GOE 385 AIRFOIL (goe385-il)
GOE 385 AIRFOIL - Gottingen 385 airfoil
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(goe385-il) GOE 385 AIRFOIL Gottingen 385 airfoil Max thickness 9.9% at 29.9% chord. Max camber 4.1% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 385 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123300 0.0198000
0.0247400 0.0303100
0.0496200 0.0445000
0.0745200 0.0561300
0.0994500 0.0643500
0.1493500 0.0773700
0.1992700 0.0851000
0.2992300 0.0908400
0.3992400 0.0895900
0.4993000 0.0820400
0.5994100 0.0694900
0.6995300 0.0556500
0.7996700 0.0385000
0.8998200 0.0213500
0.9499000 0.0112700
1.0000000 0.0021000
0.0000000 0.0000000
0.0125800 -.0093900
0.0250900 -.0103900
0.0500900 -.0101700
0.0750800 -.0099600
0.1000800 -.0097500
0.1500800 -.0093200
0.2000800 -.0089000
0.3000700 -.0080500
0.4000600 -.0072000
0.5000500 -.0063500
0.6000500 -.0055000
0.7000400 -.0046500
0.8000300 -.0038000
0.9000300 -.0029500
0.9500200 -.0025200
1.0000000 -.0021000
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Polars for GOE 385 AIRFOIL (goe385-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe385-il | 50,000 | 9 | 29.8 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe385-il | 50,000 | 5 | 37.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe385-il | 100,000 | 9 | 51.8 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe385-il | 100,000 | 5 | 56.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe385-il | 200,000 | 9 | 73 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe385-il | 200,000 | 5 | 72.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe385-il | 500,000 | 9 | 97.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe385-il | 500,000 | 5 | 93.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe385-il | 1,000,000 | 9 | 115.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe385-il | 1,000,000 | 5 | 108.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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