EPPLER 583 AIRFOIL (e583-il)
EPPLER 583 AIRFOIL - Eppler E583 sailplane airfoil
| Details | Dat file | Parser | |
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(e583-il) EPPLER 583 AIRFOIL Eppler E583 sailplane airfoil Max thickness 16.5% at 38% chord. Max camber 4.5% at 38% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 583 AIRFOIL
35. 38.
0.0000100 0.0002700
0.0001300 0.0019400
0.0006700 0.0046400
0.0022200 0.0090500
0.0087800 0.0198600
0.0195200 0.0316200
0.0343400 0.0438400
0.0531300 0.0561100
0.0757300 0.0681400
0.1019700 0.0796200
0.1316200 0.0903100
0.1644300 0.0999900
0.2001300 0.1084700
0.2383800 0.1155700
0.2788300 0.1211500
0.3210800 0.1250600
0.3647700 0.1271300
0.4099500 0.1272700
0.4550500 0.1254000
0.5008700 0.1213900
0.5468500 0.1149900
0.5932200 0.1063900
0.6398500 0.0962700
0.6862100 0.0852600
0.7316900 0.0738400
0.7756500 0.0624400
0.8174100 0.0514200
0.8562800 0.0410900
0.8915600 0.0316800
0.9226000 0.0233400
0.9487500 0.0160400
0.9697600 0.0095900
0.9857700 0.0043000
0.9962600 0.0010300
1.0000000 0.0000000
0.0000100 0.0002700
0.0000700 -.0012800
0.0001700 -.0020000
0.0003400 -.0026800
0.0005800 -.0032900
0.0009200 -.0038700
0.0013700 -.0044500
0.0019000 -.0050200
0.0031900 -.0061500
0.0047500 -.0072800
0.0075600 -.0089500
0.0140900 -.0119500
0.0303600 -.0169900
0.0521400 -.0213900
0.0791400 -.0251600
0.1110900 -.0283200
0.1475800 -.0309700
0.1881400 -.0331500
0.2322500 -.0348900
0.2793500 -.0362100
0.3288300 -.0371100
0.3800700 -.0375700
0.4324300 -.0375600
0.4852600 -.0370300
0.5379000 -.0359200
0.5897100 -.0341100
0.6400100 -.0313300
0.6886300 -.0271200
0.7357800 -.0215600
0.7814500 -.0152300
0.8253700 -.0089100
0.8668100 -.0035600
0.9046200 0.0002300
0.9375700 0.0022200
0.9644400 0.0025000
0.9841400 0.0016400
0.9960400 0.0005100
1.0000000 0.0000000
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Polars for EPPLER 583 AIRFOIL (e583-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e583-il | 50,000 | 9 | 4.8 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e583-il | 50,000 | 5 | 11.5 at α=11.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e583-il | 100,000 | 9 | 32.2 at α=12.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e583-il | 100,000 | 5 | 32.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e583-il | 200,000 | 9 | 70.4 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e583-il | 200,000 | 5 | 70 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e583-il | 500,000 | 9 | 111.5 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e583-il | 500,000 | 5 | 107.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e583-il | 1,000,000 | 9 | 143.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e583-il | 1,000,000 | 5 | 132 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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