GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL (goe315-il)
GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL - Gottingen 315 (Hansa-Brandenburg III.5) airfoil
| Details | Dat file | Parser | |
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(goe315-il) GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL Gottingen 315 (Hansa-Brandenburg III.5) airfoil Max thickness 8.1% at 29.9% chord. Max camber 4.1% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122700 0.0214300
0.0247000 0.0287600
0.0495500 0.0420300
0.0744600 0.0513900
0.0993700 0.0595500
0.1492500 0.0707800
0.1991900 0.0766100
0.2991400 0.0813700
0.3991700 0.0787300
0.4992600 0.0696900
0.5993800 0.0583500
0.6995400 0.0438200
0.7996800 0.0297800
0.8998300 0.0159400
0.9499100 0.0084700
1.0000000 0.0000000
0.0000000 0.0000000
0.0126100 -.0102700
0.0251100 -.0103300
0.0500800 -.0079700
0.0750600 -.0058000
0.1000400 -.0036400
0.1500100 -.0010100
0.1999900 0.0005200
0.2999900 0.0005800
0.4000000 0.0000400
0.5000000 0.0000000
0.6000000 0.0002600
0.6999900 0.0005200
0.8000100 -.0005200
0.9000100 -.0005600
0.9500100 -.0005300
1.0000000 0.0000000
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Polars for GOE 315 (HANSA-BRANDENBURG III.5) AIRFOIL (goe315-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe315-il | 50,000 | 9 | 35.4 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe315-il | 50,000 | 5 | 38 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe315-il | 100,000 | 9 | 54.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe315-il | 100,000 | 5 | 55.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe315-il | 200,000 | 9 | 73.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe315-il | 200,000 | 5 | 69.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe315-il | 500,000 | 9 | 95.1 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe315-il | 500,000 | 5 | 82.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe315-il | 1,000,000 | 9 | 104.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe315-il | 1,000,000 | 5 | 87 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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