EPPLER 473 AIRFOIL (e473-il)
EPPLER 473 AIRFOIL - Eppler E473 aerobatic aircraft airfoil
| Details | Dat file | Parser | |
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(e473-il) EPPLER 473 AIRFOIL Eppler E473 aerobatic aircraft airfoil Max thickness 16.2% at 21.2% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 473 AIRFOIL
31. 31.
0.0000000 0.0000000
0.0028200 0.0103400
0.0106600 0.0215800
0.0227500 0.0329400
0.0388600 0.0439300
0.0588200 0.0541300
0.0824900 0.0631400
0.1097500 0.0706400
0.1405000 0.0762800
0.1746700 0.0798000
0.2123900 0.0809500
0.2539300 0.0799400
0.2991100 0.0774200
0.3473000 0.0738200
0.3978600 0.0694000
0.4501500 0.0643800
0.5034800 0.0589400
0.5571700 0.0532400
0.6105100 0.0474400
0.6628200 0.0416600
0.7134200 0.0360100
0.7616500 0.0305900
0.8068500 0.0254800
0.8484300 0.0207300
0.8858100 0.0163800
0.9184700 0.0124400
0.9459100 0.0088000
0.9680100 0.0052600
0.9849300 0.0022100
0.9960400 0.0004700
1.0000000 0.0000000
0.0000000 0.0000000
0.0028200 -.0103400
0.0106600 -.0215800
0.0227500 -.0329400
0.0388600 -.0439300
0.0588200 -.0541300
0.0824900 -.0631400
0.1097500 -.0706400
0.1405000 -.0762800
0.1746700 -.0798000
0.2123900 -.0809500
0.2539300 -.0799400
0.2991100 -.0774200
0.3473000 -.0738200
0.3978600 -.0694000
0.4501500 -.0643800
0.5034800 -.0589400
0.5571700 -.0532400
0.6105100 -.0474400
0.6628200 -.0416600
0.7134200 -.0360100
0.7616500 -.0305900
0.8068500 -.0254800
0.8484300 -.0207300
0.8858100 -.0163800
0.9184700 -.0124400
0.9459100 -.0088000
0.9680100 -.0052600
0.9849300 -.0022100
0.9960400 -.0004700
1.0000000 0.0000000
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Polars for EPPLER 473 AIRFOIL (e473-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e473-il | 50,000 | 9 | 15.8 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e473-il | 50,000 | 5 | 21.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e473-il | 100,000 | 9 | 26.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e473-il | 100,000 | 5 | 35.9 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e473-il | 200,000 | 9 | 47.9 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e473-il | 200,000 | 5 | 53.8 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e473-il | 500,000 | 9 | 78.2 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e473-il | 500,000 | 5 | 78.7 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e473-il | 1,000,000 | 9 | 101.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e473-il | 1,000,000 | 5 | 95.7 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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