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Airfoil database list (F).

Falcon to WORTMANN FX 60-126 AIRFOIL

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(falcon-il) Falcon

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FalconFalcon airfoil used on the Carl Goldberg Falcon 56 Mk II R/C powerplane
Max thickness 13.7% at 30.6% chord
Max camber 1.6% at 20.5% chord
Source UIUC Airfoil Coordinates Database

(fauvel-il) FAUVEL 14% AIRFOIL

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FAUVEL 14% AIRFOILFauvel 14% flying wing airfoil
Max thickness 14% at 25.2% chord
Max camber 2.5% at 25.2% chord
Source UIUC Airfoil Coordinates Database

(fg1-il) Fage & Collins 1

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Fage & Collins 1Fage & Collins 1 airfoil
Max thickness 8.2% at 30% chord
Max camber 3.1% at 40% chord
Source UIUC Airfoil Coordinates Database

(fg2-il) Fage & Collins 2

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Fage & Collins 2Fage & Collins 2 airfoil
Max thickness 8.2% at 30% chord
Max camber 3.3% at 30% chord
Source UIUC Airfoil Coordinates Database

(fg3-il) Fage & Collins 3

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Fage & Collins 3Fage & Collins 3 airfoil
Max thickness 10.1% at 30% chord
Max camber 4.3% at 30% chord
Source UIUC Airfoil Coordinates Database

(fg4-il) Fage & Collins 4

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Fage & Collins 4Fage & Collins 4 airfoil
Max thickness 12.7% at 30% chord
Max camber 4.7% at 30% chord
Source UIUC Airfoil Coordinates Database

(fx049915-il) WORTMANN FX 049-915 AIRFOIL

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WORTMANN FX 049-915 AIRFOILWortmann FX 049-915 airfoil
Max thickness 14.7% at 37.1% chord
Max camber 5.8% at 37.1% chord
Source UIUC Airfoil Coordinates Database

(fx05188-il) WORTMANN FX 05-188 AIRFOIL

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WORTMANN FX 05-188 AIRFOILWortmann FX 05-188 airfoil
Max thickness 18.8% at 37.1% chord
Max camber 2.6% at 50% chord
Source UIUC Airfoil Coordinates Database

(fx05191-il) WORTMANN FX 05-191 AIRFOIL

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WORTMANN FX 05-191 AIRFOILWortmann FX 05-191 airfoil
Max thickness 19.1% at 37.1% chord
Max camber 2.6% at 50% chord
Source UIUC Airfoil Coordinates Database

(fx057816-il) WORTMANN FX 057-816

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WORTMANN FX 057-816Wortmann FX 057-816 airfoil
Max thickness 16.2% at 37.1% chord
Max camber 5.1% at 37.1% chord
Source UIUC Airfoil Coordinates Database

(fx05h126-il) WORTMANN FX 05-H-126 AIRFOIL

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WORTMANN FX 05-H-126 AIRFOILWortmann FX 05-H-126 rotorcraft airfoil
Max thickness 12.6% at 37.1% chord
Max camber 4.4% at 37.1% chord
Source UIUC Airfoil Coordinates Database

(fx082512-il) WORTMANN FX 082-512 AIRFOIL

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WORTMANN FX 082-512 AIRFOILWortmann FX 082-512 airfoil
Max thickness 11.8% at 25% chord
Max camber 4.2% at 62.9% chord
Source UIUC Airfoil Coordinates Database

(fx08s176-il) WORTMANN FX 08-S-176 AIRFOIL

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WORTMANN FX 08-S-176 AIRFOILWortmann FX 08-S-176 airfoil
Max thickness 17.6% at 37.1% chord
Max camber 5.7% at 37.1% chord
Source UIUC Airfoil Coordinates Database

(fx2-il) WORTMANN FX 2 AIRFOIL

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WORTMANN FX 2 AIRFOILWortmann FX 2 airfoil
Max thickness 20.4% at 43.5% chord
Max camber 3.8% at 69.1% chord
Source UIUC Airfoil Coordinates Database

(fx3-il) WORTMANN FX 3 AIRFOIL

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WORTMANN FX 3 AIRFOILWortmann FX 3 airfoil
Max thickness 20% at 50% chord
Max camber 4.2% at 75% chord
Source UIUC Airfoil Coordinates Database

(fx38153-il) FX 38-153 AIRFOIL

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FX 38-153 AIRFOILWortmann FX 38-153 airfoil
Max thickness 15.5% at 43.5% chord
Max camber 2.1% at 80.4% chord
Source UIUC Airfoil Coordinates Database

(fx60100-il) FX 60-100 AIRFOIL

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FX 60-100 AIRFOILWortmann FX 60-100 airfoil
Max thickness 10% at 27.9% chord
Max camber 3.6% at 56.5% chord
Source UIUC Airfoil Coordinates Database

(fx601001-il) FX 60-100 (126) AIRFOIL

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FX 60-100 (126) AIRFOILWortmann FX 60-100 (126) airfoil
Max thickness 10.1% at 30.8% chord
Max camber 3.6% at 59.7% chord
Source UIUC Airfoil Coordinates Database

(fx60100sm-il) FX60-100 10.0% smoothed

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FX60-100 10.0% smoothedWortmann FX 60-100 airfoil (smoothed)
Max thickness 10% at 27.9% chord
Max camber 3.5% at 56.5% chord
Source UIUC Airfoil Coordinates Database

(fx60126-il) WORTMANN FX 60-126 AIRFOIL

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WORTMANN FX 60-126 AIRFOILWortmann FX 60-126 airfoil
Max thickness 12.6% at 27.9% chord
Max camber 3.6% at 56.5% chord
Source UIUC Airfoil Coordinates Database
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