EPPLER 545 AIRFOIL (e545-il)
EPPLER 545 AIRFOIL - Eppler E545 general aviation airfoil
| Details | Dat file | Parser | |
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(e545-il) EPPLER 545 AIRFOIL Eppler E545 general aviation airfoil Max thickness 17.4% at 39.3% chord. Max camber 1.8% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 545 AIRFOIL
36. 37.
0.0000100 -.0001300
0.0000200 0.0006200
0.0002300 0.0022000
0.0006600 0.0038800
0.0016600 0.0065400
0.0035500 0.0101100
0.0116800 0.0201300
0.0242800 0.0307100
0.0411900 0.0414300
0.0622600 0.0519700
0.0873100 0.0620700
0.1161200 0.0715100
0.1448300 0.0800900
0.1839100 0.0876500
0.2222400 0.0940500
0.2630300 0.0991300
0.3058600 0.1027600
0.3502800 0.1047800
0.3959400 0.1049500
0.4426100 0.1031200
0.4901700 0.0992800
0.5384400 0.0937500
0.5869900 0.0868500
0.6353500 0.0788800
0.6830400 0.0701500
0.7295200 0.0609900
0.7742299 0.0517200
0.8165600 0.0426700
0.8558800 0.0341100
0.8915700 0.0262900
0.9229700 0.0193600
0.9495000 0.0134400
0.9705800 0.0084000
0.9861500 0.0040600
0.9963100 0.0010300
1.0000000 0.0000000
0.0000100 -.0001300
0.0000400 -.0008400
0.0001700 -.0015100
0.0004000 -.0021600
0.0007300 -.0028200
0.0011400 -.0034900
0.0021700 -.0048500
0.0034600 -.0062400
0.0058500 -.0083800
0.0123600 -.0129000
0.0271700 -.0202900
0.0470300 -.0275600
0.0716600 -.0345700
0.1007600 -.0411900
0.1339900 -.0473700
0.1708800 -.0530600
0.2109600 -.0581200
0.2536900 -.0624600
0.2985600 -.0659100
0.3450200 -.0683300
0.3925000 -.0695400
0.4404400 -.0693400
0.4882100 -.0672400
0.5358900 -.0625300
0.5840600 -.0552700
0.6330400 -.0462000
0.6825900 -.0364600
0.7318600 -.0270000
0.7798700 -.0184400
0.8255800 -.0112500
0.8679400 -.0057100
0.9058700 -.0019000
0.9384100 0.0002900
0.9647000 0.0011300
0.9840800 0.0009900
0.9959900 0.0003600
1.0000000 0.0000000
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Polars for EPPLER 545 AIRFOIL (e545-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e545-il | 50,000 | 9 | 6.7 at α=13.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e545-il | 50,000 | 5 | 19.2 at α=11.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e545-il | 100,000 | 9 | 43.3 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e545-il | 100,000 | 5 | 42.9 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e545-il | 200,000 | 9 | 64.3 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e545-il | 200,000 | 5 | 63.6 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e545-il | 500,000 | 9 | 91 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e545-il | 500,000 | 5 | 81.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e545-il | 1,000,000 | 9 | 106.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e545-il | 1,000,000 | 5 | 85 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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