GOE 207 (AVIATIK V8) AIRFOIL (goe207-il)
GOE 207 (AVIATIK V8) AIRFOIL - Gottingen 207 (AVIATIK V8) airfoil
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(goe207-il) GOE 207 (AVIATIK V8) AIRFOIL Gottingen 207 (AVIATIK V8) airfoil Max thickness 8.8% at 19.9% chord. Max camber 6.6% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 207 (AVIATIK V8) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122500 0.0222400
0.0246400 0.0329700
0.0494000 0.0543500
0.0742200 0.0702200
0.0991000 0.0812000
0.1489100 0.0986500
0.1988200 0.1071000
0.2987900 0.1098000
0.3988600 0.1030100
0.4990000 0.0902100
0.5991700 0.0751200
0.6993600 0.0578300
0.7995600 0.0397400
0.8997600 0.0215400
0.9498600 0.0129000
1.0000000 0.0037500
0.0000000 0.0000000
0.0126600 -.0146600
0.0251500 -.0134200
0.0500800 -.0071500
0.0750000 0.0000300
0.0999400 0.0053000
0.1498500 0.0137600
0.1997900 0.0194100
0.2997500 0.0228100
0.3997600 0.0216200
0.4997900 0.0187200
0.5998400 0.0145300
0.6998800 0.0106300
0.7999300 0.0060400
0.8999900 0.0009400
0.9500100 -.0011000
1.0000000 -.0037500
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Polars for GOE 207 (AVIATIK V8) AIRFOIL (goe207-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe207-il | 50,000 | 9 | 20.8 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe207-il | 50,000 | 5 | 33.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe207-il | 100,000 | 9 | 47.4 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe207-il | 100,000 | 5 | 52 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe207-il | 200,000 | 9 | 70.4 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe207-il | 200,000 | 5 | 71.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe207-il | 500,000 | 9 | 99.1 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe207-il | 500,000 | 5 | 96.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe207-il | 1,000,000 | 9 | 120.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe207-il | 1,000,000 | 5 | 113.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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