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Airfoil database list (U).

UA(2)-180 (University Of Alberta/Marsden) to USA 34 AIRFOIL

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(ua2-180-il) UA(2)-180 (University of Alberta/Marsden)

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UA(2)-180 (University of Alberta/Marsden)UA(2)-180 airfoil for ultralight category aircraft
Max thickness 18.1% at 31.5% chord
Max camber 7% at 36.6% chord
Source UIUC Airfoil Coordinates Database

(ua2-180sm-il) UA(2)-180 smoothed

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UA(2)-180 smoothedUA(2)-180 (smoothed) airfoil for ultralight category aircraft
Max thickness 18.2% at 34.1% chord
Max camber 6.5% at 39.3% chord
Source UIUC Airfoil Coordinates Database

(ua79sf18-il) UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL

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UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOILUniversity of Alberta/Marsden UA 79-SF-187 FLAPPED sailplane airfoil
Max thickness 18.8% at 42.8% chord
Max camber 3.7% at 63.4% chord
Source UIUC Airfoil Coordinates Database

(ua79sff-il) UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT

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UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENTUniversity of Alberta/Marsden UA 79-SF-187 sailplane airfoil FLAP
Max thickness 8.7% at 73.1% chord
Max camber 3.4% at 78.1% chord
Source UIUC Airfoil Coordinates Database

(ua79sfm-il) UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT

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UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENTUniversity of Alberta/Marsden UA 79-SF-187 sailplane airfoil MAIN ELEMENT
Max thickness 18.8% at 42.8% chord
Max camber 3% at 66.9% chord
Source UIUC Airfoil Coordinates Database

(uag8814320-il) UAG 88-143/20

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UAG 88-143/20UAG 88-143/20 airfoil
Max thickness 14.3% at 43.5% chord
Max camber 6.2% at 46.7% chord
Source UIUC Airfoil Coordinates Database

(ui1720-il) UNIVERSITY OF ILLINOIS UI-1720 AIRFOIL

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UNIVERSITY OF ILLINOIS UI-1720 AIRFOILUniversity of Illinois UI-1720 high lift airfoil
Max thickness 13.8% at 19% chord
Max camber 4.6% at 21.2% chord
Source UIUC Airfoil Coordinates Database

(ultimate-il) ULTIMATE

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ULTIMATECarl Goldberg R/C Ultimate Bipe airfoil
Max thickness 12.8% at 34.2% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(us1000root-il) US1000ROOT

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US1000ROOTGreat Planes R/C Ultra-Sport 1000 airfoil
Max thickness 18.6% at 27.1% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(usa22-il) USA 22 AIRFOIL

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USA 22 AIRFOILUSA-22 airfoil
Max thickness 9.1% at 19.9% chord
Max camber 4.4% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(usa25-il) USA 25 AIRFOIL

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USA 25 AIRFOILUSA-25 airfoil
Max thickness 8.3% at 19.9% chord
Max camber 5.2% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(usa26-il) USA 26 AIRFOIL

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USA 26 AIRFOILUSA-26 airfoil
Max thickness 9.8% at 19.9% chord
Max camber 4.3% at 39.9% chord
Source UIUC Airfoil Coordinates Database

(usa27-il) USA 27 AIRFOIL

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USA 27 AIRFOILUSA-27 airfoil
Max thickness 11.1% at 30% chord
Max camber 5.1% at 40% chord
Source UIUC Airfoil Coordinates Database

(usa27m2-il) USA 27 mod. AIRFOIL

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USA 27 mod. AIRFOILUSA-27MOD airfoil
Max thickness 13.3% at 30% chord
Max camber 5% at 40% chord
Source UIUC Airfoil Coordinates Database

(usa28-il) USA 28 AIRFOIL

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USA 28 AIRFOILUSA-28 airfoil
Max thickness 13.2% at 29.9% chord
Max camber 3.8% at 49.9% chord
Source UIUC Airfoil Coordinates Database

(usa29-il) USA 29 AIRFOIL

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USA 29 AIRFOILUSA-29 airfoil
Max thickness 13.2% at 29.7% chord
Max camber 5.5% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(usa31-il) USA 31 AIRFOIL

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USA 31 AIRFOILUSA-31 airfoil
Max thickness 14.8% at 19.7% chord
Max camber 9.3% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(usa32-il) USA 32 AIRFOIL

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USA 32 AIRFOILUSA-32 airfoil
Max thickness 14.7% at 19.8% chord
Max camber 9.3% at 39.8% chord
Source UIUC Airfoil Coordinates Database

(usa33-il) USA 33 AIRFOIL

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USA 33 AIRFOILUSA-33 airfoil
Max thickness 14.2% at 29.9% chord
Max camber 4.9% at 29.9% chord
Source UIUC Airfoil Coordinates Database

(usa34-il) USA 34 AIRFOIL

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USA 34 AIRFOILUSA-34 airfoil
Max thickness 18% at 29.5% chord
Max camber 7.7% at 39.5% chord
Source UIUC Airfoil Coordinates Database
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