EPPLER 546 AIRFOIL (e546-il)
EPPLER 546 AIRFOIL - Eppler E546 general aviation airfoil
| Details | Dat file | Parser | |
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(e546-il) EPPLER 546 AIRFOIL Eppler E546 general aviation airfoil Max thickness 16.2% at 40.3% chord. Max camber 1.8% at 26.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 546 AIRFOIL
36. 37.
0.0000100 -.0001600
0.0000200 0.0005500
0.0002200 0.0020500
0.0006300 0.0036400
0.0016100 0.0061800
0.0028500 0.0085900
0.0103600 0.0180800
0.0223400 0.0281800
0.0386400 0.0384400
0.0591300 0.0485500
0.0836100 0.0582300
0.1118800 0.0672500
0.1436800 0.0754400
0.1787100 0.0826200
0.2166300 0.0886200
0.2570500 0.0933100
0.2995600 0.0964800
0.3438500 0.0979000
0.3896800 0.0974500
0.4368900 0.0951500
0.4852000 0.0912100
0.5342000 0.0858500
0.5834600 0.0793100
0.6324900 0.0718400
0.6807900 0.0637400
0.7278100 0.0552900
0.7729800 0.0468000
0.8156900 0.0385500
0.8553100 0.0307900
0.8912100 0.0237300
0.9227600 0.0175000
0.9493800 0.0121800
0.9705300 0.0076400
0.9861400 0.0036900
0.9963100 0.0009300
1.0000000 0.0000000
0.0000100 -.0001600
0.0000500 -.0008300
0.0001800 -.0014600
0.0004100 -.0020700
0.0007400 -.0026800
0.0011500 -.0033100
0.0021800 -.0045800
0.0034800 -.0058700
0.0058700 -.0078600
0.0138000 -.0128100
0.0292500 -.0196500
0.0498000 -.0263300
0.0751600 -.0327300
0.1050400 -.0387700
0.1390900 -.0444000
0.1768600 -.0496000
0.2178400 -.0542800
0.2615300 -.0583300
0.3073700 -.0616600
0.3548100 -.0641300
0.4033000 -.0656200
0.4522500 -.0659800
0.5010900 -.0650300
0.5491900 -.0623300
0.5965800 -.0572300
0.6438100 -.0497400
0.6912600 -.0406800
0.7386200 -.0312400
0.7849700 -.0223800
0.8292800 -.0146600
0.8704799 -.0084800
0.9075000 -.0039900
0.9393400 -.0011600
0.9651500 0.0002600
0.9842500 0.0005900
0.9960200 0.0002600
1.0000000 0.0000000
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Polars for EPPLER 546 AIRFOIL (e546-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e546-il | 50,000 | 9 | 8.9 at α=13.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e546-il | 50,000 | 5 | 21.6 at α=10.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e546-il | 100,000 | 9 | 44.8 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e546-il | 100,000 | 5 | 43.3 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e546-il | 200,000 | 9 | 61.2 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e546-il | 200,000 | 5 | 61.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e546-il | 500,000 | 9 | 87.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e546-il | 500,000 | 5 | 82.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e546-il | 1,000,000 | 9 | 106.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e546-il | 1,000,000 | 5 | 96.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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