GOE 535 AIRFOIL (goe535-il)
GOE 535 AIRFOIL - Gottingen 535 airfoil
| Details | Dat file | Parser | |
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(goe535-il) GOE 535 AIRFOIL Gottingen 535 airfoil Max thickness 16.1% at 20% chord. Max camber 5.8% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 535 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0410200
0.0250000 0.0555400
0.0500000 0.0745700
0.0750000 0.0891100
0.1000000 0.1006500
0.1500000 0.1162300
0.2000000 0.1258000
0.3000000 0.1324500
0.4000000 0.1271000
0.5000000 0.1152500
0.6000000 0.0984000
0.7000000 0.0782500
0.8000000 0.0557000
0.9000000 0.0298500
0.9500000 0.0154300
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0194800
0.0250000 -.0264600
0.0500000 -.0329300
0.0750000 -.0348900
0.1000000 -.0358500
0.1500000 -.0362800
0.2000000 -.0347000
0.3000000 -.0280500
0.4000000 -.0149000
0.5000000 -.0002500
0.6000000 0.0119000
0.7000000 0.0160500
0.8000000 0.0152000
0.9000000 0.0088500
0.9500000 0.0029200
1.0000000 0.0000000
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Polars for GOE 535 AIRFOIL (goe535-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe535-il | 50,000 | 9 | 7.2 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe535-il | 50,000 | 5 | 29.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe535-il | 100,000 | 9 | 43.1 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe535-il | 100,000 | 5 | 50.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe535-il | 200,000 | 9 | 68.1 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe535-il | 200,000 | 5 | 68.5 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe535-il | 500,000 | 9 | 96.6 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe535-il | 500,000 | 5 | 90.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe535-il | 1,000,000 | 9 | 116.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe535-il | 1,000,000 | 5 | 110.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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