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Airfoil database list (R).

RAF 26 AIRFOIL to NASA/LANGLEY RC-10(B)3 AIRFOIL

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(raf26-il) RAF 26 AIRFOIL

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RAF 26 AIRFOILRAF-26 airfoil
Max thickness 6.6% at 29.9% chord
Max camber 2.1% at 49.9% chord
Source UIUC Airfoil Coordinates Database

(raf27-il) RAF 27 AIRFOIL

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RAF 27 AIRFOILRAF-27 airfoil
Max thickness 9.8% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(raf28-il) RAF 28 AIRFOIL

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RAF 28 AIRFOILRAF-28 airfoil
Max thickness 9.8% at 30% chord
Max camber 1.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(raf30-il) RAF 30 AIRFOIL

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RAF 30 AIRFOILRAF-30 airfoil
Max thickness 12.6% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(raf30md-il) RAF 30 MOD AIRFOIL

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RAF 30 MOD AIRFOILRAF-30 MOD airfoil
Max thickness 7.6% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(raf31-il) RAF 31 AIRFOIL

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RAF 31 AIRFOILRAF-31 airfoil
Max thickness 12.7% at 30% chord
Max camber 2.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(raf32-il) RAF 32 AIRFOIL

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RAF 32 AIRFOILRAF-32 airfoil
Max thickness 12.7% at 30% chord
Max camber 5% at 50% chord
Source UIUC Airfoil Coordinates Database

(raf32md-il) RAF 32 MOD AIRFOIL

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RAF 32 MOD AIRFOILRAF-32 MOD airfoil
Max thickness 10.2% at 30% chord
Max camber 4% at 50% chord
Source UIUC Airfoil Coordinates Database

(raf33-il) RAF 33 AIRFOIL

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RAF 33 AIRFOILRAF-33 airfoil
Max thickness 12.6% at 30% chord
Max camber 4.7% at 30% chord
Source UIUC Airfoil Coordinates Database

(raf34-il) RAF 34 AIRFOIL

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RAF 34 AIRFOILRAF-34 airfoil
Max thickness 12.6% at 30% chord
Max camber 2% at 30% chord
Source UIUC Airfoil Coordinates Database

(raf38-il) RAF 38 AIRFOIL

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RAF 38 AIRFOILRAF-38 airfoil
Max thickness 12.7% at 30% chord
Max camber 2.5% at 40% chord
Source UIUC Airfoil Coordinates Database

(raf48-il) RAF-48 AIRFOIL

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RAF-48 AIRFOILRAF-48 airfoil
Max thickness 15% at 30% chord
Max camber 2.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(raf6-il) RAF 6 AIRFOIL

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RAF 6 AIRFOILRAF-6 airfoil
Max thickness 10% at 30% chord
Max camber 4.6% at 30% chord
Source UIUC Airfoil Coordinates Database

(raf69-il) RAF 69 AIRFOIL

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RAF 69 AIRFOILRAF-69 airfoil
Max thickness 20.6% at 30% chord
Max camber 1.7% at 50% chord
Source UIUC Airfoil Coordinates Database

(raf89-il) RAF 89 AIRFOIL

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RAF 89 AIRFOILRAF-89 airfoil
Max thickness 25% at 30% chord
Max camber 1.6% at 50% chord
Source UIUC Airfoil Coordinates Database

(rc0864c-il) NASA/LANGLEY RC08-64C AIRFOIL

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NASA/LANGLEY RC08-64C AIRFOILNASA/Langley 08-64C rotorcraft airfoil
Max thickness 8% at 40% chord
Max camber 1% at 35% chord
Source UIUC Airfoil Coordinates Database

(rc08b3-il) NASA/LANGLEY RC-08(B)3 AIRFOIL

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NASA/LANGLEY RC-08(B)3 AIRFOILNASA/Langley RC-08(B)3 rotorcraft airfoil
Max thickness 8% at 37.8% chord
Max camber 1.1% at 34.1% chord
Source UIUC Airfoil Coordinates Database

(rc08n1-il) NASA/LANGLEY RC-08(N)1 AIRFOIL

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NASA/LANGLEY RC-08(N)1 AIRFOILNASA/Langley RC-08(N)1 rotorcraft airfoil
Max thickness 8% at 37.5% chord
Max camber 1.6% at 25% chord
Source UIUC Airfoil Coordinates Database

(rc1064c-il) NASA/LANGLEY RC10-64C AIRFOIL

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NASA/LANGLEY RC10-64C AIRFOILNASA/Langley 10-64C rotorcraft airfoil
Max thickness 10% at 40% chord
Max camber 1% at 35% chord
Source UIUC Airfoil Coordinates Database

(rc10b3-il) NASA/LANGLEY RC-10(B)3 AIRFOIL

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NASA/LANGLEY RC-10(B)3 AIRFOILNASA/Langley RC-10(B)3 rotorcraft airfoil
Max thickness 10% at 37.7% chord
Max camber 1.7% at 30.3% chord
Source UIUC Airfoil Coordinates Database
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