GOE 309 (MVA H.41) AIRFOIL (goe309-il)
GOE 309 (MVA H.41) AIRFOIL - Gottingen 309 (MVA H.41) airfoil
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(goe309-il) GOE 309 (MVA H.41) AIRFOIL Gottingen 309 (MVA H.41) airfoil Max thickness 8.4% at 30% chord. Max camber 4.7% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 309 (MVA H.41) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125100 0.0158900
0.0250200 0.0264800
0.0500300 0.0430600
0.0750400 0.0543500
0.1000400 0.0633300
0.1500500 0.0747900
0.2000600 0.0820600
0.3000600 0.0888900
0.4000600 0.0866200
0.5000600 0.0791500
0.6000500 0.0674800
0.7000400 0.0525100
0.8000300 0.0365400
0.9000100 0.0195700
0.9500100 0.0102400
1.0000000 0.0020000
0.0000000 0.0000000
0.0124900 -.0085100
0.0249900 -.0101200
0.0499900 -.0103300
0.0749900 -.0090500
0.1000000 -.0064700
0.1500000 -.0027000
0.2000000 0.0000600
0.3000000 0.0045900
0.4000000 0.0026200
0.5000000 -.0017500
0.6000000 -.0068200
0.6999900 -.0101900
0.7999900 -.0106600
0.8999900 -.0075300
0.9500000 -.0048600
1.0000000 -.0020000
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Polars for GOE 309 (MVA H.41) AIRFOIL (goe309-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe309-il | 50,000 | 9 | 34.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe309-il | 50,000 | 5 | 37.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe309-il | 100,000 | 9 | 54.7 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe309-il | 100,000 | 5 | 55.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe309-il | 200,000 | 9 | 73.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe309-il | 200,000 | 5 | 71.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe309-il | 500,000 | 9 | 97 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe309-il | 500,000 | 5 | 90.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe309-il | 1,000,000 | 9 | 113.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe309-il | 1,000,000 | 5 | 101.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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