GOE 323 (HANSA-BRANDENBURG V.1) AIRFOIL (goe323-il)
GOE 323 (HANSA-BRANDENBURG V.1) AIRFOIL - Gottingen 323 (Hansa-Brandenburg V.1) airfoil
| Details | Dat file | Parser | |
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(goe323-il) GOE 323 (HANSA-BRANDENBURG V.1) AIRFOIL Gottingen 323 (Hansa-Brandenburg V.1) airfoil Max thickness 11.1% at 29.8% chord. Max camber 5.2% at 29.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 323 (HANSA-BRANDENBURG V.1) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0120800 0.0256000
0.0243700 0.0385000
0.0509900 0.0584600
0.0738600 0.0698100
0.0986900 0.0799100
0.1484700 0.0934300
0.1983400 0.1013400
0.2982500 0.1069800
0.3983100 0.1034100
0.4985300 0.0896500
0.5988500 0.0700900
0.6991900 0.0495300
0.7994700 0.0321700
0.8997500 0.0153100
0.9498700 0.0081300
1.0000000 0.0005500
0.0000000 0.0000000
0.0127400 -.0145900
0.0252700 -.0164900
0.0502400 -.0149800
0.0752200 -.0135700
0.1002000 -.0120600
0.1501500 -.0091500
0.2001000 -.0062300
0.3000600 -.0034900
0.4000500 -.0029600
0.5000600 -.0034200
0.6000600 -.0033900
0.7000500 -.0033500
0.8000400 -.0027200
0.9000300 -.0016800
0.9500200 -.0013700
1.0000000 -.0005500
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Polars for GOE 323 (HANSA-BRANDENBURG V.1) AIRFOIL (goe323-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe323-il | 50,000 | 9 | 11.9 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe323-il | 50,000 | 5 | 29.3 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe323-il | 100,000 | 9 | 48.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe323-il | 100,000 | 5 | 54.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe323-il | 200,000 | 9 | 75.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe323-il | 200,000 | 5 | 74.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe323-il | 500,000 | 9 | 106.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe323-il | 500,000 | 5 | 96.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe323-il | 1,000,000 | 9 | 125.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe323-il | 1,000,000 | 5 | 114.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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