GOE 518 AIRFOIL (goe518-il)
GOE 518 AIRFOIL - Gottingen 518 airfoil
| Details | Dat file | Parser | |
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(goe518-il) GOE 518 AIRFOIL Gottingen 518 airfoil Max thickness 18% at 29.8% chord. Max camber 7.3% at 29.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 518 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0120600 0.0436200
0.0243700 0.0632400
0.0491200 0.0884900
0.0739300 0.1067400
0.0988000 0.1204900
0.1485900 0.1414900
0.1984500 0.1549800
0.2983700 0.1629800
0.3984200 0.1584800
0.4985300 0.1469900
0.5987100 0.1294900
0.6989300 0.1074900
0.7992200 0.0784900
0.8995700 0.0430000
0.9497800 0.0220000
1.0000000 0.0000000
0.0000000 0.0000000
0.0126200 -.0123700
0.0251500 -.0152500
0.0501700 -.0175000
0.0751900 -.0187500
0.1001800 -.0185000
0.1501800 -.0180000
0.2001800 -.0180000
0.3001700 -.0170000
0.4001600 -.0160000
0.5001500 -.0150000
0.6001400 -.0140000
0.7001300 -.0130000
0.8001200 -.0120000
0.9000800 -.0075000
0.9500500 -.0045000
1.0000000 0.0000000
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Polars for GOE 518 AIRFOIL (goe518-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe518-il | 50,000 | 9 | 6.5 at α=-3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe518-il | 50,000 | 5 | 23.7 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe518-il | 100,000 | 9 | 41.4 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe518-il | 100,000 | 5 | 39.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe518-il | 200,000 | 9 | 54.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe518-il | 200,000 | 5 | 48.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe518-il | 500,000 | 9 | 64.5 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe518-il | 500,000 | 5 | 61.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe518-il | 1,000,000 | 9 | 81 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe518-il | 1,000,000 | 5 | 79.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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