GOE 100 (SOPWITH) AIRFOIL (goe100-il)
GOE 100 (SOPWITH) AIRFOIL - Gottingen 100 (Sopwith) airfoil
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(goe100-il) GOE 100 (SOPWITH) AIRFOIL Gottingen 100 (Sopwith) airfoil Max thickness 6.6% at 20% chord. Max camber 3.6% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 100 (SOPWITH) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124100 0.0114900
0.0248400 0.0211900
0.0497300 0.0360800
0.0746500 0.0459700
0.0996000 0.0523600
0.1495400 0.0600400
0.1995100 0.0644200
0.2994800 0.0679800
0.3994900 0.0676400
0.4995100 0.0642000
0.5995700 0.0585100
0.6996200 0.0495200
0.7997200 0.0364800
0.8998400 0.0210400
0.9499000 0.0126200
1.0000000 0.0020000
0.0000000 0.0000000
0.0125500 -.0061000
0.0250500 -.0086100
0.0500700 -.0092200
0.0750700 -.0090300
0.1000600 -.0082400
0.1500300 -.0045500
0.2000100 -.0012800
0.2999800 0.0022800
0.3999700 0.0042400
0.4999800 0.0021000
0.6000000 -.0005400
0.7000200 -.0025800
0.8000300 -.0035200
0.9000200 -.0027600
0.9500200 -.0023800
1.0000000 -.0020000
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Similar airfoils
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Polars for GOE 100 (SOPWITH) AIRFOIL (goe100-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe100-il | 50,000 | 9 | 37.7 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe100-il | 50,000 | 5 | 38 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe100-il | 100,000 | 9 | 54.4 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe100-il | 100,000 | 5 | 50.9 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe100-il | 200,000 | 9 | 71.3 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe100-il | 200,000 | 5 | 61.7 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe100-il | 500,000 | 9 | 88.2 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe100-il | 500,000 | 5 | 73.1 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe100-il | 1,000,000 | 9 | 88.8 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe100-il | 1,000,000 | 5 | 83.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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