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NASA SC(2)-0410 AIRFOIL to SD6060-104-88

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(sc20410-il) NASA SC(2)-0410 AIRFOIL

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NASA SC(2)-0410 AIRFOILNASA SC(2)-0410 airfoil (NASA TP-2969)
Max thickness 10% at 38% chord
Max camber 1.1% at 85% chord
Source UIUC Airfoil Coordinates Database

(sc20412-il) NASA SC(2)-0412 AIRFOIL

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NASA SC(2)-0412 AIRFOILNASA SC(2)-0412 airfoil (NASA TP-2969)
Max thickness 12% at 37% chord
Max camber 1.3% at 83% chord
Source UIUC Airfoil Coordinates Database

(sc20414-il) NASA SC(2)-0414 AIRFOIL

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NASA SC(2)-0414 AIRFOILNASA SC(2)-0414 airfoil (NASA TP-2969)
Max thickness 14% at 36% chord
Max camber 1.5% at 83% chord
Source UIUC Airfoil Coordinates Database

(sc20503-il) NASA SC(2)-0503 AIRFOIL

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NASA SC(2)-0503 AIRFOILNASA SC(2)-0503 airfoil (NASA TP-2969)
Max thickness 3% at 32% chord
Max camber 0.8% at 82% chord
Source UIUC Airfoil Coordinates Database

(sc20518-il) NASA SC(2)-0518 AIRFOIL

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NASA SC(2)-0518 AIRFOILNASA SC(2)-0518 airfoil (NASA TP-2969)
Max thickness 18% at 35% chord
Max camber 1.9% at 82% chord
Source UIUC Airfoil Coordinates Database

(sc20606-il) NASA SC(2)-0606 AIRFOIL

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NASA SC(2)-0606 AIRFOILNASA SC(2)-0606 airfoil (NASA TP-2969)
Max thickness 6% at 34% chord
Max camber 1.3% at 81% chord
Source UIUC Airfoil Coordinates Database

(sc20610-il) NASA SC(2)-0610 AIRFOIL

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NASA SC(2)-0610 AIRFOILNASA SC(2)-0610 airfoil (NASA TP-2969)
Max thickness 10% at 38% chord
Max camber 1.8% at 82% chord
Source UIUC Airfoil Coordinates Database

(sc20612-il) NASA SC(2)-0612 AIRFOIL

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NASA SC(2)-0612 AIRFOILNASA SC(2)-0612 airfoil (NASA TP-2969)
Max thickness 12% at 37% chord
Max camber 1.9% at 81% chord
Source UIUC Airfoil Coordinates Database

(sc20614-il) NASA SC(2)-0614 AIRFOIL

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NASA SC(2)-0614 AIRFOILNASA SC(2)-0614 airfoil (NASA TP-2969)
Max thickness 14% at 36% chord
Max camber 2.1% at 81% chord
Source UIUC Airfoil Coordinates Database

(sc20706-il) NASA SC(2)-0706 AIRFOIL

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NASA SC(2)-0706 AIRFOILNASA SC(2)-0706 airfoil (NASA TP-2969)
Max thickness 6% at 34% chord
Max camber 1.6% at 82% chord
Source UIUC Airfoil Coordinates Database

(sc20710-il) NASA SC(2)-0710 AIRFOIL

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NASA SC(2)-0710 AIRFOILNASA SC(2)-0710 airfoil (NASA TP-2969)
Max thickness 10% at 37% chord
Max camber 2.1% at 81% chord
Source UIUC Airfoil Coordinates Database

(sc20712-il) NASA SC(2)-0712 AIRFOIL

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NASA SC(2)-0712 AIRFOILNASA SC(2)-0712 airfoil (NASA TP-2969)
Max thickness 12% at 37% chord
Max camber 2.2% at 81% chord
Source UIUC Airfoil Coordinates Database

(sc20714-il) NASA SC(2)-0714 AIRFOIL

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NASA SC(2)-0714 AIRFOILNASA SC(2)-0714 airfoil (NASA TP-2969)
Max thickness 14% at 37% chord
Max camber 2.5% at 81% chord
Source UIUC Airfoil Coordinates Database

(sc21006-il) NASA SC(2)-1006 AIRFOIL

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NASA SC(2)-1006 AIRFOILNASA SC(2)-1006 airfoil
Max thickness 6% at 30% chord
Max camber 2.6% at 73% chord
Source UIUC Airfoil Coordinates Database

(sc21010-il) NASA SC(2)-1010 AIRFOIL

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NASA SC(2)-1010 AIRFOILNASA SC(2)-1010 airfoil
Max thickness 10% at 32% chord
Max camber 2.8% at 71% chord
Source UIUC Airfoil Coordinates Database

(sc2110-il) SIKORSKY SC2110 AIRFOIL

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SIKORSKY SC2110 AIRFOILSikorsky/Lednicer & Owen SC2110 rotorcraft airfoil (SC5410)
Max thickness 9.9% at 37.7% chord
Max camber 1.9% at 15.7% chord
Source UIUC Airfoil Coordinates Database

(sd2030-il) SD2030-086-88

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SD2030-086-88Selig/Donovan SD2030 low Reynolds number airfoil
Max thickness 8.6% at 35.5% chord
Max camber 2.2% at 45.3% chord
Source UIUC Airfoil Coordinates Database

(sd2083-il) SD2083 (9.0%)

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SD2083 (9.0%)Selig/Donovan SD2083 low Reynolds number airfoil
Max thickness 9% at 35.2% chord
Max camber 2.5% at 49.6% chord
Source UIUC Airfoil Coordinates Database

(sd5060-il) SD5060 (9.5%)

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SD5060 (9.5%)Selig/Donovan SD5060 low Reynolds number airfoil
Max thickness 9.5% at 24.9% chord
Max camber 2% at 48.5% chord
Source UIUC Airfoil Coordinates Database

(sd6060-il) SD6060-104-88

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SD6060-104-88Selig/Donovan SD6060 low Reynolds number airfoil
Max thickness 10.4% at 33.9% chord
Max camber 1.6% at 38.6% chord
Source UIUC Airfoil Coordinates Database
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