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Airfoil database list (L).

LIEBECK L1003 AIRFOIL to LWK 79-100

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(l1003-il) LIEBECK L1003 AIRFOIL

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LIEBECK L1003 AIRFOILLiebeck high lift airfoil
Max thickness 17.7% at 30% chord
Max camber 6.5% at 30% chord
Source UIUC Airfoil Coordinates Database

(l188root-il) LOCKHEED L-188 ROOT AIRFOIL

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LOCKHEED L-188 ROOT AIRFOILLockheed L-188/P-3 root airfoil NACA 0014 -1.10 40/1.051 Cli=.3 a=.8
Max thickness 14% at 41.3% chord
Max camber 2% at 51.7% chord
Source UIUC Airfoil Coordinates Database

(l188tip-il) LOCKHEED L-188 TIP AIRFOIL

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LOCKHEED L-188 TIP AIRFOILLockheed L-188/P-3 tip airfoil NACA 0012 -1.10 40/1.051 Cli=.4 a=.8
Max thickness 12% at 41.3% chord
Max camber 2.7% at 51.7% chord
Source UIUC Airfoil Coordinates Database

(l7769-il) LISSAMAN 7769 AIRFOIL

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LISSAMAN 7769 AIRFOILLissaman 7769 human powered aircraft airfoil
Max thickness 11% at 30% chord
Max camber 4.4% at 30% chord
Source UIUC Airfoil Coordinates Database

(la203a-il) DOUGLAS LA203A AIRFOIL

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DOUGLAS LA203A AIRFOILDouglas/Liebeck LA203A high lift airfoil
Max thickness 15.7% at 34.3% chord
Max camber 5.5% at 46% chord
Source UIUC Airfoil Coordinates Database

(la2573a-il) LA2573A

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LA2573ALiebeck LA2573A airfoil
Max thickness 13.7% at 28.8% chord
Max camber 3.2% at 26.1% chord
Source UIUC Airfoil Coordinates Database

(la5055-il) LIEBECK LA5055 AIRFOIL

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LIEBECK LA5055 AIRFOILLiebeck high lift airfoil
Max thickness 15.9% at 35% chord
Max camber 5.9% at 40% chord
Source UIUC Airfoil Coordinates Database

(lds2-il) LDS-2 AIRFOIL

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LDS-2 AIRFOILLDS-2 airfoil
Max thickness 12% at 34.9% chord
Max camber 2.2% at 45% chord
Source UIUC Airfoil Coordinates Database

(lg10sc-il) LOCKHEED-GEORGIA SUPERCRITICAL AIRFOIL

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LOCKHEED-GEORGIA SUPERCRITICAL AIRFOILLockheed-Georgia/NASA/Blackwell rotorcraft airfoil
Max thickness 10% at 32% chord
Max camber 1.5% at 16% chord
Source UIUC Airfoil Coordinates Database

(lnv109a-il) LNV109A

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LNV109ADouglas/Liebeck LNV109A high lift airfoil
Max thickness 13% at 23.5% chord
Max camber 6% at 31.5% chord
Source UIUC Airfoil Coordinates Database

(lrn1007-il) lrn1007

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lrn1007LRN(1)-1007 low Reynolds number airfoil
Max thickness 7.3% at 39.8% chord
Max camber 5.9% at 44.6% chord
Source UIUC Airfoil Coordinates Database

(lrn1015-il) NASA LRN 1015 (NASA TM 102840)

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NASA LRN 1015 (NASA TM 102840)LRN 1015 airfoil used on the Northrop Grumman RQ-4 Global Hawk airfoil
Max thickness 15.2% at 40% chord
Max camber 4.9% at 44% chord
Source UIUC Airfoil Coordinates Database

(ls013-il) NASA/LANGLEY LS(1)-0013 AIRFOIL

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NASA/LANGLEY LS(1)-0013 AIRFOILNASA/Langley LS(1)-0013 general aviation airfoil
Max thickness 12.9% at 40% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database

(ls413-il) NASA/LANGLEY LS(1)-0413 (GA(W)-2) AIRFOIL

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NASA/LANGLEY LS(1)-0413 (GA(W)-2) AIRFOILNASA/Langley LS(1)-0413 (GA(W)-2) general aviation airfoil
Max thickness 12.9% at 37.5% chord
Max camber 2.4% at 65% chord
Source UIUC Airfoil Coordinates Database

(ls413mod-il) NASA/LANGLEY LS(1)-0413MOD AIRFOIL

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NASA/LANGLEY LS(1)-0413MOD AIRFOILNASA/Langley LS(1)-0413MOD general aviation airfoil
Max thickness 13% at 35% chord
Max camber 2.2% at 40% chord
Source UIUC Airfoil Coordinates Database

(ls417-il) NASA/LANGLEY LS(1)-0417 (GA(W)-1) AIRFOIL

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NASA/LANGLEY LS(1)-0417 (GA(W)-1) AIRFOILNASA/Langley/Whitcomb LS(1)-0417 (GA(W)-1) general aviation airfoil
Max thickness 17% at 40% chord
Max camber 2.4% at 65% chord
Source UIUC Airfoil Coordinates Database

(ls417mod-il) NASA/LANGLEY LS(1)-0417MOD AIRFOIL

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NASA/LANGLEY LS(1)-0417MOD AIRFOILNASA/Langley LS(1)-0417MOD general aviation airfoil
Max thickness 17% at 30.2% chord
Max camber 2.3% at 20.2% chord
Source UIUC Airfoil Coordinates Database

(ls421-il) NASA/LANGLEY LS(1)-0421 AIRFOIL

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NASA/LANGLEY LS(1)-0421 AIRFOILNASA/Langley LS(1)-0421 general aviation airfoil
Max thickness 20.9% at 40% chord
Max camber 2.4% at 65% chord
Source UIUC Airfoil Coordinates Database

(ls421mod-il) NASA/LANGLEY LS(1)-0421MOD AIRFOIL

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NASA/LANGLEY LS(1)-0421MOD AIRFOILNASA/Langley LS(1)-0421MOD general aviation airfoil
Max thickness 21% at 32.5% chord
Max camber 2.3% at 30% chord
Source UIUC Airfoil Coordinates Database

(lwk79100-il) LWK 79-100

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LWK 79-100LWK 79-100 symmetrical airfoil
Max thickness 10% at 27.9% chord
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
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