GOE 798 AIRFOIL (goe798-il)
GOE 798 AIRFOIL - Gottingen 798 airfoil
| Details | Dat file | Parser | |
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(goe798-il) GOE 798 AIRFOIL Gottingen 798 airfoil Max thickness 20% at 30% chord. Max camber 6% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 798 AIRFOIL
16. 16.
0.0000000 0.0000000
0.0125000 0.0345200
0.0250000 0.0514400
0.0500000 0.0753700
0.0750000 0.0931100
0.1000000 0.1069500
0.1500000 0.1274300
0.2000000 0.1427000
0.3000000 0.1572500
0.4000000 0.1605000
0.5000000 0.1537500
0.6000000 0.1365000
0.7000000 0.1114500
0.8000000 0.0822000
0.9000000 0.0467500
1.0000000 0.0075000
0.0000000 0.0000000
0.0125000 -.0267800
0.0250000 -.0360600
0.0500000 -.0451200
0.0750000 -.0496900
0.1000000 -.0504500
0.1500000 -.0503700
0.2000000 -.0485000
0.3000000 -.0427500
0.4000000 -.0370000
0.5000000 -.0312500
0.6000000 -.0255000
0.7000000 -.0197500
0.8000000 -.0140000
0.9000000 -.0082500
1.0000000 0.0000000
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Polars for GOE 798 AIRFOIL (goe798-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe798-il | 50,000 | 9 | 3.8 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe798-il | 50,000 | 5 | 10.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe798-il | 100,000 | 9 | 20.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe798-il | 100,000 | 5 | 31.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe798-il | 200,000 | 9 | 65.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe798-il | 200,000 | 5 | 61.7 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe798-il | 500,000 | 9 | 98.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe798-il | 500,000 | 5 | 83.8 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe798-il | 1,000,000 | 9 | 120 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe798-il | 1,000,000 | 5 | 84.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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