GOE 164 (MVA MK.10) AIRFOIL (goe164-il)
GOE 164 (MVA MK.10) AIRFOIL - Gottingen 164 (MVA MK.10) airfoil
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(goe164-il) GOE 164 (MVA MK.10) AIRFOIL Gottingen 164 (MVA MK.10) airfoil Max thickness 8.9% at 19.9% chord. Max camber 6.6% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 164 (MVA MK.10) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122700 0.0222300
0.0246500 0.0333600
0.0494700 0.0502200
0.0743500 0.0615800
0.0992300 0.0729500
0.1490900 0.0861700
0.1989900 0.0955000
0.2989200 0.1020500
0.3989300 0.1015100
0.4990000 0.0947600
0.5991200 0.0837200
0.6992800 0.0686800
0.7994600 0.0515300
0.8996700 0.0315900
0.9498100 0.0177200
1.0000000 0.0005500
0.0000000 0.0000000
0.0125700 -.0065700
0.0250900 -.0086400
0.0501100 -.0099700
0.0751100 -.0103100
0.1000900 -.0089400
0.1500200 -.0020200
0.1999300 0.0070100
0.2999700 0.0211700
0.3996700 0.0313200
0.4996400 0.0339700
0.5996500 0.0336300
0.6997000 0.0288800
0.7997900 0.0194400
0.8999000 0.0094900
0.9499500 0.0050200
1.0000000 -.0005500
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Polars for GOE 164 (MVA MK.10) AIRFOIL (goe164-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe164-il | 50,000 | 9 | 34.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe164-il | 50,000 | 5 | 43.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe164-il | 100,000 | 9 | 60.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe164-il | 100,000 | 5 | 62.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe164-il | 200,000 | 9 | 81.4 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe164-il | 200,000 | 5 | 77.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe164-il | 500,000 | 9 | 104.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe164-il | 500,000 | 5 | 92 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe164-il | 1,000,000 | 9 | 112.5 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe164-il | 1,000,000 | 5 | 102.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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