GOE 796 AIRFOIL (goe796-il)
GOE 796 AIRFOIL - Gottingen 796 airfoil
| Details | Dat file | Parser | |
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(goe796-il) GOE 796 AIRFOIL Gottingen 796 airfoil Max thickness 12% at 30% chord. Max camber 3.6% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 796 AIRFOIL
21. 21.
0.0000000 0.0000000
0.0020000 0.0075700
0.0040000 0.0109400
0.0060000 0.0135000
0.0080000 0.0160700
0.0125000 0.0206300
0.0250000 0.0308500
0.0500000 0.0452000
0.0750000 0.0557500
0.1000000 0.0642000
0.1500000 0.0763000
0.2000000 0.0856000
0.3000000 0.0942000
0.4000000 0.0961000
0.5000000 0.0920000
0.6000000 0.0816000
0.7000000 0.0666000
0.8000000 0.0490000
0.9000000 0.0276000
0.9500000 0.0158000
1.0000000 0.0040000
0.0000000 0.0000000
0.0020000 -.0059300
0.0040000 -.0093600
0.0060000 -.0118000
0.0080000 -.0135300
0.0125000 -.0160700
0.0250000 -.0216500
0.0500000 -.0271000
0.0750000 -.0298500
0.1000000 -.0304000
0.1500000 -.0303000
0.2000000 -.0292000
0.3000000 -.0258000
0.4000000 -.0224000
0.5000000 -.0190000
0.6000000 -.0156000
0.7000000 -.0122000
0.8000000 -.0088000
0.9000000 -.0054000
0.9500000 -.0029000
1.0000000 0.0000000
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Polars for GOE 796 AIRFOIL (goe796-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe796-il | 50,000 | 9 | 32.2 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe796-il | 50,000 | 5 | 35.5 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe796-il | 100,000 | 9 | 55.5 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe796-il | 100,000 | 5 | 55.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe796-il | 200,000 | 9 | 78 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe796-il | 200,000 | 5 | 73.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe796-il | 500,000 | 9 | 105.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe796-il | 500,000 | 5 | 90.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe796-il | 1,000,000 | 9 | 122.7 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe796-il | 1,000,000 | 5 | 105.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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