GOE 388 AIRFOIL (goe388-il)
GOE 388 AIRFOIL - Gottingen 388 airfoil
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(goe388-il) GOE 388 AIRFOIL Gottingen 388 airfoil Max thickness 10.2% at 29.9% chord. Max camber 5.4% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 388 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0121800 0.0226700
0.0245500 0.0325400
0.0493300 0.0278900
0.0741600 0.0600300
0.0990200 0.0699800
0.1488200 0.0846800
0.1986800 0.0949700
0.2985700 0.1028700
0.3985600 0.1031600
0.4986600 0.0959600
0.5988200 0.0844500
0.6990700 0.0665500
0.7993400 0.0470500
0.8996601 0.0243500
0.9498200 0.0132500
1.0000000 0.0010500
0.0000000 0.0000000
0.0126800 -.0127200
0.0252000 -.0146500
0.0502000 -.0143000
0.0751900 -.0134500
0.1001700 -.0125000
0.1501200 -.0086100
0.2000700 -.0052100
0.2999900 0.0009800
0.3999200 0.0055800
0.4998900 0.0080700
0.5998800 0.0083700
0.6999000 0.0072600
0.7999200 0.0058600
0.8999600 0.0029500
0.9499800 0.0012500
1.0000000 -.0010500
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Polars for GOE 388 AIRFOIL (goe388-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe388-il | 50,000 | 9 | 41.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe388-il | 50,000 | 5 | 36.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe388-il | 100,000 | 9 | 55.8 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe388-il | 100,000 | 5 | 37.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe388-il | 200,000 | 9 | 34.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe388-il | 200,000 | 5 | 36.2 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe388-il | 500,000 | 9 | 40.2 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe388-il | 500,000 | 5 | 41.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe388-il | 1,000,000 | 9 | 53.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe388-il | 1,000,000 | 5 | 67.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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