GOE 383 AIRFOIL (goe383-il)
GOE 383 AIRFOIL - Gottingen 383 airfoil
| Details | Dat file | Parser | |
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(goe383-il) GOE 383 AIRFOIL Gottingen 383 airfoil Max thickness 20.2% at 28.7% chord. Max camber 5% at 38.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 383 AIRFOIL
17. 17.
0.0000200 0.0000000
0.0091300 0.0381100
0.0204100 0.0518100
0.0436200 0.0719700
0.0672100 0.0878700
0.0909300 0.1022700
0.1390900 0.1230500
0.1879000 0.1363800
0.2866900 0.1499600
0.3868000 0.1487400
0.4877500 0.1380100
0.5895900 0.1172500
0.6918100 0.0923300
0.7943100 0.0641300
0.8970800 0.0328600
0.9485700 0.0161300
1.0000000 0.0016000
0.0000200 0.0000000
0.0148500 -.0257800
0.0278600 -.0320300
0.0534600 -.0388500
0.0789200 -.0439900
0.1042000 -.0471500
0.1544600 -.0505800
0.2046800 -.0525300
0.3046000 -.0516500
0.4043200 -.0486000
0.5038800 -.0435600
0.6032800 -.0368300
0.7024900 -.0280200
0.8017099 -.0192100
0.9009200 -.0104000
0.9505300 -.0059900
1.0000000 -.0016000
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Polars for GOE 383 AIRFOIL (goe383-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe383-il | 50,000 | 9 | 3.6 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe383-il | 50,000 | 5 | 13.9 at α=0.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe383-il | 100,000 | 9 | 25 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe383-il | 100,000 | 5 | 40.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe383-il | 200,000 | 9 | 62.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe383-il | 200,000 | 5 | 60.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe383-il | 500,000 | 9 | 88.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe383-il | 500,000 | 5 | 83.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe383-il | 1,000,000 | 9 | 111.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe383-il | 1,000,000 | 5 | 106.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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