GOE 415 AIRFOIL (goe415-il)
GOE 415 AIRFOIL - Gottingen 415 airfoil
| Details | Dat file | Parser | |
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(goe415-il) GOE 415 AIRFOIL Gottingen 415 airfoil Max thickness 8.5% at 19.9% chord. Max camber 3.7% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 415 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123300 0.0167300
0.0247300 0.0270500
0.0495700 0.0423000
0.0744600 0.0527600
0.0993900 0.0600100
0.1492900 0.0706200
0.1992300 0.0760200
0.2992100 0.0781400
0.3992500 0.0737500
0.4993400 0.0651700
0.5994400 0.0553800
0.6995500 0.0439000
0.7996800 0.0311200
0.8998400 0.0156300
0.9499100 0.0084400
1.0000000 0.0005500
0.0000000 0.0000000
0.0125400 -.0047000
0.0250500 -.0056000
0.0500700 -.0071000
0.0750800 -.0084000
0.1000900 -.0091800
0.1500900 -.0091800
0.2000900 -.0086700
0.3000500 -.0049500
0.4000100 -.0012400
0.4999800 0.0018700
0.5999800 0.0023900
0.6999700 0.0028000
0.7999700 0.0028200
0.8999900 0.0005300
0.9500100 -.0005600
1.0000000 -.0005500
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Polars for GOE 415 AIRFOIL (goe415-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe415-il | 50,000 | 9 | 34 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe415-il | 50,000 | 5 | 37.2 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe415-il | 100,000 | 9 | 52 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe415-il | 100,000 | 5 | 53.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe415-il | 200,000 | 9 | 68.9 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe415-il | 200,000 | 5 | 69.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe415-il | 500,000 | 9 | 92.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe415-il | 500,000 | 5 | 90.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe415-il | 1,000,000 | 9 | 109.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe415-il | 1,000,000 | 5 | 106.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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