GOE 195 AIRFOIL (goe195-il)
GOE 195 AIRFOIL - Gottingen 195 airfoil
| Details | Dat file | Parser | |
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(goe195-il) GOE 195 AIRFOIL Gottingen 195 airfoil Max thickness 8.6% at 20% chord. Max camber 5.1% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 195 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0202100
0.0250000 0.0284200
0.0500000 0.0418500
0.0750000 0.0512800
0.1000000 0.0587000
0.1500000 0.0705500
0.2000000 0.0784000
0.3000000 0.0871000
0.4000000 0.0878000
0.5000000 0.0815000
0.6000000 0.0732000
0.7000000 0.0599000
0.8000000 0.0446000
0.9000000 0.0253000
0.9500000 0.0141500
1.0000000 0.0020000
0.0000000 0.0000000
0.0125000 -.0117900
0.0250000 -.0135700
0.0500000 -.0151500
0.0750000 -.0157200
0.1000000 -.0153000
0.1500000 -.0124500
0.2000000 -.0076000
0.3000000 0.0051000
0.4000000 0.0138000
0.5000000 0.0205000
0.6000000 0.0242000
0.7000000 0.0229000
0.8000000 0.0166000
0.9000000 0.0083000
0.9500000 0.0041500
1.0000000 0.0000000
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Polars for GOE 195 AIRFOIL (goe195-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe195-il | 50,000 | 9 | 40.7 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe195-il | 50,000 | 5 | 44 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe195-il | 100,000 | 9 | 63.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe195-il | 100,000 | 5 | 64.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe195-il | 200,000 | 9 | 86 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe195-il | 200,000 | 5 | 84 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe195-il | 500,000 | 9 | 116.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe195-il | 500,000 | 5 | 109.1 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe195-il | 1,000,000 | 9 | 139 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe195-il | 1,000,000 | 5 | 106.1 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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