GOE 422 AIRFOIL (goe422-il)
GOE 422 AIRFOIL - Gottingen 422 airfoil
| Details | Dat file | Parser | |
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(goe422-il) GOE 422 AIRFOIL Gottingen 422 airfoil Max thickness 17.1% at 29.5% chord. Max camber 6.5% at 39.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 422 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0113200 0.0345900
0.0232700 0.0505000
0.0475300 0.0722300
0.0720400 0.0863700
0.0965900 0.0995100
0.1458900 0.1200000
0.1953900 0.1344900
0.2949500 0.1475000
0.3949200 0.1483300
0.4952100 0.1399600
0.5957500 0.1241000
0.6965500 0.1008600
0.7975300 0.0722200
0.8986300 0.0398800
0.9493200 0.0197100
1.0000000 0.0010500
0.0000000 0.0000000
0.0132200 -.0209500
0.0258800 -.0258100
0.0510200 -.0298500
0.0760700 -.0310900
0.1010500 -.0307400
0.1510300 -.0301300
0.2009700 -.0284200
0.3007800 -.0229000
0.4006100 -.0178800
0.5004600 -.0133600
0.6003200 -.0094400
0.7002100 -.0060200
0.8000500 -.0015000
0.9001100 -.0009800
0.9500400 -.0011600
1.0000000 -.0010500
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Polars for GOE 422 AIRFOIL (goe422-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe422-il | 50,000 | 9 | 5.8 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe422-il | 50,000 | 5 | 19.4 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe422-il | 100,000 | 9 | 44.9 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe422-il | 100,000 | 5 | 47.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe422-il | 200,000 | 9 | 71 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe422-il | 200,000 | 5 | 66.5 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe422-il | 500,000 | 9 | 97.4 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe422-il | 500,000 | 5 | 85.3 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe422-il | 1,000,000 | 9 | 117.3 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe422-il | 1,000,000 | 5 | 98.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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