GOE 777 AIRFOIL (goe777-il)
GOE 777 AIRFOIL - Gottingen 777 airfoil
| Details | Dat file | Parser | |
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(goe777-il) GOE 777 AIRFOIL Gottingen 777 airfoil Max thickness 22% at 30% chord. Max camber 5.9% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 777 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0527200
0.0250000 0.0673300
0.0500000 0.0907600
0.0750000 0.1089000
0.1000000 0.1238300
0.1500000 0.1459900
0.2000000 0.1604600
0.3000000 0.1695900
0.4000000 0.1636200
0.5000000 0.1423500
0.6000000 0.1160800
0.7000000 0.0876100
0.8000000 0.0593400
0.9000000 0.0309700
0.9500000 0.0167300
1.0000000 0.0026000
0.0000000 0.0000000
0.0125000 -.0141800
0.0250000 -.0212700
0.0500000 -.0301300
0.0750000 -.0349000
0.1000000 -.0386700
0.1500000 -.0446000
0.2000000 -.0483400
0.3000000 -.0504100
0.4000000 -.0486800
0.5000000 -.0445500
0.6000000 -.0362200
0.7000000 -.0268900
0.8000000 -.0179600
0.9000000 -.0091300
0.9500000 -.0050700
1.0000000 0.0000000
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Polars for GOE 777 AIRFOIL (goe777-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe777-il | 50,000 | 9 | 3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe777-il | 50,000 | 5 | 8.1 at α=0.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe777-il | 100,000 | 9 | 15.5 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe777-il | 100,000 | 5 | 32.1 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe777-il | 200,000 | 9 | 54.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe777-il | 200,000 | 5 | 57.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe777-il | 500,000 | 9 | 90.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe777-il | 500,000 | 5 | 81.7 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe777-il | 1,000,000 | 9 | 109 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe777-il | 1,000,000 | 5 | 101.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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