EPPLER 552 AIRFOIL (e552-il)
EPPLER 552 AIRFOIL - Eppler E552 general aviation airfoil
| Details | Dat file | Parser | |
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(e552-il) EPPLER 552 AIRFOIL Eppler E552 general aviation airfoil Max thickness 18.4% at 32.4% chord. Max camber 2.6% at 51.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 552 AIRFOIL
35. 37.
0.0000100 0.0004400
0.0001500 0.0022100
0.0004600 0.0040900
0.0013600 0.0070600
0.0048000 0.0141400
0.0136400 0.0255600
0.0267400 0.0374800
0.0439500 0.0495100
0.0651100 0.0612900
0.0900100 0.0725400
0.1184300 0.0830100
0.1500900 0.0924600
0.1846800 0.1007000
0.2218700 0.1075000
0.2612600 0.1126700
0.3024400 0.1159300
0.3451200 0.1169300
0.3892400 0.1153000
0.4350600 0.1110600
0.4825900 0.1047800
0.5313400 0.0970300
0.5807900 0.0882000
0.6303600 0.0786800
0.6793900 0.0688400
0.7272300 0.0590200
0.7731800 0.0495100
0.8165100 0.0405600
0.8565500 0.0323400
0.8926200 0.0249800
0.9241101 0.0185400
0.9504901 0.0130100
0.9712700 0.0082500
0.9865200 0.0040500
0.9964100 0.0010400
1.0000000 0.0000000
0.0000100 0.0004400
0.0000300 -.0004000
0.0001100 -.0012100
0.0002700 -.0019700
0.0005300 -.0027100
0.0013300 -.0042200
0.0024200 -.0057500
0.0037700 -.0073200
0.0062300 -.0097100
0.0095400 -.0124000
0.0230000 -.0205300
0.0414500 -.0285500
0.0645700 -.0362400
0.0920500 -.0434200
0.1235200 -.0500100
0.1585600 -.0558700
0.1966800 -.0608300
0.2373700 -.0646900
0.2801200 -.0672000
0.3243800 -.0679100
0.3700600 -.0662000
0.4175000 -.0618800
0.4669900 -.0553900
0.5183800 -.0475300
0.5710600 -.0390200
0.6243200 -.0304100
0.6773500 -.0222200
0.7292700 -.0148400
0.7791500 -.0086000
0.8260400 -.0037300
0.8689900 -.0003100
0.9070700 0.0016900
0.9394600 0.0024300
0.9654500 0.0022200
0.9844800 0.0014100
0.9961000 0.0004500
1.0000000 0.0000000
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Polars for EPPLER 552 AIRFOIL (e552-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e552-il | 50,000 | 9 | 11 at α=-3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e552-il | 50,000 | 5 | 13.3 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e552-il | 100,000 | 9 | 31.2 at α=12.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e552-il | 100,000 | 5 | 43.1 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e552-il | 200,000 | 9 | 70.3 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e552-il | 200,000 | 5 | 70.7 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e552-il | 500,000 | 9 | 106.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e552-il | 500,000 | 5 | 100.5 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e552-il | 1,000,000 | 9 | 131 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e552-il | 1,000,000 | 5 | 119.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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