GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOIL (goe316-il)
GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOIL - Gottingen 316 (Hansa-Brandenburg IV.5) airfoil
| Details | Dat file | Parser | |
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(goe316-il) GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOIL Gottingen 316 (Hansa-Brandenburg IV.5) airfoil Max thickness 9.1% at 29.9% chord. Max camber 4.2% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123000 0.0210200
0.0247100 0.0308300
0.0495800 0.0443700
0.0744700 0.0556100
0.0993900 0.0642400
0.1492700 0.0769200
0.1991900 0.0852900
0.2991700 0.0878400
0.3992000 0.0839900
0.4992900 0.0749400
0.5994000 0.0626900
0.6995500 0.0472500
0.7997000 0.0319000
0.8998400 0.0170500
0.9499100 0.0092200
1.0000000 0.0021000
0.0000000 0.0000000
0.0126100 -.0104800
0.0251000 -.0114500
0.0500900 -.0090200
0.0750600 -.0072800
0.1000500 -.0056500
0.1500300 -.0036700
0.2000300 -.0032000
0.3000300 -.0029500
0.4000200 -.0025000
0.5000300 -.0026500
0.6000300 -.0027000
0.7000300 -.0028500
0.8000300 -.0029000
0.9000200 -.0025500
0.9500200 -.0025700
1.0000000 -.0021000
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Polars for GOE 316 (HANSA-BRANDENBURG IV.5) AIRFOIL (goe316-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe316-il | 50,000 | 9 | 23.4 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe316-il | 50,000 | 5 | 34.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe316-il | 100,000 | 9 | 50.9 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe316-il | 100,000 | 5 | 52 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe316-il | 200,000 | 9 | 71.2 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe316-il | 200,000 | 5 | 72 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe316-il | 500,000 | 9 | 100.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe316-il | 500,000 | 5 | 98.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe316-il | 1,000,000 | 9 | 123.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe316-il | 1,000,000 | 5 | 118.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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