GOE 287 AIRFOIL (goe287-il)
GOE 287 AIRFOIL - Gottingen 287 airfoil
| Details | Dat file | Parser | |
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(goe287-il) GOE 287 AIRFOIL Gottingen 287 airfoil Max thickness 8.9% at 29.9% chord. Max camber 4.9% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 287 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123600 0.0171000
0.0247900 0.0261000
0.0496600 0.0423000
0.0745600 0.0547000
0.0994800 0.0637100
0.1493700 0.0777100
0.1993100 0.0851100
0.2992500 0.0923200
0.3992500 0.0926300
0.4993300 0.0828400
0.5994400 0.0689600
0.6995700 0.0526700
0.7997200 0.0346800
0.8998600 0.0178900
0.9499300 0.0088900
1.0000000 0.0025000
0.0000000 0.0000000
0.0125800 -.0098000
0.0250800 -.0104000
0.0500700 -.0089900
0.0750600 -.0070900
0.1000400 -.0050900
0.1500200 -.0022800
0.2000100 -.0001000
0.2999700 0.0036300
0.3999600 0.0050400
0.4999600 0.0052500
0.5999700 0.0036600
0.6999800 0.0018700
0.8000000 0.0005800
0.9000100 -.0009100
0.9500100 -.0017000
1.0000000 -.0025000
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Polars for GOE 287 AIRFOIL (goe287-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe287-il | 50,000 | 9 | 36.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe287-il | 50,000 | 5 | 38 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe287-il | 100,000 | 9 | 58.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe287-il | 100,000 | 5 | 59.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe287-il | 200,000 | 9 | 80 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe287-il | 200,000 | 5 | 77.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe287-il | 500,000 | 9 | 106.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe287-il | 500,000 | 5 | 94.5 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe287-il | 1,000,000 | 9 | 123 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe287-il | 1,000,000 | 5 | 106.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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