Source UIUC Airfoil Coordinates Database

(fx66s196-il) FX 66-S-196 AIRFOIL

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FX 66-S-196 AIRFOILWortmann FX 66-S-196 airfoil
Max thickness 19.6% at 37.1% chord
Max camber 3.8% at 43.5% chord
Source UIUC Airfoil Coordinates Database

(fx67k150-il) FX 67-K-150/17 AIRFOIL

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FX 67-K-150/17 AIRFOILWortmann FX 67-K-150/17 airfoil
Max thickness 15% at 40.2% chord
Max camber 4.8% at 43.5% chord
Source UIUC Airfoil Coordinates Database

(fx67k170-il) FX 67-K-170/17 AIRFOIL

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FX 67-K-170/17 AIRFOILWortmann FX 67-K-170/17 airfoil
Max thickness 17% at 40.2% chord
Max camber 5.1% at 43.5% chord
Source UIUC Airfoil Coordinates Database

(fx68h120-il) FX 68-H-120

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FX 68-H-120Wortmann FX 68-H-120 airfoil
Max thickness 11.8% at 25% chord
Max camber 2.3% at 33.9% chord
Source UIUC Airfoil Coordinates Database

(fx69274-il) WORTMANN FX 69-274

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WORTMANN FX 69-274Wortmann FX 69-274 airfoil
Max thickness 27.4% at 33.9% chord
Max camber 3.2% at 37.1% chord
Source UIUC Airfoil Coordinates Database

(fx69h083-il) BELL/WORTMANN FX 69-H-083 AIRFOIL

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BELL/WORTMANN FX 69-H-083 AIRFOILBell/Wortmann FX 69-H-083 rotorcraft airfoil
Max thickness 8.4% at 33.3% chord
Max camber 2.5% at 33.3% chord
Source UIUC Airfoil Coordinates Database

(fx69h098-il) BELL/WORTMANN FX 69-H-098 AIRFOIL

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BELL/WORTMANN FX 69-H-098 AIRFOILBell/Wortmann FX 69-H-098 rotorcraft airfoil
Max thickness 9.9% at 28.2% chord
Max camber 1.7% at 22.5% chord
Source UIUC Airfoil Coordinates Database

(fx69pr281-il) FX 69-PR-281

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FX 69-PR-281Wortmann FX 69-PR-281 airfoil
Max thickness 28.1% at 22.2% chord
Max camber 5.6% at 50% chord
Source UIUC Airfoil Coordinates Database

(fx71089a-il) WORTMANN FX 71-089A AIRFOIL

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WORTMANN FX 71-089A AIRFOILWortmann FX 71-089A airfoil
Max thickness 8.9% at 22.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx71120-il) WORTMANN FX 71-120 AIRFOIL

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WORTMANN FX 71-120 AIRFOILWortmann FX 71-120 airfoil
Max thickness 12% at 25% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(fx711520-il) FX 71-L-150/20 AIRFOIL

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FX 71-L-150/20 AIRFOILWortmann FX 71-L-150/20 airfoil
Max thickness 15% at 33.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
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