GOE 495 AIRFOIL (goe495-il)
GOE 495 AIRFOIL - Gottingen 495 airfoil
| Details | Dat file | Parser | |
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(goe495-il) GOE 495 AIRFOIL Gottingen 495 airfoil Max thickness 6.9% at 30% chord. Max camber 5% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 495 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0166400
0.0250000 0.0237900
0.0500000 0.0345700
0.0750000 0.0428600
0.1000000 0.0496500
0.1500000 0.0597200
0.2000000 0.0678000
0.3000000 0.0774500
0.4000000 0.0806000
0.5000000 0.0777500
0.6000000 0.0704000
0.7000000 0.0585500
0.8000000 0.0422000
0.9000000 0.0233500
0.9500000 0.0124200
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0078600
0.0250000 -.0097100
0.0500000 -.0109200
0.0750000 -.0106400
0.1000000 -.0093500
0.1500000 -.0052700
0.2000000 -.0007000
0.3000000 0.0084500
0.4000000 0.0166000
0.5000000 0.0222500
0.6000000 0.0249000
0.7000000 0.0240500
0.8000000 0.0192000
0.9000000 0.0108500
0.9500000 0.0059200
1.0000000 0.0000000
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Polars for GOE 495 AIRFOIL (goe495-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe495-il | 50,000 | 9 | 44.8 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe495-il | 50,000 | 5 | 45.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe495-il | 100,000 | 9 | 69.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe495-il | 100,000 | 5 | 69.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe495-il | 200,000 | 9 | 95.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe495-il | 200,000 | 5 | 93.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe495-il | 500,000 | 9 | 132.8 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe495-il | 500,000 | 5 | 122.7 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe495-il | 1,000,000 | 9 | 158.9 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe495-il | 1,000,000 | 5 | 126.9 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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