GOE 396 AIRFOIL (goe396-il)
GOE 396 AIRFOIL - Gottingen 396 airfoil
| Details | Dat file | Parser | |
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(goe396-il) GOE 396 AIRFOIL Gottingen 396 airfoil Max thickness 4.7% at 30% chord. Max camber 5.8% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 396 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0120400
0.0250000 0.0200700
0.0500000 0.0321500
0.0750000 0.0412200
0.1000000 0.0473000
0.1500000 0.0584500
0.2000000 0.0676000
0.3000000 0.0779000
0.4000000 0.0802000
0.5000000 0.0765000
0.6000000 0.0678000
0.7000000 0.0551000
0.8000000 0.0384000
0.9000000 0.0207000
0.9500000 0.0108500
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0039600
0.0250000 -.0039300
0.0500000 -.0018500
0.0750000 0.0012300
0.1000000 0.0053000
0.1500000 0.0134500
0.2000000 0.0206000
0.3000000 0.0309000
0.4000000 0.0352000
0.5000000 0.0325000
0.6000000 0.0278000
0.7000000 0.0211000
0.8000000 0.0134000
0.9000000 0.0057000
0.9500000 0.0018500
1.0000000 0.0000000
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Polars for GOE 396 AIRFOIL (goe396-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe396-il | 50,000 | 9 | 44.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe396-il | 50,000 | 5 | 44.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe396-il | 100,000 | 9 | 67 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe396-il | 100,000 | 5 | 66.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe396-il | 200,000 | 5 | 89.1 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe396-il | 200,000 | 0 | 92.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe396-il | 500,000 | 9 | 121.3 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe396-il | 500,000 | 5 | 111.2 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe396-il | 1,000,000 | 9 | 141.7 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe396-il | 1,000,000 | 5 | 99.8 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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