GOE 165 (MVA MK.11) AIRFOIL (goe165-il)
GOE 165 (MVA MK.11) AIRFOIL - Gottingen 165 (MVA MK.11) airfoil
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(goe165-il) GOE 165 (MVA MK.11) AIRFOIL Gottingen 165 (MVA MK.11) airfoil Max thickness 12.1% at 19.7% chord. Max camber 5.7% at 49.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 165 (MVA MK.11) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0119500 0.0194400
0.0240800 0.0324800
0.0486500 0.0476800
0.0732100 0.0628800
0.0979300 0.0728800
0.1475000 0.0881900
0.1972300 0.0977000
0.2970800 0.1029400
0.3971300 0.1010800
0.4973000 0.0952200
0.5976600 0.0824700
0.6980700 0.0678300
0.7985300 0.0516800
0.8991100 0.0313300
0.9494600 0.0188600
1.0000000 0.0006000
0.0000000 0.0000000
0.0126900 -.0066400
0.0253100 -.0108800
0.0504200 -.0148700
0.0755500 -.0193500
0.1006000 -.0209400
0.1506900 -.0241200
0.2006600 -.0233000
0.3004200 -.0146700
0.3999100 0.0032600
0.4994300 0.0199800
0.5992200 0.0274200
0.6992400 0.0267600
0.7993900 0.0215000
0.8996400 0.0127500
0.9498300 0.0060800
1.0000000 -.0006000
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Polars for GOE 165 (MVA MK.11) AIRFOIL (goe165-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe165-il | 50,000 | 9 | 31.3 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe165-il | 50,000 | 5 | 39.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe165-il | 100,000 | 9 | 54.4 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe165-il | 100,000 | 5 | 53.4 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe165-il | 200,000 | 9 | 69.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe165-il | 200,000 | 5 | 66.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe165-il | 500,000 | 9 | 85.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe165-il | 500,000 | 5 | 79.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe165-il | 1,000,000 | 9 | 96.6 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe165-il | 1,000,000 | 5 | 85.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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