GOE 288 AIRFOIL (goe288-il)
GOE 288 AIRFOIL - Gottingen 288 airfoil
| Details | Dat file | Parser | |
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(goe288-il) GOE 288 AIRFOIL Gottingen 288 airfoil Max thickness 17.4% at 29.3% chord. Max camber 5.5% at 39.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 288 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0110700 0.0272800
0.0228300 0.0414000
0.0467300 0.0624500
0.0709000 0.0784100
0.0951800 0.0921800
0.1440600 0.1134400
0.1933700 0.1266200
0.2928500 0.1365300
0.3929200 0.1352700
0.4935400 0.1234400
0.5944900 0.1052200
0.6956000 0.0840100
0.7968600 0.0599200
0.8982800 0.0329200
0.9490300 0.0184800
1.0000000 0.0029500
0.0000000 0.0000000
0.0137300 -.0233800
0.0265600 -.0298100
0.0519500 -.0372800
0.0771900 -.0417600
0.1023100 -.0440400
0.1523800 -.0455200
0.2023400 -.0447100
0.3019200 -.0365900
0.4012400 -.0237000
0.5006600 -.0125900
0.6002400 -.0044800
0.6999900 0.0001400
0.7999300 0.0012800
0.8999700 0.0006100
0.9500500 -.0009600
1.0000000 -.0029500
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Polars for GOE 288 AIRFOIL (goe288-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe288-il | 50,000 | 9 | 7.6 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe288-il | 50,000 | 5 | 27.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe288-il | 100,000 | 9 | 43.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe288-il | 100,000 | 5 | 50.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe288-il | 200,000 | 9 | 70.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe288-il | 200,000 | 5 | 69.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe288-il | 500,000 | 9 | 96.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe288-il | 500,000 | 5 | 91.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe288-il | 1,000,000 | 9 | 117.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe288-il | 1,000,000 | 5 | 113.9 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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