GOE 677 (= M 6) AIRFOIL (goe677-il)
GOE 677 (= M 6) AIRFOIL - Gottingen 677 (= M 6) airfoil
| Details | Dat file | Parser | |
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(goe677-il) GOE 677 (= M 6) AIRFOIL Gottingen 677 (= M 6) airfoil Max thickness 12% at 30% chord. Max camber 2.2% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 677 (= M 6) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0180300
0.0250000 0.0275500
0.0500000 0.0406000
0.0750000 0.0491500
0.1000000 0.0567000
0.1500000 0.0678000
0.2000000 0.0754000
0.3000000 0.0826000
0.4000000 0.0808000
0.5000000 0.0745000
0.6000000 0.0617000
0.7000000 0.0474000
0.8000000 0.0331000
0.9000000 0.0183000
0.9500000 0.0114000
1.0000000 0.0040000
0.0000000 0.0000000
0.0125000 -.0169700
0.0250000 -.0224500
0.0500000 -.0274000
0.0750000 -.0298500
0.1000000 -.0318000
0.1500000 -.0337000
0.2000000 -.0356000
0.3000000 -.0369000
0.4000000 -.0377000
0.5000000 -.0370000
0.6000000 -.0358000
0.7000000 -.0321000
0.8000000 -.0259000
0.9000000 -.0147000
0.9500000 -.0076000
1.0000000 0.0000000
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Similar airfoils
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Polars for GOE 677 (= M 6) AIRFOIL (goe677-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe677-il | 50,000 | 9 | 29.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe677-il | 50,000 | 5 | 33 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe677-il | 100,000 | 9 | 49.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe677-il | 100,000 | 5 | 48.9 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe677-il | 200,000 | 9 | 66.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe677-il | 200,000 | 5 | 63.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe677-il | 500,000 | 9 | 87.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe677-il | 500,000 | 5 | 73.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe677-il | 1,000,000 | 9 | 94.1 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe677-il | 1,000,000 | 5 | 81.1 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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