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Airfoil database list (R).

RONCZ 1046 VOYAGER CANARD AIRFOIL to RAF 25 AIRFOIL

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(r1046-il) RONCZ 1046 VOYAGER CANARD AIRFOIL

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RONCZ 1046 VOYAGER CANARD AIRFOILRoncz 1046 Voyager canard airfoil
Max thickness 18.1% at 38% chord
Max camber 6.7% at 42% chord
Source UIUC Airfoil Coordinates Database

(r1080-il) RONCZ 1080 VOYAGER INNER AFT WING AIRFOIL

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RONCZ 1080 VOYAGER INNER AFT WING AIRFOILRoncz 1080 Voyager inner aft wing airfoil
Max thickness 18% at 40% chord
Max camber 3.3% at 40% chord
Source UIUC Airfoil Coordinates Database

(r1082-il) RONCZ 1082 VOYAGER ROOT OUTER AFT WING AIRFOIL

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RONCZ 1082 VOYAGER ROOT OUTER AFT WING AIRFOILRoncz 1082 Voyager root outer aft wing airfoil
Max thickness 18% at 40% chord
Max camber 3.4% at 40% chord
Source UIUC Airfoil Coordinates Database

(r1082t-il) RONCZ 1082T VOYAGER TIP OUTER AFT WING AIRFOIL

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RONCZ 1082T VOYAGER TIP OUTER AFT WING AIRFOILRoncz 1082T Voyager tip outer aft wing airfoil
Max thickness 16% at 40% chord
Max camber 3% at 40% chord
Source UIUC Airfoil Coordinates Database

(r140-il) R140 (original)

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R140 (original)R140 Quickee 500 airfoil (original)
Max thickness 12% at 39.3% chord
Max camber 0.5% at 42.3% chord
Source UIUC Airfoil Coordinates Database

(r140sm-il) R140 12.04% (smoothed)

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R140  12.04% (smoothed)R140 Quickee 500 airfoil (smoothed)
Max thickness 12% at 39.3% chord
Max camber 0.4% at 39.3% chord
Source UIUC Airfoil Coordinates Database

(rae100-il) RAE 100 AIRFOIL

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RAE 100 AIRFOILRAE 100 airfoil
Max thickness 10% at 26% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(rae101-il) RAE 101 AIRFOIL

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RAE 101 AIRFOILRAE 101 airfoil
Max thickness 10% at 30% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(rae102-il) RAE 102 AIRFOIL

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RAE 102 AIRFOILRAE 102 airfoil
Max thickness 10% at 36% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(rae103-il) RAE 103 AIRFOIL

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RAE 103 AIRFOILRAE 103 airfoil
Max thickness 10% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(rae104-il) RAE 104 AIRFOIL

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RAE 104 AIRFOILRAE 104 airfoil
Max thickness 10% at 42% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(rae2822-il) RAE 2822 AIRFOIL

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RAE 2822 AIRFOILRAE 2822 transonic airfoil
Max thickness 12.1% at 37.9% chord
Max camber 1.3% at 75.7% chord
Source UIUC Airfoil Coordinates Database

(rae5212-il) RAE(NPL) 5212 AIRFOIL

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RAE(NPL) 5212 AIRFOILRAE(NPL) 5212 transonic airfoil
Max thickness 11.9% at 35.5% chord
Max camber 1.8% at 69.1% chord
Source UIUC Airfoil Coordinates Database

(rae5213-il) RAE(NPL) 5213 AIRFOIL

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RAE(NPL) 5213 AIRFOILRAE(NPL) 5213 transonic airfoil
Max thickness 10% at 35.5% chord
Max camber 1.4% at 69.1% chord
Source UIUC Airfoil Coordinates Database

(rae5214-il) RAE 5214 AIRFOIL

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RAE 5214 AIRFOILRAE 5214 transonic airfoil
Max thickness 9.7% at 35.5% chord
Max camber 1.4% at 69.1% chord
Source UIUC Airfoil Coordinates Database

(rae5215-il) RAE 5215 AIRFOIL

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RAE 5215 AIRFOILRAE 5215 transonic airfoil
Max thickness 9.7% at 35.5% chord
Max camber 1.5% at 69.1% chord
Source UIUC Airfoil Coordinates Database

(rae69ck-il) RAE6-9CK AIRFOIL

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RAE6-9CK AIRFOILRAE6-9CK transonic airfoil
Max thickness 12.1% at 37.9% chord
Max camber 1.3% at 75.7% chord
Source UIUC Airfoil Coordinates Database

(raf15-il) RAF 15 AIRFOIL

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RAF 15 AIRFOILRAF-15 airfoil
Max thickness 6.5% at 15% chord
Max camber 2.6% at 30% chord
Source UIUC Airfoil Coordinates Database

(raf19-il) RAF 19 AIRFOIL

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RAF 19 AIRFOILRAF-19 airfoil
Max thickness 10.5% at 15% chord
Max camber 10.1% at 40% chord
Source UIUC Airfoil Coordinates Database

(raf25-il) RAF 25 AIRFOIL

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RAF 25 AIRFOILRAF-25 airfoil
Max thickness 6.5% at 29.9% chord
Max camber 1% at 49.9% chord
Source UIUC Airfoil Coordinates Database
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