EPPLER 636 AIRFOIL (e636-il)
EPPLER 636 AIRFOIL - Eppler E636 airfoil
| Details | Dat file | Parser | |
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(e636-il) EPPLER 636 AIRFOIL Eppler E636 airfoil Max thickness 11.9% at 26.9% chord. Max camber 3.2% at 22.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 636 AIRFOIL
32. 30.
0.0000100 -.0004700
0.0023200 0.0078300
0.0087200 0.0175300
0.0190800 0.0279100
0.0333500 0.0384800
0.0514200 0.0488900
0.0731500 0.0588200
0.0983500 0.0679500
0.1267600 0.0760300
0.1581200 0.0826600
0.1922900 0.0874600
0.2292600 0.0901800
0.2689600 0.0907100
0.3114200 0.0890500
0.3565400 0.0855100
0.4039700 0.0804300
0.4533000 0.0740900
0.5040400 0.0668400
0.5556400 0.0589900
0.6074900 0.0508900
0.6589300 0.0428600
0.7092299 0.0351500
0.7576600 0.0280900
0.8034500 0.0217900
0.8458500 0.0163800
0.8841500 0.0118900
0.9176900 0.0083000
0.9458700 0.0054100
0.9684500 0.0029500
0.9854100 0.0010800
0.9962400 0.0001800
1.0000000 0.0000000
0.0000100 -.0004700
0.0030000 -.0063400
0.0123500 -.0104400
0.0278000 -.0139100
0.0490100 -.0167600
0.0757300 -.0190900
0.1076900 -.0210700
0.1444200 -.0229500
0.1852800 -.0248200
0.2296200 -.0266700
0.2768100 -.0284000
0.3262700 -.0299000
0.3774600 -.0310700
0.4298000 -.0318800
0.4827400 -.0322900
0.5356700 -.0322900
0.5880200 -.0318400
0.6392100 -.0309300
0.6886700 -.0295300
0.7359200 -.0276000
0.7805200 -.0251400
0.8220800 -.0222300
0.8601900 -.0189800
0.8944500 -.0155300
0.9245099 -.0120200
0.9499000 -.0085900
0.9704400 -.0052100
0.9861200 -.0022700
0.9963700 -.0005100
1.0000000 0.0000000
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Polars for EPPLER 636 AIRFOIL (e636-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e636-il | 50,000 | 9 | 14.7 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e636-il | 50,000 | 5 | 24.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e636-il | 100,000 | 9 | 33 at α=13° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e636-il | 100,000 | 5 | 44 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e636-il | 200,000 | 9 | 61.7 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e636-il | 200,000 | 5 | 65.8 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e636-il | 500,000 | 9 | 95.6 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e636-il | 500,000 | 5 | 94.8 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e636-il | 1,000,000 | 9 | 120.7 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e636-il | 1,000,000 | 5 | 108.3 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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