EPPLER 543 AIRFOIL (e543-il)
EPPLER 543 AIRFOIL - Eppler E543 general aviation airfoil
| Details | Dat file | Parser | |
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(e543-il) EPPLER 543 AIRFOIL Eppler E543 general aviation airfoil Max thickness 17.2% at 40.7% chord. Max camber 1.9% at 31% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 543 AIRFOIL
36. 37.
0.0000100 -.0001800
0.0000200 0.0005400
0.0002200 0.0020700
0.0006300 0.0037000
0.0016200 0.0062900
0.0029400 0.0088600
0.0105800 0.0185600
0.0227400 0.0288900
0.0392600 0.0394000
0.0600000 0.0497700
0.0847700 0.0597500
0.1133700 0.0691000
0.1455300 0.0776500
0.1809400 0.0852400
0.2192600 0.0917200
0.2601200 0.0969600
0.3030800 0.1008400
0.3477200 0.1032600
0.3935300 0.1040400
0.4401300 0.1029400
0.4873500 0.0997600
0.5351400 0.0945800
0.5833300 0.0877800
0.6314700 0.0797800
0.6790600 0.0709200
0.7256000 0.0615700
0.7704901 0.0520800
0.8131400 0.0428100
0.8529000 0.0340600
0.8891000 0.0261000
0.9210600 0.0191000
0.9481400 0.0131600
0.9697400 0.0081800
0.9857399 0.0039200
0.9962000 0.0009800
1.0000000 0.0000000
0.0000100 -.0001800
0.0000500 -.0008600
0.0001800 -.0015000
0.0004200 -.0021200
0.0007500 -.0027500
0.0011700 -.0033900
0.0022200 -.0046800
0.0035300 -.0060000
0.0059600 -.0080300
0.0138000 -.0129900
0.0293700 -.0199700
0.0500800 -.0268000
0.0756500 -.0333700
0.1057900 -.0395800
0.1401400 -.0454100
0.1782400 -.0508300
0.2195900 -.0557500
0.2636700 -.0600900
0.3099200 -.0637200
0.3578000 -.0665600
0.4067300 -.0684800
0.4561400 -.0693600
0.5054400 -.0690600
0.5540600 -.0674100
0.6013700 -.0639800
0.6474000 -.0581000
0.6927201 -.0497400
0.7379100 -.0396700
0.7828400 -.0293200
0.8264601 -.0199200
0.8675900 -.0120900
0.9049900 -.0062000
0.9374700 -.0023100
0.9639900 -.0002100
0.9837101 0.0004600
0.9958799 0.0002400
1.0000000 0.0000000
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Polars for EPPLER 543 AIRFOIL (e543-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e543-il | 50,000 | 9 | 21.3 at α=12.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e543-il | 50,000 | 5 | 17.9 at α=11.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e543-il | 100,000 | 9 | 42.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e543-il | 100,000 | 5 | 35.3 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e543-il | 200,000 | 9 | 56.6 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e543-il | 200,000 | 5 | 58.6 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e543-il | 500,000 | 9 | 86.2 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e543-il | 500,000 | 5 | 82.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e543-il | 1,000,000 | 9 | 108.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e543-il | 1,000,000 | 5 | 98.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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