GOE 482 AIRFOIL (goe482-il)
GOE 482 AIRFOIL - Gottingen 482 airfoil
| Details | Dat file | Parser | |
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(goe482-il) GOE 482 AIRFOIL Gottingen 482 airfoil Max thickness 16.5% at 29.6% chord. Max camber 8.8% at 39.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 482 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0117300 0.0307900
0.0238200 0.0471000
0.0481700 0.0732000
0.0726500 0.0938200
0.0972500 0.1099300
0.1466700 0.1331700
0.1962600 0.1494100
0.2958900 0.1644000
0.3959200 0.1634000
0.4957000 0.1506100
0.5967400 0.1304200
0.6974300 0.1029400
0.7982500 0.0699600
0.8990900 0.0364800
0.9495400 0.0182400
1.0000000 0.0000000
0.0000000 0.0000000
0.0128800 -.0151800
0.0255300 -.0213600
0.0505900 -.0237400
0.0755800 -.0231100
0.1005500 -.0219900
0.1504300 -.0172400
0.2003000 -.0119900
0.3000100 -.0005000
0.3996800 0.0129900
0.4994500 0.0219900
0.5992800 0.0289800
0.6992300 0.0309800
0.7993000 0.0279800
0.8995500 0.0179900
0.9497600 0.0097400
1.0000000 0.0000000
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Polars for GOE 482 AIRFOIL (goe482-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe482-il | 50,000 | 9 | 4.9 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe482-il | 50,000 | 5 | 17.3 at α=1.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe482-il | 100,000 | 9 | 35.8 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe482-il | 100,000 | 5 | 51 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe482-il | 200,000 | 9 | 71.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe482-il | 200,000 | 5 | 73.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe482-il | 500,000 | 9 | 107.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe482-il | 500,000 | 5 | 100.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe482-il | 1,000,000 | 9 | 137.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe482-il | 1,000,000 | 5 | 121.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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