GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOIL (goe318-il)
GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOIL - Gottingen 318 (Hansa-Brandenburg VI.5) airfoil
| Details | Dat file | Parser | |
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(goe318-il) GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOIL Gottingen 318 (Hansa-Brandenburg VI.5) airfoil Max thickness 9.1% at 29.9% chord. Max camber 4.3% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122900 0.0195300
0.0246900 0.0290600
0.0495400 0.0431300
0.0744200 0.0544900
0.0993300 0.0634500
0.1491800 0.0773800
0.1991100 0.0840100
0.2990600 0.0888700
0.3990900 0.0855300
0.4992000 0.0755900
0.5993600 0.0600500
0.6995500 0.0429200
0.7997200 0.0262800
0.8998700 0.0125400
0.9499300 0.0068700
1.0000000 0.0020000
0.0000000 0.0000000
0.0126300 -.0108700
0.0251300 -.0123300
0.0501200 -.0117700
0.0751200 -.0112000
0.1001100 -.0098900
0.1500800 -.0071100
0.2000500 -.0049800
0.3000300 -.0024200
0.4000200 -.0017600
0.5000200 -.0018000
0.6000200 -.0018400
0.7000300 -.0023800
0.8000300 -.0030200
0.9000300 -.0024600
0.9500300 -.0025300
1.0000000 -.0020000
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Polars for GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOIL (goe318-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe318-il | 50,000 | 9 | 20.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe318-il | 50,000 | 5 | 35.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe318-il | 100,000 | 9 | 50.4 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe318-il | 100,000 | 5 | 53.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe318-il | 200,000 | 9 | 69 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe318-il | 200,000 | 5 | 70 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe318-il | 500,000 | 9 | 93.3 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe318-il | 500,000 | 5 | 92.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe318-il | 1,000,000 | 9 | 113.9 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe318-il | 1,000,000 | 5 | 111 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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