GOE 527 AIRFOIL (goe527-il)
GOE 527 AIRFOIL - Gottingen 527 airfoil
| Details | Dat file | Parser | |
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(goe527-il) GOE 527 AIRFOIL Gottingen 527 airfoil Max thickness 16.5% at 29.5% chord. Max camber 5.8% at 39.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 527 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0112500 0.0339200
0.0231900 0.0488600
0.0474000 0.0702500
0.0717900 0.0866600
0.0963500 0.0985700
0.1456800 0.1168900
0.1952600 0.1282200
0.2948400 0.1394100
0.3948900 0.1381100
0.4953300 0.1263300
0.5960000 0.1080500
0.6968600 0.0847800
0.7978300 0.0585200
0.8988800 0.0302600
0.9494200 0.0156300
1.0000000 0.0000000
0.0000000 0.0000000
0.0130900 -.0160200
0.0258000 -.0215500
0.0510000 -.0271100
0.0760800 -.0291900
0.1011000 -.0297600
0.1511300 -.0304100
0.2010900 -.0295600
0.3009600 -.0258600
0.4007800 -.0211700
0.5005900 -.0159800
0.6004200 -.0112800
0.7002800 -.0075900
0.8001600 -.0043900
0.9000800 -.0022000
0.9500100 -.0003500
1.0000000 0.0000000
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Polars for GOE 527 AIRFOIL (goe527-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe527-il | 50,000 | 9 | 4.3 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 50,000 | 5 | 15.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe527-il | 100,000 | 9 | 36.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 100,000 | 5 | 47 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe527-il | 200,000 | 9 | 69.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 200,000 | 5 | 69.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe527-il | 500,000 | 9 | 102.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 500,000 | 5 | 96.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe527-il | 1,000,000 | 9 | 128.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 1,000,000 | 5 | 116.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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