GOE 371 AIRFOIL (goe371-il)
GOE 371 AIRFOIL - Gottingen 371 airfoil
| Details | Dat file | Parser | |
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(goe371-il) GOE 371 AIRFOIL Gottingen 371 airfoil Max thickness 7% at 29.9% chord. Max camber 4.6% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 371 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123900 0.0175800
0.0248300 0.0266600
0.0497500 0.0388200
0.0746900 0.0479900
0.0996400 0.0551500
0.1495800 0.0649700
0.1995300 0.0718000
0.2994800 0.0794500
0.3994900 0.0786000
0.4995200 0.0737500
0.5995700 0.0659000
0.6996601 0.0525500
0.7997600 0.0372000
0.8998700 0.0198500
0.9499300 0.0101700
1.0000000 0.0000000
0.0000000 0.0000000
0.0125500 -.0074200
0.0250500 -.0073400
0.0500400 -.0061700
0.0750300 -.0045100
0.1000200 -.0023500
0.1499900 0.0014700
0.1999700 0.0048000
0.2999400 0.0099500
0.3999100 0.0136000
0.4999000 0.0152500
0.5999000 0.0149000
0.6999199 0.0125500
0.7999400 0.0092000
0.8999700 0.0043500
0.9499900 0.0016700
1.0000000 0.0000000
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Polars for GOE 371 AIRFOIL (goe371-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe371-il | 50,000 | 9 | 37.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe371-il | 50,000 | 5 | 43.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe371-il | 100,000 | 9 | 61.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe371-il | 100,000 | 5 | 62.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe371-il | 200,000 | 9 | 82 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe371-il | 200,000 | 5 | 80 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe371-il | 500,000 | 9 | 108.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe371-il | 500,000 | 5 | 103.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe371-il | 1,000,000 | 9 | 129.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe371-il | 1,000,000 | 5 | 120.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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