GOE 243 (MVA PR.3) AIRFOIL (goe243-il)
GOE 243 (MVA PR.3) AIRFOIL - Gottingen 243 (MVA PR.3) airfoil
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(goe243-il) GOE 243 (MVA PR.3) AIRFOIL Gottingen 243 (MVA PR.3) airfoil Max thickness 19% at 29.3% chord. Max camber 8.4% at 59.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 243 (MVA PR.3) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0108300 0.0384700
0.0225700 0.0559800
0.0463900 0.0830200
0.0705400 0.1025700
0.0948600 0.1181300
0.1440300 0.1372700
0.1934400 0.1509100
0.2928600 0.1642400
0.3928800 0.1635900
0.4933000 0.1539600
0.5940900 0.1358400
0.6952000 0.1102400
0.7965800 0.0786500
0.8981700 0.0420700
0.9490700 0.0212800
1.0000000 0.0015000
0.0000000 0.0000000
0.0134500 -.0219100
0.0261500 -.0263600
0.0513200 -.0302700
0.0764000 -.0321800
0.1014600 -.0335900
0.1515800 -.0364100
0.2015800 -.0362300
0.3010800 -.0249000
0.4003100 -.0070900
0.4994500 0.0127300
0.5985600 0.0330400
0.6980300 0.0453600
0.7980800 0.0442200
0.8989500 0.0241000
0.9495100 0.0113000
1.0000000 -.0015000
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Polars for GOE 243 (MVA PR.3) AIRFOIL (goe243-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe243-il | 50,000 | 9 | 5.7 at α=-0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 50,000 | 5 | 17.9 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe243-il | 100,000 | 9 | 44.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 100,000 | 5 | 49.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe243-il | 200,000 | 9 | 70.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 200,000 | 5 | 69.4 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe243-il | 500,000 | 9 | 99.1 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 500,000 | 5 | 90.3 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe243-il | 1,000,000 | 9 | 119.1 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 1,000,000 | 5 | 107.9 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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