GOE 12K AIRFOIL (goe12k-il)
GOE 12K AIRFOIL - Gottingen 12K airfoil
| Details | Dat file | Parser | |
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(goe12k-il) GOE 12K AIRFOIL Gottingen 12K airfoil Max thickness 11.1% at 50% chord. Max camber 4.1% at 60% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 12K AIRFOIL
15. 15.
0.0000000 0.0000000
0.0250000 0.0287600
0.0500000 0.0402200
0.1000000 0.0554400
0.1500000 0.0667600
0.2000000 0.0755800
0.3000000 0.0876200
0.4000000 0.0930600
0.5000000 0.0960000
0.6000000 0.0944400
0.7000000 0.0846800
0.8000000 0.0670200
0.9000000 0.0395600
0.9500000 0.0239800
1.0000000 0.0000000
0.0000000 0.0000000
0.0250000 -.0192400
0.0500000 -.0226800
0.1000000 -.0239600
0.1500000 -.0228400
0.2000000 -.0217200
0.3000000 -.0194800
0.4000000 -.0172400
0.5000000 -.0150000
0.6000000 -.0127600
0.7000000 -.0105200
0.8000000 -.0082800
0.9000000 -.0060400
0.9500000 -.0049200
1.0000000 0.0000000
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Polars for GOE 12K AIRFOIL (goe12k-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe12k-il | 50,000 | 9 | 28.9 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe12k-il | 50,000 | 5 | 27.3 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe12k-il | 100,000 | 9 | 42.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe12k-il | 100,000 | 5 | 40.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe12k-il | 200,000 | 9 | 66.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe12k-il | 200,000 | 5 | 65.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe12k-il | 500,000 | 9 | 114 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe12k-il | 500,000 | 5 | 104.2 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe12k-il | 1,000,000 | 9 | 146.7 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe12k-il | 1,000,000 | 5 | 84.6 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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