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Airfoil database list (C).

LOCKHEED C-141 BL0 AIRFOIL to CLARK Y AIRFOIL

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(c141a-il) LOCKHEED C-141 BL0 AIRFOIL

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LOCKHEED C-141 BL0 AIRFOILLockheed-Georgia C-141 transonic wing airfoils
Max thickness 13% at 40.2% chord
Max camber 1.1% at 64.5% chord
Source UIUC Airfoil Coordinates Database

(c141b-il) LOCKHEED C-141 BL113.6 AIRFOIL

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LOCKHEED C-141 BL113.6 AIRFOILLockheed-Georgia C-141 transonic wing airfoils
Max thickness 12.6% at 40.2% chord
Max camber 1.1% at 64.5% chord
Source UIUC Airfoil Coordinates Database

(c141c-il) LOCKHEED C-141 BL426.57 AIRFOIL

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LOCKHEED C-141 BL426.57 AIRFOILLockheed-Georgia C-141 transonic wing airfoils
Max thickness 11% at 40.2% chord
Max camber 1.3% at 50% chord
Source UIUC Airfoil Coordinates Database

(c141d-il) LOCKHEED C-141 BL610.61 AIRFOIL

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LOCKHEED C-141 BL610.61 AIRFOILLockheed-Georgia C-141 transonic wing airfoils
Max thickness 10.8% at 40.2% chord
Max camber 1.5% at 50% chord
Source UIUC Airfoil Coordinates Database

(c141e-il) LOCKHEED C-141 BL761.11 AIRFOIL

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LOCKHEED C-141 BL761.11 AIRFOILLockheed-Georgia C-141 transonic wing airfoils
Max thickness 10.5% at 40.2% chord
Max camber 1.8% at 50% chord
Source UIUC Airfoil Coordinates Database

(c141f-il) LOCKHEED C-141 BL958.89 AIRFOIL

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LOCKHEED C-141 BL958.89 AIRFOILLockheed-Georgia C-141 transonic wing airfoils
Max thickness 10% at 40.2% chord
Max camber 2.3% at 45.1% chord
Source UIUC Airfoil Coordinates Database

(c5a-il) LOCKHEED C-5A BL0 AIRFOIL

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LOCKHEED C-5A BL0 AIRFOILLockheed-Georgia C-5A transonic wing airfoils
Max thickness 13.1% at 40% chord
Max camber 0.7% at 85% chord
Source UIUC Airfoil Coordinates Database

(c5b-il) LOCKHEED C-5A BL488.2 AIRFOIL

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LOCKHEED C-5A BL488.2 AIRFOILLockheed-Georgia C-5A transonic wing airfoils
Max thickness 11.5% at 40% chord
Max camber 1.2% at 70% chord
Source UIUC Airfoil Coordinates Database

(c5c-il) LOCKHEED C-5A BL576 AIRFOIL

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LOCKHEED C-5A BL576 AIRFOILLockheed-Georgia C-5A transonic wing airfoils
Max thickness 11.1% at 40% chord
Max camber 1.4% at 65% chord
Source UIUC Airfoil Coordinates Database

(c5d-il) LOCKHEED C-5A BL758.6 AIRFOIL

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LOCKHEED C-5A BL758.6 AIRFOILLockheed-Georgia C-5A transonic wing airfoils
Max thickness 11.1% at 40% chord
Max camber 1.4% at 60% chord
Source UIUC Airfoil Coordinates Database

(c5e-il) LOCKHEED C-5A BL1256 AIRFOIL

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LOCKHEED C-5A BL1256 AIRFOILLockheed-Georgia C-5A transonic wing airfoils
Max thickness 10.8% at 40% chord
Max camber 1.4% at 30% chord
Source UIUC Airfoil Coordinates Database

(cap21c-il) CAP 21 (TraCFoil)

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CAP 21   (TraCFoil)CAP 21 (TraCFoil) airfoil
Max thickness 15.6% at 15.7% chord
Max camber 0.6% at 23.9% chord
Source UIUC Airfoil Coordinates Database

(cast102-il) CAST 10-2/DOA 2 AIRFOIL

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CAST 10-2/DOA 2 AIRFOILCAST 10-2/DOA 2 transonic airfoil
Max thickness 12.2% at 45.4% chord
Max camber 1.5% at 69.4% chord
Source UIUC Airfoil Coordinates Database

(ch10sm-il) CH10 (smoothed)

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CH10 (smoothed)Chuch Hollinger CH 10-48-13 high lift low Reynolds number airfoil
Max thickness 12.8% at 30.6% chord
Max camber 10.2% at 49.3% chord
Source UIUC Airfoil Coordinates Database

(chen-il) CHEN AIRFOIL

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CHEN AIRFOILUniversity of Illinois at Urbana-Champaign / Chen high lift airfoil
Max thickness 12.5% at 27.7% chord
Max camber 7.8% at 25.4% chord
Source UIUC Airfoil Coordinates Database

(clarkk-il) CLARK K AIRFOIL

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CLARK K AIRFOILCLARK K airfoil
Max thickness 11.7% at 29.7% chord
Max camber 3.3% at 39.6% chord
Source UIUC Airfoil Coordinates Database

(clarkv-il) CLARK V AIRFOIL

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CLARK V AIRFOILCLARK V airfoil
Max thickness 11.6% at 30% chord
Max camber 3.4% at 50% chord
Source UIUC Airfoil Coordinates Database

(clarkw-il) CLARK W AIRFOIL

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CLARK W AIRFOILCLARK W airfoil
Max thickness 11.2% at 30% chord
Max camber 3.7% at 40% chord
Source UIUC Airfoil Coordinates Database

(clarkx-il) CLARK X AIRFOIL

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CLARK X AIRFOILCLARK X airfoil
Max thickness 11.7% at 30% chord
Max camber 3.3% at 40% chord
Source UIUC Airfoil Coordinates Database

(clarky-il) CLARK Y AIRFOIL

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CLARK Y AIRFOILCLARK Y airfoil
Max thickness 11.7% at 28% chord
Max camber 3.4% at 42% chord
Source UIUC Airfoil Coordinates Database
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