EPPLER 485 AIRFOIL (e485-il)
EPPLER 485 AIRFOIL - Eppler E485 tailplane airfoil
| Details | Dat file | Parser | |
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(e485-il) EPPLER 485 AIRFOIL Eppler E485 tailplane airfoil Max thickness 12.5% at 31.8% chord. Max camber 1.1% at 27.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 485 AIRFOIL
35. 38.
0.0000100 0.0004100
0.0000800 0.0011100
0.0003800 0.0025800
0.0008800 0.0041200
0.0019800 0.0065500
0.0062200 0.0127000
0.0158600 0.0216300
0.0298000 0.0305800
0.0479800 0.0391600
0.0703000 0.0471100
0.0966700 0.0542200
0.1269200 0.0603400
0.1608400 0.0653500
0.1982100 0.0692000
0.2387000 0.0718700
0.2819400 0.0733700
0.3275300 0.0736900
0.3750200 0.0728700
0.4239600 0.0709300
0.4738700 0.0679200
0.5242900 0.0639100
0.5747400 0.0590000
0.6247700 0.0533100
0.6739000 0.0470200
0.7216700 0.0403500
0.7676100 0.0336000
0.8111300 0.0270900
0.8515500 0.0211100
0.8882000 0.0158100
0.9204300 0.0112700
0.9476600 0.0074600
0.9695500 0.0042300
0.9859600 0.0017500
0.9963800 0.0003800
1.0000000 0.0000000
0.0000100 0.0004100
0.0000100 -.0002600
0.0000700 -.0008900
0.0002300 -.0015100
0.0004700 -.0021400
0.0007900 -.0027800
0.0015900 -.0040800
0.0026300 -.0053900
0.0045600 -.0073700
0.0068300 -.0092500
0.0182100 -.0159500
0.0345600 -.0223400
0.0557600 -.0282300
0.0816500 -.0335600
0.1119700 -.0382600
0.1464100 -.0423000
0.1846200 -.0456500
0.2261900 -.0482900
0.2706800 -.0502200
0.3175900 -.0514100
0.3664100 -.0518500
0.4166200 -.0515400
0.4676800 -.0504800
0.5190200 -.0486600
0.5701300 -.0460700
0.6204900 -.0427100
0.6696399 -.0386000
0.7172000 -.0338200
0.7627700 -.0285400
0.8059400 -.0229900
0.8462900 -.0174400
0.8833700 -.0122500
0.9165699 -.0078500
0.9451000 -.0044400
0.9682900 -.0020400
0.9855700 -.0006300
0.9963300 -.0000800
1.0000000 0.0000000
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Polars for EPPLER 485 AIRFOIL (e485-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e485-il | 50,000 | 9 | 27.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e485-il | 50,000 | 5 | 30.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e485-il | 100,000 | 9 | 44.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e485-il | 100,000 | 5 | 44.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e485-il | 200,000 | 9 | 59.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e485-il | 200,000 | 5 | 55.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e485-il | 500,000 | 9 | 73.8 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e485-il | 500,000 | 5 | 69 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e485-il | 1,000,000 | 9 | 86.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e485-il | 1,000,000 | 5 | 81.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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