GOE 492 AIRFOIL (goe492-il)
GOE 492 AIRFOIL - Gottingen 492 airfoil
| Details | Dat file | Parser | |
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(goe492-il) GOE 492 AIRFOIL Gottingen 492 airfoil Max thickness 6.2% at 29.9% chord. Max camber 3.4% at 49.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 492 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123800 0.0096500
0.0248100 0.0148100
0.0497200 0.0226200
0.0746300 0.0294300
0.0995400 0.0344000
0.1494500 0.0438700
0.1993600 0.0514900
0.2992300 0.0612400
0.3991900 0.0644900
0.4992200 0.0627400
0.5992900 0.0564900
0.6994000 0.0477400
0.7995600 0.0349900
0.8997700 0.0187500
0.9498800 0.0098700
1.0000000 0.0000000
0.0000000 0.0000000
0.0125900 -.0073400
0.0251200 -.0096900
0.0501400 -.0108700
0.0751400 -.0115600
0.1001400 -.0115500
0.1501300 -.0109000
0.2001100 -.0085000
0.3000100 -.0007500
0.3999900 0.0025000
0.4999400 0.0047500
0.5999100 0.0070000
0.6999000 0.0077500
0.7999099 0.0075000
0.8999500 0.0039500
0.9499700 0.0021700
1.0000000 0.0000000
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Polars for GOE 492 AIRFOIL (goe492-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe492-il | 50,000 | 9 | 31.1 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe492-il | 50,000 | 5 | 39 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe492-il | 100,000 | 9 | 57.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe492-il | 100,000 | 5 | 57.4 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe492-il | 200,000 | 9 | 81.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe492-il | 200,000 | 5 | 78.6 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe492-il | 500,000 | 9 | 112 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe492-il | 500,000 | 5 | 99.4 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe492-il | 1,000,000 | 9 | 128.6 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe492-il | 1,000,000 | 5 | 95.5 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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