GOE 198 (L.F.G. 5294) AIRFOIL (goe198-il)
GOE 198 (L.F.G. 5294) AIRFOIL - Gottingen 198 (L.F.G. 5294) airfoil
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(goe198-il) GOE 198 (L.F.G. 5294) AIRFOIL Gottingen 198 (L.F.G. 5294) airfoil Max thickness 7.8% at 19.9% chord. Max camber 6.5% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 198 (L.F.G. 5294) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122900 0.0223200
0.0246900 0.0329300
0.0495700 0.0458700
0.0744500 0.0582000
0.0993600 0.0682400
0.1492200 0.0827100
0.1991200 0.0926800
0.2990500 0.1010300
0.3990300 0.1028700
0.4990800 0.0970200
0.5991700 0.0874600
0.6993100 0.0726100
0.7995099 0.0518600
0.8997400 0.0275000
0.9498500 0.0163800
1.0000000 0.0042500
0.0000000 0.0000000
0.0126300 -.0135800
0.0251300 -.0134600
0.0500900 -.0095300
0.0750300 -.0034900
0.0999900 0.0012400
0.1499200 0.0088200
0.1998600 0.0150900
0.2997700 0.0245300
0.3997400 0.0275800
0.4997400 0.0274200
0.5997800 0.0236700
0.6998300 0.0179100
0.7999000 0.0107600
0.8999600 0.0038000
0.9500000 0.0002800
1.0000000 -.0042500
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Polars for GOE 198 (L.F.G. 5294) AIRFOIL (goe198-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe198-il | 50,000 | 9 | 36.2 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe198-il | 50,000 | 5 | 43.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe198-il | 100,000 | 9 | 64.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe198-il | 100,000 | 5 | 64 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe198-il | 200,000 | 9 | 88.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe198-il | 200,000 | 5 | 80.4 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe198-il | 500,000 | 9 | 112.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe198-il | 500,000 | 5 | 92.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe198-il | 1,000,000 | 9 | 117 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe198-il | 1,000,000 | 5 | 92.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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