GOE 404 AIRFOIL (goe404-il)
GOE 404 AIRFOIL - Gottingen 404 airfoil
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(goe404-il) GOE 404 AIRFOIL Gottingen 404 airfoil Max thickness 13.2% at 29.6% chord. Max camber 5% at 29.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 404 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0115300 0.0312600
0.0235700 0.0459300
0.0480200 0.0636900
0.0726000 0.0772600
0.0972900 0.0871300
0.1468800 0.1003700
0.1965900 0.1098100
0.2964000 0.1156200
0.3965600 0.1107300
0.4968700 0.1005500
0.5973500 0.0850800
0.6979200 0.0669100
0.7985300 0.0472300
0.8992500 0.0242700
0.9496100 0.0125300
1.0000000 0.0008000
0.0000000 0.0000000
0.0131500 -.0208900
0.0258000 -.0258000
0.0509300 -.0298200
0.0759200 -.0295400
0.1008600 -.0276600
0.1507500 -.0240100
0.2006300 -.0203600
0.3005000 -.0161500
0.4004100 -.0130500
0.5003400 -.0110400
0.6002800 -.0089300
0.7001800 -.0058200
0.8001300 -.0043200
0.9001100 -.0034100
0.9500700 -.0023500
1.0000000 -.0008000
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Polars for GOE 404 AIRFOIL (goe404-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe404-il | 50,000 | 9 | 15.2 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe404-il | 50,000 | 5 | 31.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe404-il | 100,000 | 9 | 45.2 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe404-il | 100,000 | 5 | 50.8 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe404-il | 200,000 | 9 | 68.8 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe404-il | 200,000 | 5 | 69.7 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe404-il | 500,000 | 9 | 98.8 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe404-il | 500,000 | 5 | 94.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe404-il | 1,000,000 | 9 | 121.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe404-il | 1,000,000 | 5 | 110.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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