EPPLER 472 AIRFOIL (e472-il)
EPPLER 472 AIRFOIL - Eppler E472 aerobatic aircraft airfoil
| Details | Dat file | Parser | |
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(e472-il) EPPLER 472 AIRFOIL Eppler E472 aerobatic aircraft airfoil Max thickness 12.1% at 17.5% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 472 AIRFOIL
31. 31.
0.0000000 0.0000000
0.0026200 0.0092900
0.0099400 0.0192400
0.0213300 0.0290300
0.0367000 0.0381000
0.0560300 0.0459900
0.0793800 0.0523600
0.1068300 0.0569500
0.1385100 0.0596000
0.1746200 0.0604900
0.2149900 0.0601300
0.2590600 0.0588400
0.3062800 0.0568000
0.3560500 0.0541500
0.4077600 0.0510300
0.4607800 0.0475400
0.5144600 0.0437900
0.5681400 0.0398700
0.6211600 0.0358700
0.6728800 0.0318600
0.7226600 0.0279100
0.7698800 0.0240700
0.8139600 0.0203900
0.8543400 0.0169100
0.8905000 0.0136400
0.9219800 0.0105900
0.9483400 0.0076400
0.9695200 0.0046400
0.9856700 0.0019700
0.9962400 0.0004100
1.0000000 0.0000000
0.0000000 0.0000000
0.0026200 -.0092900
0.0099400 -.0192400
0.0213300 -.0290300
0.0367000 -.0381000
0.0560300 -.0459900
0.0793800 -.0523600
0.1068300 -.0569500
0.1385100 -.0596000
0.1746200 -.0604900
0.2149900 -.0601300
0.2590600 -.0588400
0.3062800 -.0568000
0.3560500 -.0541500
0.4077600 -.0510300
0.4607800 -.0475400
0.5144600 -.0437900
0.5681400 -.0398700
0.6211600 -.0358700
0.6728800 -.0318600
0.7226600 -.0279100
0.7698800 -.0240700
0.8139600 -.0203900
0.8543400 -.0169100
0.8905000 -.0136400
0.9219800 -.0105900
0.9483400 -.0076400
0.9695200 -.0046400
0.9856700 -.0019700
0.9962400 -.0004100
1.0000000 0.0000000
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Polars for EPPLER 472 AIRFOIL (e472-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e472-il | 50,000 | 9 | 17.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e472-il | 50,000 | 5 | 21.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e472-il | 100,000 | 9 | 26.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e472-il | 100,000 | 5 | 33.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e472-il | 200,000 | 9 | 41.4 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e472-il | 200,000 | 5 | 49.3 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e472-il | 500,000 | 9 | 69.5 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e472-il | 500,000 | 5 | 72.6 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e472-il | 1,000,000 | 9 | 91.7 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e472-il | 1,000,000 | 5 | 90.8 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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