GOE 530 AIRFOIL (goe530-il)
GOE 530 AIRFOIL - Gottingen 530 airfoil
| Details | Dat file | Parser | |
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(goe530-il) GOE 530 AIRFOIL Gottingen 530 airfoil Max thickness 12.9% at 29.8% chord. Max camber 5.1% at 29.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 530 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0120000 0.0341700
0.0243300 0.0463500
0.0490900 0.0627100
0.0739100 0.0750700
0.0987500 0.0859300
0.1485400 0.1006500
0.1984200 0.1088800
0.2983300 0.1153300
0.3983700 0.1122800
0.4985000 0.1037300
0.5987100 0.0891800
0.6989800 0.0701400
0.7993000 0.0480900
0.8996601 0.0235500
0.9498300 0.0117700
1.0000000 0.0000000
0.0000000 0.0000000
0.0127400 -.0163200
0.0253100 -.0216300
0.0503500 -.0242700
0.0753400 -.0234100
0.1003300 -.0225500
0.1502900 -.0203200
0.2002600 -.0176000
0.3002000 -.0136500
0.4001700 -.0117000
0.5001500 -.0102500
0.6001600 -.0113000
0.7001800 -.0123500
0.8001900 -.0134000
0.9001500 -.0104500
0.9500901 -.0062200
1.0000000 0.0000000
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Polars for GOE 530 AIRFOIL (goe530-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe530-il | 50,000 | 9 | 14 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe530-il | 50,000 | 5 | 32.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe530-il | 100,000 | 9 | 49.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe530-il | 100,000 | 5 | 50.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe530-il | 200,000 | 9 | 69 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe530-il | 200,000 | 5 | 66.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe530-il | 500,000 | 9 | 94.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe530-il | 500,000 | 5 | 89.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe530-il | 1,000,000 | 9 | 115.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe530-il | 1,000,000 | 5 | 101.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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