GOE 242 (MVA PR.2) AIRFOIL (goe242-il)
GOE 242 (MVA PR.2) AIRFOIL - Gottingen 242 (MVA PR.2) airfoil
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(goe242-il) GOE 242 (MVA PR.2) AIRFOIL Gottingen 242 (MVA PR.2) airfoil Max thickness 16.2% at 29.6% chord. Max camber 7.5% at 49.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 242 (MVA PR.2) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0117900 0.0278000
0.0239000 0.0431100
0.0483700 0.0637300
0.0729600 0.0800600
0.0975800 0.0949900
0.1470200 0.1167500
0.1966800 0.1300200
0.2963300 0.1440600
0.3962600 0.1466000
0.4965300 0.1359600
0.5970000 0.1177200
0.6975700 0.0952900
0.7983000 0.0668600
0.8991001 0.0354300
0.9495201 0.0190100
1.0000000 0.0020000
0.0000000 0.0000000
0.0127600 -.0101700
0.0253300 -.0128500
0.0504300 -.0167100
0.0755000 -.0195700
0.1005500 -.0214400
0.1506000 -.0236600
0.2005700 -.0223900
0.3004500 -.0175400
0.4001100 -.0043000
0.4996200 0.0147400
0.5992000 0.0314800
0.6989700 0.0403200
0.7990300 0.0378800
0.8994200 0.0229400
0.9497000 0.0117200
1.0000000 -.0020000
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Polars for GOE 242 (MVA PR.2) AIRFOIL (goe242-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe242-il | 50,000 | 9 | 6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe242-il | 50,000 | 5 | 20.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe242-il | 100,000 | 9 | 46.8 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe242-il | 100,000 | 5 | 54.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe242-il | 200,000 | 9 | 78.6 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe242-il | 200,000 | 5 | 80.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe242-il | 500,000 | 9 | 116.8 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe242-il | 500,000 | 5 | 114.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe242-il | 1,000,000 | 9 | 146.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe242-il | 1,000,000 | 5 | 137.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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