GOE 571 AIRFOIL (goe571-il)
GOE 571 AIRFOIL - Gottingen 571 airfoil
| Details | Dat file | Parser | |
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(goe571-il) GOE 571 AIRFOIL Gottingen 571 airfoil Max thickness 24.9% at 29.4% chord. Max camber 9.8% at 29.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 571 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0113900 0.0403100
0.0232100 0.0651400
0.0471900 0.1023000
0.0714000 0.1309600
0.0957600 0.1541300
0.1448900 0.1859800
0.1943400 0.2058400
0.2938700 0.2230800
0.3940400 0.2168400
0.4945900 0.1966000
0.5954400 0.1658700
0.6964100 0.1306500
0.7974401 0.0929300
0.8985600 0.0522100
0.9491900 0.0296000
1.0000000 0.0000000
0.0000000 0.0000000
0.0131200 -.0226400
0.0257000 -.0252900
0.0507700 -.0281000
0.0758000 -.0289200
0.1007900 -.0287300
0.1507900 -.0288500
0.2007800 -.0284800
0.3007200 -.0262300
0.4006600 -.0239800
0.5005800 -.0212300
0.6005100 -.0184900
0.7004300 -.0157400
0.8003399 -.0124900
0.9002500 -.0092400
0.9502000 -.0073700
1.0000000 0.0000000
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Polars for GOE 571 AIRFOIL (goe571-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe571-il | 50,000 | 9 | 3.7 at α=-12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 50,000 | 5 | 5.7 at α=-7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe571-il | 100,000 | 9 | 8.1 at α=-8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 100,000 | 5 | 8.6 at α=0.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe571-il | 200,000 | 9 | 33.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 200,000 | 5 | 34 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe571-il | 500,000 | 9 | 56.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 500,000 | 5 | 42.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe571-il | 1,000,000 | 9 | 62.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 1,000,000 | 5 | 52.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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