GOE 590 AIRFOIL (goe590-il)
GOE 590 AIRFOIL - Gottingen 590 airfoil
| Details | Dat file | Parser | |
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(goe590-il) GOE 590 AIRFOIL Gottingen 590 airfoil Max thickness 5.7% at 30% chord. Max camber 4% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 590 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124900 0.0110100
0.0249900 0.0165100
0.0499900 0.0255200
0.0749800 0.0330400
0.0999800 0.0400500
0.1499700 0.0510700
0.1999700 0.0596000
0.2999700 0.0686500
0.3999700 0.0672000
0.4999700 0.0592500
0.5999800 0.0493000
0.6999800 0.0368500
0.7999900 0.0249000
0.8999900 0.0124500
0.9500000 0.0064700
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0049900
0.0250000 -.0049900
0.0500000 -.0034700
0.0750000 -.0009600
0.1000000 0.0015500
0.1500000 0.0060700
0.2000000 0.0091000
0.2999900 0.0116500
0.3999900 0.0107000
0.5000000 0.0052500
0.6000000 0.0003000
0.7000000 -.0041500
0.8000000 -.0046000
0.9000000 -.0040500
0.9500000 -.0025200
1.0000000 0.0000000
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Polars for GOE 590 AIRFOIL (goe590-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe590-il | 50,000 | 9 | 37.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe590-il | 50,000 | 5 | 38.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe590-il | 100,000 | 9 | 52.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe590-il | 100,000 | 5 | 53.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe590-il | 200,000 | 9 | 67.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe590-il | 200,000 | 5 | 70.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe590-il | 500,000 | 9 | 94.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe590-il | 500,000 | 5 | 93.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe590-il | 1,000,000 | 9 | 114.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe590-il | 1,000,000 | 5 | 111.5 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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