EPPLER 343 AIRFOIL (e343-il)
EPPLER 343 AIRFOIL - Eppler E343 flying wing airfoil
| Details | Dat file | Parser | |
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(e343-il) EPPLER 343 AIRFOIL Eppler E343 flying wing airfoil Max thickness 14.5% at 30.9% chord. Max camber 4% at 26% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 343 AIRFOIL
34. 39.
0.0000100 -.0002600
0.0000900 0.0023500
0.0004700 0.0047800
0.0044800 0.0152300
0.0124600 0.0267800
0.0243400 0.0388700
0.0400400 0.0510400
0.0594400 0.0629200
0.0823900 0.0742000
0.1086700 0.0845500
0.1380700 0.0936800
0.1703300 0.1012900
0.2052200 0.1070400
0.2425600 0.1106200
0.2823000 0.1117100
0.3246500 0.1102900
0.3695400 0.1067400
0.4166200 0.1014300
0.4654600 0.0946800
0.5155800 0.0868200
0.5664300 0.0781800
0.6174200 0.0691100
0.6678900 0.0599300
0.7171299 0.0509400
0.7644400 0.0424000
0.8090700 0.0345000
0.8503000 0.0273900
0.8874600 0.0211200
0.9199100 0.0156900
0.9470600 0.0109200
0.9688100 0.0065300
0.9853500 0.0028300
0.9961600 0.0006300
1.0000000 0.0000000
0.0000100 -.0002600
0.0001500 -.0018800
0.0004700 -.0033700
0.0007000 -.0040600
0.0009800 -.0047100
0.0013300 -.0052900
0.0017800 -.0058200
0.0023300 -.0063400
0.0029600 -.0068400
0.0044600 -.0078100
0.0062500 -.0087400
0.0094200 -.0100700
0.0196800 -.0131300
0.0388000 -.0166800
0.0637400 -.0196400
0.0941800 -.0222100
0.1296600 -.0246700
0.1694900 -.0271200
0.2130100 -.0295400
0.2595700 -.0318300
0.3085800 -.0338500
0.3594800 -.0355200
0.4117000 -.0367700
0.4646600 -.0375800
0.5177500 -.0378900
0.5703700 -.0376900
0.6219300 -.0369400
0.6718400 -.0356100
0.7195400 -.0336600
0.7644700 -.0310200
0.8060700 -.0274400
0.8443800 -.0224900
0.8799400 -.0165000
0.9126600 -.0106200
0.9516900 -.0057500
0.9659900 -.0023500
0.9844500 -.0005500
0.9960400 -.0000100
1.0000000 0.0000000
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Polars for EPPLER 343 AIRFOIL (e343-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e343-il | 50,000 | 9 | 14.5 at α=-0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e343-il | 50,000 | 5 | 24.3 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e343-il | 100,000 | 9 | 30.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e343-il | 100,000 | 5 | 43.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e343-il | 200,000 | 9 | 58.7 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e343-il | 200,000 | 5 | 64.6 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e343-il | 500,000 | 9 | 92.6 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e343-il | 500,000 | 5 | 87.9 at α=10.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e343-il | 1,000,000 | 9 | 114.4 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e343-il | 1,000,000 | 5 | 113.4 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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