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Airfoil database list (D).

DAE-11 AIRFOIL to DORNIER A-5 AIRFOIL

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(dae11-il) DAE-11 AIRFOIL

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DAE-11 AIRFOILDrela DAE11 low Reynolds number airfoil
Max thickness 12.8% at 32.8% chord
Max camber 6.6% at 44.4% chord
Source UIUC Airfoil Coordinates Database

(dae21-il) DAE-21 AIRFOIL

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DAE-21 AIRFOILDrela DAE21 low Reynolds number airfoil
Max thickness 11.8% at 32% chord
Max camber 6.6% at 43.7% chord
Source UIUC Airfoil Coordinates Database

(dae31-il) DAE-31 AIRFOIL

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DAE-31 AIRFOILDrela DAE31 low Reynolds number airfoil
Max thickness 11.1% at 29.3% chord
Max camber 6.7% at 47% chord
Source UIUC Airfoil Coordinates Database

(dae51-il) DAE-51 AIRFOIL

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DAE-51 AIRFOILDrela DAE51 low Reynolds number airfoil
Max thickness 9.4% at 30.7% chord
Max camber 4% at 46.4% chord
Source UIUC Airfoil Coordinates Database

(davis-corrected-il) DAVIS BASIC B-24 WING AIRFOIL

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DAVIS BASIC B-24 WING AIRFOILDavis basic B-24 wing airfoil
Max thickness 15.9% at 29.6% chord
Max camber 2.5% at 29.6% chord
Source UIUC Airfoil Coordinates Database

(davis-il) Davis AIRFOIL

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Davis AIRFOILConsolidated/Davis airfoil (B-24 wing?)
Max thickness 11.3% at 30% chord
Max camber 3.7% at 40% chord
Source UIUC Airfoil Coordinates Database

(davissm-il) davissm

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davissmDavis 3R F1B free flight airfoil (smoothed)
Max thickness 5.9% at 30.6% chord
Max camber 5.9% at 45.4% chord
Source UIUC Airfoil Coordinates Database

(daytonwright6-il) Dayton-Wright 6

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Dayton-Wright 6Dayton-Wright 6 airfoil
Max thickness 13.6% at 30% chord
Max camber 4.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(daytonwrightt1-il) Dayton-Wright T-1

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Dayton-Wright T-1Dayton-Wright T-1 airfoil
Max thickness 13.4% at 30% chord
Max camber 4.4% at 40% chord
Source UIUC Airfoil Coordinates Database

(dbln526-il) SIKORSKY DBLN-526 AIRFOIL

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SIKORSKY DBLN-526 AIRFOILSikorsky DBLN-526 double ended rotorcraft airfoil
Max thickness 26% at 50% chord
Max camber 4% at 50% chord
Source UIUC Airfoil Coordinates Database

(defcnd1-il) DEFIANT CANARD BL20 AIRFOIL

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DEFIANT CANARD BL20 AIRFOILRutan DEFIANT canard BL20 airfoil
Max thickness 20.9% at 28.6% chord
Max camber 4.5% at 36.1% chord
Source UIUC Airfoil Coordinates Database

(defcnd2-il) DEFIANT CANARD BL110 AIRFOIL

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DEFIANT CANARD BL110 AIRFOILRutan DEFIANT canard BL110 airfoil
Max thickness 14.7% at 28.6% chord
Max camber 3.8% at 28.6% chord
Source UIUC Airfoil Coordinates Database

(defcnd3-il) DEFIANT CANARD BL145 AIRFOIL

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DEFIANT CANARD BL145 AIRFOILRutan DEFIANT canard BL145 airfoil
Max thickness 11.5% at 28.6% chord
Max camber 2.4% at 28.6% chord
Source UIUC Airfoil Coordinates Database

(df101-il) DF 101 AIRFOIL

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DF 101 AIRFOILDavid Fraser DF 101 low Reynolds number airfoil
Max thickness 11% at 29.1% chord
Max camber 2.3% at 43.5% chord
Source UIUC Airfoil Coordinates Database

(df102-il) DF102

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DF102David Fraser DF 102 low Reynolds number airfoil
Max thickness 11% at 29.1% chord
Max camber 2.4% at 43.5% chord
Source UIUC Airfoil Coordinates Database

(dfvlrr4-il) DFVLR R-4 AIRFOIL

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DFVLR R-4 AIRFOILDFVLR R-4 transonic airfoil
Max thickness 13.4% at 37.9% chord
Max camber 2.1% at 79.9% chord
Source UIUC Airfoil Coordinates Database

(dga1138-il) D.G.A. 1138

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D.G.A. 1138D.G.A. 1138 airfoil
Max thickness 6.9% at 30% chord
Max camber 2.6% at 40% chord
Source UIUC Airfoil Coordinates Database

(dga1182-il) D.G.A. 1182

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D.G.A. 1182D.G.A. 1182 airfoil
Max thickness 7.6% at 30% chord
Max camber 0.9% at 20% chord
Source UIUC Airfoil Coordinates Database

(dh4009sm-il) dh4009sm

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dh4009smDale House DH4009 (smoothed) used on the Storm R/C aerobatic aircraft
Max thickness 8.9% at 41.6% chord
Max camber 0.2% at 9.6% chord
Source UIUC Airfoil Coordinates Database

(doa5-il) DORNIER A-5 AIRFOIL

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DORNIER A-5 AIRFOILDornier A-5 airfoil (reconstruction) (DO 228 wing)
Max thickness 16.2% at 40.1% chord
Max camber 2.5% at 76% chord
Source UIUC Airfoil Coordinates Database
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