GOE 278 (DAIMLER IX) AIRFOIL (goe278-il)
GOE 278 (DAIMLER IX) AIRFOIL - Gottingen 278 (DAIMLER IX) airfoil
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(goe278-il) GOE 278 (DAIMLER IX) AIRFOIL Gottingen 278 (DAIMLER IX) airfoil Max thickness 7.4% 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 278 (DAIMLER IX) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123500 0.0203900
0.0248000 0.0277800
0.0497100 0.0395600
0.0746400 0.0495400
0.0995800 0.0575300
0.1495000 0.0682900
0.1994500 0.0754600
0.2994200 0.0797900
0.3994300 0.0785200
0.4994600 0.0734500
0.5995300 0.0647800
0.6996100 0.0541100
0.7997100 0.0392400
0.8998500 0.0211700
0.9499199 0.0116300
1.0000000 0.0010000
0.0000000 0.0000000
0.0125600 -.0082100
0.0250600 -.0076200
0.0500300 -.0048000
0.0750200 -.0020500
0.1000000 0.0002300
0.1499800 0.0026900
0.1999700 0.0035600
0.2999600 0.0053900
0.3999600 0.0061200
0.4999600 0.0061800
0.5999600 0.0059800
0.6999700 0.0046100
0.7999800 0.0027400
0.9000000 0.0003700
0.9500100 -.0004300
1.0000000 -.0010000
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Polars for GOE 278 (DAIMLER IX) AIRFOIL (goe278-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe278-il | 50,000 | 9 | 38.5 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe278-il | 50,000 | 5 | 40.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe278-il | 100,000 | 9 | 55.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe278-il | 100,000 | 5 | 56.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe278-il | 200,000 | 9 | 72.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe278-il | 200,000 | 5 | 72.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe278-il | 500,000 | 9 | 95.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe278-il | 500,000 | 5 | 92.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe278-il | 1,000,000 | 9 | 113.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe278-il | 1,000,000 | 5 | 102.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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