GOE 403 AIRFOIL (goe403-il)
GOE 403 AIRFOIL - Gottingen 403 airfoil
| Details | Dat file | Parser | |
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(goe403-il) GOE 403 AIRFOIL Gottingen 403 airfoil Max thickness 6.7% at 29.9% chord. Max camber 4.3% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 403 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123900 0.0106300
0.0248100 0.0182600
0.0496800 0.0300200
0.0745800 0.0397800
0.0995000 0.0480400
0.1493700 0.0595700
0.1992900 0.0675900
0.2992100 0.0751400
0.3992200 0.0741900
0.4992800 0.0682400
0.5993700 0.0597900
0.6995000 0.0478400
0.7996500 0.0329000
0.8998100 0.0179500
0.9499000 0.0094700
1.0000000 0.0000000
0.0000000 0.0000000
0.0125800 -.0078700
0.0251000 -.0097400
0.0501000 -.0099700
0.0750900 -.0087100
0.1000700 -.0064500
0.1500200 -.0019200
0.1999800 0.0021000
0.2999100 0.0086500
0.3998700 0.0122000
0.4998600 0.0137500
0.5998700 0.0128000
0.6998900 0.0103500
0.7999200 0.0074000
0.8999600 0.0039500
0.9499800 0.0019700
1.0000000 0.0000000
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Polars for GOE 403 AIRFOIL (goe403-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe403-il | 50,000 | 9 | 42.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe403-il | 50,000 | 5 | 41.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe403-il | 100,000 | 9 | 59.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe403-il | 100,000 | 5 | 57.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe403-il | 200,000 | 9 | 75.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe403-il | 200,000 | 5 | 73 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe403-il | 500,000 | 9 | 98.6 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe403-il | 500,000 | 5 | 92.9 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe403-il | 1,000,000 | 9 | 116.1 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe403-il | 1,000,000 | 5 | 107.9 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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