GOE 298 AIRFOIL (goe298-il)
GOE 298 AIRFOIL - Gottingen 298 airfoil
| Details | Dat file | Parser | |
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(goe298-il) GOE 298 AIRFOIL Gottingen 298 airfoil Max thickness 12.8% at 19.6% chord. Max camber 4.5% at 39.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 298 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0113300 0.0282700
0.0233400 0.0399700
0.0475900 0.0581700
0.0720800 0.0703900
0.0967700 0.0789100
0.1462200 0.0912600
0.1959500 0.0988200
0.2956900 0.1039600
0.3956900 0.1040000
0.4960800 0.0944600
0.5966500 0.0809300
0.6973300 0.0626500
0.7982100 0.0430900
0.8990900 0.0218700
0.9494700 0.0127600
1.0000000 0.0029500
0.0000000 0.0000000
0.0135800 -.0260400
0.0264000 -.0338100
0.0516700 -.0402600
0.0767100 -.0412200
0.1016200 -.0389900
0.1514100 -.0340200
0.2012000 -.0289600
0.3008300 -.0201300
0.4005400 -.0130000
0.5004100 -.0094700
0.6002900 -.0070200
0.7002400 -.0055300
0.8001700 -.0041300
0.9001000 -.0023900
0.9500800 -.0020200
1.0000000 -.0029500
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Polars for GOE 298 AIRFOIL (goe298-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe298-il | 50,000 | 9 | 27.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe298-il | 50,000 | 5 | 35.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe298-il | 100,000 | 9 | 52.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe298-il | 100,000 | 5 | 52.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe298-il | 200,000 | 9 | 71.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe298-il | 200,000 | 5 | 65.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe298-il | 500,000 | 9 | 91.7 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe298-il | 500,000 | 5 | 88.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe298-il | 1,000,000 | 9 | 112.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe298-il | 1,000,000 | 5 | 103.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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