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NASA/LANGLEY RC-10(N)1 AIRFOIL to Rhode St. Genese 30

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(rc10n1-il) NASA/LANGLEY RC-10(N)1 AIRFOIL

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NASA/LANGLEY RC-10(N)1 AIRFOILNASA/Langley RC-10(N)1 rotorcraft airfoil
Max thickness 10% at 37.6% chord
Max camber 1.5% at 25% chord
Source UIUC Airfoil Coordinates Database

(rc1264c-il) NASA/LANGLEY RC12-64C AIRFOIL

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NASA/LANGLEY RC12-64C AIRFOILNASA/Langley 12-64C rotorcraft airfoil
Max thickness 12% at 40% chord
Max camber 1% at 35% chord
Source UIUC Airfoil Coordinates Database

(rc12b3-il) NASA/LANGLEY RC-12(B)3 AIRFOIL

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NASA/LANGLEY RC-12(B)3 AIRFOILNASA/Langley RC-12(B)3 rotorcraft airfoil
Max thickness 12% at 38% chord
Max camber 2.2% at 34.3% chord
Source UIUC Airfoil Coordinates Database

(rc12n1-il) NASA/LANGLEY RC-12(N)1 AIRFOIL

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NASA/LANGLEY RC-12(N)1 AIRFOILNASA/Langley RC-12(N)1 rotorcraft airfoil
Max thickness 12% at 37.4% chord
Max camber 1.4% at 30% chord
Source UIUC Airfoil Coordinates Database

(rc410-il) NASA RC(4)-10 AIRFOIL

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NASA RC(4)-10 AIRFOILNASA/Langley RC(4)-10 rotorcraft airfoil
Max thickness 10% at 37.8% chord
Max camber 2.1% at 30.3% chord
Source UIUC Airfoil Coordinates Database

(rc510-il) NASA RC(5)-10 AIRFOIL

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NASA RC(5)-10 AIRFOILNASA/Langley RC(5)-10 rotorcraft airfoil
Max thickness 10% at 40.1% chord
Max camber 2.2% at 25.3% chord
Source UIUC Airfoil Coordinates Database

(rcsc2-il) NASA/LANGLEY RC-SC2 AIRFOIL

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NASA/LANGLEY RC-SC2 AIRFOILNASA/Langley RC-SC2 rotorcraft airfoil
Max thickness 10% at 40% chord
Max camber 0.5% at 62.5% chord
Source UIUC Airfoil Coordinates Database

(rg12-il) RG-12

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RG-12Rolf Girsberger RG 12 airfoil
Max thickness 9.3% at 34.4% chord
Max camber 1.4% at 34.4% chord
Source UIUC Airfoil Coordinates Database

(rg12a-il) AIRFOIL PROFILE12A 9.00%

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AIRFOIL PROFILE12A 9.00%Rolf Girsberger RG 12A airfoil
Max thickness 9% at 34.4% chord
Max camber 1.8% at 34.4% chord
Source UIUC Airfoil Coordinates Database

(rg12a189-il) RG 12A-1.8/9.0 AIRFOIL

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RG 12A-1.8/9.0 AIRFOILRolf Girsberger RG 12A-1.8/9.0 airfoil
Max thickness 9% at 34.4% chord
Max camber 1.8% at 34.4% chord
Source UIUC Airfoil Coordinates Database

(rg14-il) RG 14 AIRFOIL

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RG 14 AIRFOILRolf Girsberger RG 14 airfoil
Max thickness 8.5% at 29.7% chord
Max camber 1.6% at 39.2% chord
Source UIUC Airfoil Coordinates Database

(rg1410-il) RG 14 10% AIRFOIL

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RG 14 10% AIRFOILRolf Girsberger RG 14 (10%) airfoil
Max thickness 10% at 31% chord
Max camber 1.6% at 36% chord
Source UIUC Airfoil Coordinates Database

(rg149-il) RG 14 9% AIRFOIL

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RG 14 9% AIRFOILRolf Girsberger RG 14 (9%) airfoil
Max thickness 9% at 31% chord
Max camber 1.6% at 36% chord
Source UIUC Airfoil Coordinates Database

(rg1495-il) RG 14 9.5% AIRFOIL

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RG 14 9.5% AIRFOILRolf Girsberger RG 14 (9.5%) airfoil
Max thickness 9.5% at 31% chord
Max camber 1.6% at 36% chord
Source UIUC Airfoil Coordinates Database

(rg14a147-il) RG 14A-1.4/7.0 AIRFOIL

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RG 14A-1.4/7.0 AIRFOILRolf Girsberger RG 14A-1.4/7.0 airfoil
Max thickness 7% at 29.7% chord
Max camber 1.4% at 34.3% chord
Source UIUC Airfoil Coordinates Database

(rg15-il) RG-15 8.9%

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RG-15 8.9%Rolf Girsberger RG 15 low Reynolds number airfoil
Max thickness 8.9% at 30.2% chord
Max camber 1.8% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(rg15a111-il) RG 15A-1.8/11.0 AIRFOIL

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RG 15A-1.8/11.0 AIRFOILRolf Girsberger RG 15A-1.8/11.0 airfoil
Max thickness 11% at 30.2% chord
Max camber 1.8% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(rg15a213-il) RG 15A 2.5/13.0 AIRFOIL

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RG 15A 2.5/13.0 AIRFOILRolf Girsberger RG 15A 2.5/13.0 airfoil
Max thickness 13% at 30.2% chord
Max camber 2.5% at 39.7% chord
Source UIUC Airfoil Coordinates Database

(rg8-il) RG 8 AIRFOIL

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RG 8 AIRFOILRolf Girsberger RG 8 airfoil
Max thickness 10.8% at 31.1% chord
Max camber 2.2% at 60.5% chord
Source UIUC Airfoil Coordinates Database

(rhodesg30-il) Rhode St. Genese 30

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Rhode St. Genese 30Rhode St. Genese 30 airfoil
Max thickness 9.7% at 30% chord
Max camber 3.2% at 40% chord
Source UIUC Airfoil Coordinates Database
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