GOE 336 (MVA H.44) AIRFOIL (goe336-il)
GOE 336 (MVA H.44) AIRFOIL - Gottingen 336 (MVA H.44) airfoil
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(goe336-il) GOE 336 (MVA H.44) AIRFOIL Gottingen 336 (MVA H.44) airfoil Max thickness 9% at 29.9% chord. Max camber 5.4% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 336 (MVA H.44) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123800 0.0195700
0.0247900 0.0326500
0.0497200 0.0473000
0.0746500 0.0589500
0.0996000 0.0673000
0.1495200 0.0802000
0.1994700 0.0887000
0.2994100 0.0988000
0.3994200 0.0967000
0.4994800 0.0875000
0.5995500 0.0743000
0.6996601 0.0578000
0.7997500 0.0413000
0.8998600 0.0226000
0.9499300 0.0125000
1.0000000 0.0015000
0.0000000 0.0000000
0.0125700 -.0110200
0.0250700 -.0123500
0.0500700 -.0122000
0.0750600 -.0097500
0.1000400 -.0064000
0.1500000 -.0008000
0.1999800 0.0037000
0.2999400 0.0093000
0.3999400 0.0094000
0.4999600 0.0059000
0.5999900 0.0011000
0.7000200 -.0033000
0.8000400 -.0072000
0.9000400 -.0071000
0.9500300 -.0058000
1.0000000 -.0015000
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Polars for GOE 336 (MVA H.44) AIRFOIL (goe336-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe336-il | 50,000 | 9 | 30.6 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe336-il | 50,000 | 5 | 34.2 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe336-il | 100,000 | 9 | 56.7 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe336-il | 100,000 | 5 | 57.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe336-il | 200,000 | 9 | 79.5 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe336-il | 200,000 | 5 | 77.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe336-il | 500,000 | 9 | 107.1 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe336-il | 500,000 | 5 | 97.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe336-il | 1,000,000 | 9 | 125.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe336-il | 1,000,000 | 5 | 94.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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