EPPLER 342 AIRFOIL (e342-il)
EPPLER 342 AIRFOIL - Eppler E342 flying wing airfoil
| Details | Dat file | Parser | |
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(e342-il) EPPLER 342 AIRFOIL Eppler E342 flying wing airfoil Max thickness 14.3% at 31.8% chord. Max camber 3.5% at 22.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 342 AIRFOIL
33. 39.
0.0000100 0.0003600
0.0001900 0.0029800
0.0031600 0.0121200
0.0103000 0.0231500
0.0213800 0.0347900
0.0363500 0.0465600
0.0550800 0.0581000
0.0774200 0.0690800
0.1031600 0.0791700
0.1320800 0.0880700
0.1639500 0.0954800
0.1985400 0.1010800
0.2356700 0.1045500
0.2753100 0.1055800
0.3176300 0.1041500
0.3625700 0.1006400
0.4097700 0.0954200
0.4588300 0.0888000
0.5092400 0.0811000
0.5604700 0.0726700
0.6119100 0.0638600
0.6628800 0.0549900
0.7126900 0.0463700
0.7606000 0.0382400
0.8058500 0.0307900
0.8477100 0.0241700
0.8854800 0.0184300
0.9185000 0.0135400
0.9461800 0.0093200
0.9683800 0.0054900
0.9852101 0.0023200
0.9961400 0.0004900
1.0000000 0.0000000
0.0000100 0.0003600
0.0000900 -.0012700
0.0003500 -.0027600
0.0005500 -.0034600
0.0008000 -.0041100
0.0011100 -.0047000
0.0015300 -.0052400
0.0020400 -.0057700
0.0026500 -.0062900
0.0040800 -.0073100
0.0057900 -.0083100
0.0088500 -.0097700
0.0242300 -.0145600
0.0446800 -.0184600
0.0707200 -.0218500
0.1020600 -.0249000
0.1382000 -.0278400
0.1785100 -.0307400
0.2223300 -.0335500
0.2690400 -.0361700
0.3180500 -.0384600
0.3688200 -.0403300
0.4207800 -.0417200
0.4733700 -.0425800
0.5259900 -.0428900
0.5780600 -.0426100
0.6290000 -.0417100
0.6782300 -.0401600
0.7252100 -.0379300
0.7694000 -.0349600
0.8102600 -.0310300
0.8478000 -.0256900
0.8825800 -.0192800
0.9145300 -.0129400
0.9428300 -.0075400
0.9665200 -.0035200
0.9846200 -.0011200
0.9960700 0.0001600
1.0000000 0.0000000
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Polars for EPPLER 342 AIRFOIL (e342-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e342-il | 50,000 | 9 | 14.6 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e342-il | 50,000 | 5 | 24.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e342-il | 100,000 | 9 | 30.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e342-il | 100,000 | 5 | 43.5 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e342-il | 200,000 | 9 | 59.4 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e342-il | 200,000 | 5 | 61.9 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e342-il | 500,000 | 9 | 88.3 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e342-il | 500,000 | 5 | 83.7 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e342-il | 1,000,000 | 9 | 108.3 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e342-il | 1,000,000 | 5 | 106.3 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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