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Airfoil database list (C).

CLARK YH AIRFOIL to Curtis C-72

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(clarkyh-il) CLARK YH AIRFOIL

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CLARK YH AIRFOILCLARK YH airfoil
Max thickness 11.9% at 30% chord
Max camber 2.5% at 30% chord
Source UIUC Airfoil Coordinates Database

(clarkys-il) CLARK YS AIRFOIL

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CLARK YS AIRFOILCLARK YS airfoil
Max thickness 11.7% at 30% chord
Max camber 2.4% at 30% chord
Source UIUC Airfoil Coordinates Database

(clarkysm-il) CLARK-Y 11.7% smoothed

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CLARK-Y 11.7% smoothedCLARK Y airfoil (smoothed)
Max thickness 11.7% at 30.9% chord
Max camber 3.5% at 43.5% chord
Source UIUC Airfoil Coordinates Database

(clarkz-il) CLARK Z AIRFOIL

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CLARK Z AIRFOILCLARK Z airfoil
Max thickness 11.8% at 30% chord
Max camber 4% at 40% chord
Source UIUC Airfoil Coordinates Database

(clarym15-il) CLARK YM-15 AIRFOIL

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CLARK YM-15 AIRFOILCLARK YM15 airfoil
Max thickness 15% at 29.6% chord
Max camber 3.6% at 39.6% chord
Source UIUC Airfoil Coordinates Database

(clarym18-il) CLARK YM-18 AIRFOIL

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CLARK YM-18 AIRFOILCLARK YM18 airfoil
Max thickness 18% at 29.6% chord
Max camber 3.6% at 39.6% chord
Source UIUC Airfoil Coordinates Database

(coanda1-il) Coanda 1

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Coanda 1Coanda 1 airfoil
Max thickness 5.7% at 30% chord
Max camber 2.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(coanda2-il) Coanda 2

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Coanda 2Coanda 2 airfoil
Max thickness 6% at 30% chord
Max camber 2.9% at 30% chord
Source UIUC Airfoil Coordinates Database

(coanda3-il) Coanda 3

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Coanda 3Coanda 3 airfoil
Max thickness 7% at 30% chord
Max camber 2.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(cootie-il) WACO COOTIE AIRFOIL

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WACO COOTIE AIRFOILWaco Cootie airfoil
Max thickness 8.5% at 30% chord
Max camber 5.5% at 40% chord
Source UIUC Airfoil Coordinates Database

(cp-060-050-gn) Cambered plate C=6% T=5% R=2.11

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Cambered plate C=6% T=5% R=2.11HAWT pipe blade with coordinates based on top surface. Camber=6% Wall thickness=5% Radius=2.113
Max thickness 10.8% at 6.3% chord
Max camber 2.7% at 52.1% chord
Source Generated

(cp-080-050-gn) Cambered plate C=8% T=5% R=1.6

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Cambered plate C=8% T=5% R=1.6HAWT pipe blade with coordinates based on top surface. Camber=8% Wall thickness=5% Radius=1.603
Max thickness 8.4% at 5% chord
Max camber 5.3% at 47% chord
Source Generated

(cp-100-050-gn) Cambered plate C=10% T=5% R=1.3

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Cambered plate C=10% T=5% R=1.3HAWT pipe blade with coordinates based on top surface. Camber=10% Wall thickness=5% Radius=1.3
Max thickness 7% at 4.2% chord
Max camber 7.9% at 46.5% chord
Source Generated

(cp-120-050-gn) Cambered plate C=12% T=5% R=1.1

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Cambered plate C=12% T=5% R=1.1HAWT pipe blade with coordinates based on top surface. Camber=12% Wall thickness=5% Radius=1.102
Max thickness 6.1% at 4% chord
Max camber 9.9% at 47.9% chord
Source Generated

(cp-140-050-gn) Cambered plate C=14% T=5% R=0.96

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Cambered plate C=14% T=5% R=0.96HAWT pipe blade with coordinates based on top surface. Camber=14% Wall thickness=5% Radius=0.963
Max thickness 5.5% at 3.6% chord
Max camber 12.2% at 47.7% chord
Source Generated

(cp-160-050-gn) Cambered plate C=16% T=5% R=0.86

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Cambered plate C=16% T=5% R=0.86HAWT pipe blade with coordinates based on top surface. Camber=16% Wall thickness=5% Radius=0.861
Max thickness 5.2% at 3.4% chord
Max camber 14.3% at 49.2% chord
Source Generated

(cp-180-050-gn) Cambered plate C=18% T=5% R=0.78

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Cambered plate C=18% T=5% R=0.78HAWT pipe blade with coordinates based on top surface. Camber=18% Wall thickness=5% Radius=0.784
Max thickness 5% at 3.2% chord
Max camber 16.4% at 49.3% chord
Source Generated

(cr001sm-il) cr001sm

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cr001smCody Robertson CR 001 R/C hand-launch low Reynolds number airfoil (smoothed)
Max thickness 7.3% at 27.1% chord
Max camber 4.1% at 45.4% chord
Source UIUC Airfoil Coordinates Database

(cr1-il) CURTISS CR-1 AIRFOIL

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CURTISS CR-1 AIRFOILCurtiss CR-1 general aviation airfoil
Max thickness 12.2% at 24% chord
Max camber 4.7% at 42% chord
Source UIUC Airfoil Coordinates Database

(curtisc72-il) Curtis C-72

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Curtis C-72Curtis C-72 airfoil
Max thickness 11.7% at 30% chord
Max camber 3.8% at 50% chord
Source UIUC Airfoil Coordinates Database
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