EPPLER 337 AIRFOIL (e337-il)
EPPLER 337 AIRFOIL - Eppler E337 flying wing airfoil
| Details | Dat file | Parser | |
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(e337-il) EPPLER 337 AIRFOIL Eppler E337 flying wing airfoil Max thickness 13.1% at 32% chord. Max camber 3.2% at 22.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 337 AIRFOIL
34. 40.
0.0000200 0.0007200
0.0002900 0.0031800
0.0029100 0.0105800
0.0098700 0.0208500
0.0208100 0.0317200
0.0356900 0.0427400
0.0543800 0.0535300
0.0767400 0.0637700
0.1025800 0.0731700
0.1025800 0.0731700
0.1316800 0.0814300
0.1638100 0.0882700
0.1987500 0.0933800
0.2363600 0.0965000
0.2765400 0.0974000
0.3193600 0.0960800
0.3647300 0.0928500
0.4122600 0.0880300
0.4615300 0.0819200
0.5120700 0.0748000
0.5633300 0.0670100
0.6147000 0.0588600
0.6655200 0.0506500
0.7151100 0.0426700
0.7627300 0.0351500
0.8076800 0.0282700
0.8492200 0.0221500
0.8866700 0.0168400
0.9194000 0.0123400
0.9468500 0.0084700
0.9688500 0.0049600
0.9854700 0.0020800
0.9962200 0.0004400
1.0000000 0.0000000
0.0000200 0.0007200
0.0000500 -.0008100
0.0002500 -.0022100
0.0004200 -.0028600
0.0006400 -.0034700
0.0009300 -.0040100
0.0013100 -.0045200
0.0018000 -.0050100
0.0023700 -.0054900
0.0037300 -.0064300
0.0053700 -.0073500
0.0083100 -.0087100
0.0105100 -.0095700
0.0253800 -.0136300
0.0460700 -.0171300
0.0723000 -.0201400
0.1038000 -.0228300
0.1400800 -.0254200
0.1805000 -.0280100
0.2244200 -.0305400
0.2712200 -.0329200
0.3202900 -.0350200
0.3711100 -.0367400
0.4231100 -.0380200
0.4757200 -.0388200
0.5283600 -.0391100
0.5804300 -.0388600
0.6313700 -.0380500
0.6806000 -.0366400
0.7275800 -.0346100
0.7717600 -.0319000
0.8126300 -.0283100
0.8501600 -.0234400
0.8848100 -.0176400
0.9164500 -.0119300
0.9442700 -.0070600
0.9674100 -.0033900
0.9850300 -.0011200
0.9961700 -.0001700
1.0000000 0.0000000
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Polars for EPPLER 337 AIRFOIL (e337-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e337-il | 50,000 | 9 | 16 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e337-il | 50,000 | 5 | 25.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e337-il | 100,000 | 9 | 34.4 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e337-il | 100,000 | 5 | 45.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e337-il | 200,000 | 9 | 62.7 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e337-il | 200,000 | 5 | 65.7 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e337-il | 500,000 | 9 | 92.6 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e337-il | 500,000 | 5 | 84.1 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e337-il | 1,000,000 | 9 | 107.3 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e337-il | 1,000,000 | 5 | 103.9 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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