GOE 363 AIRFOIL (goe363-il)
GOE 363 AIRFOIL - Gottingen 363 airfoil
| Details | Dat file | Parser | |
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(goe363-il) GOE 363 AIRFOIL Gottingen 363 airfoil Max thickness 11.1% at 19.8% chord. Max camber 5.7% at 39.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 363 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0121200 0.0242900
0.0243900 0.0389800
0.0490700 0.0597600
0.0738300 0.0752500
0.0986800 0.0847300
0.1484700 0.0984100
0.1983700 0.1050800
0.2982900 0.1098400
0.3983200 0.1081900
0.4984400 0.1000500
0.5986200 0.0887100
0.6988800 0.0720700
0.7992200 0.0503300
0.8995800 0.0268900
0.9497899 0.0136700
1.0000000 0.0005500
0.0000000 0.0000000
0.0126500 -.0095000
0.0251900 -.0119100
0.0502200 -.0142200
0.0752300 -.0149300
0.1002200 -.0140400
0.1501500 -.0094700
0.2000900 -.0054900
0.2999700 0.0019600
0.3999000 0.0062200
0.4998800 0.0077700
0.5998900 0.0072300
0.6999000 0.0065800
0.7999099 0.0058400
0.8999500 0.0032900
0.9499800 0.0013700
1.0000000 -.0005500
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Polars for GOE 363 AIRFOIL (goe363-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe363-il | 50,000 | 9 | 32.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe363-il | 50,000 | 5 | 37 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe363-il | 100,000 | 9 | 53.3 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe363-il | 100,000 | 5 | 52.3 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe363-il | 200,000 | 9 | 70.1 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe363-il | 200,000 | 5 | 65.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe363-il | 500,000 | 9 | 89.5 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe363-il | 500,000 | 5 | 88.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe363-il | 1,000,000 | 9 | 110.5 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe363-il | 1,000,000 | 5 | 104.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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