GOE 456 AIRFOIL (goe456-il)
GOE 456 AIRFOIL - Gottingen 456 airfoil
| Details | Dat file | Parser | |
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(goe456-il) GOE 456 AIRFOIL Gottingen 456 airfoil Max thickness 7.2% at 29.9% chord. Max camber 5.2% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 456 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124100 0.0125900
0.0248400 0.0206900
0.0497400 0.0343700
0.0746600 0.0450600
0.0996000 0.0537500
0.1495100 0.0656200
0.1994500 0.0735000
0.2993700 0.0837500
0.3993500 0.0870000
0.4993800 0.0827500
0.5994500 0.0735000
0.6995400 0.0607500
0.7996700 0.0435000
0.8998300 0.0232500
0.9499100 0.0121200
1.0000000 0.0000000
0.0000000 0.0000000
0.0125300 -.0048100
0.0250400 -.0063100
0.0500600 -.0076200
0.0750600 -.0079400
0.1000500 -.0067500
0.1499900 -.0019300
0.1999800 0.0030000
0.2999100 0.0117500
0.3998700 0.0170000
0.4998600 0.0187500
0.5998600 0.0185000
0.6998700 0.0167500
0.7999099 0.0125000
0.8999600 0.0057500
0.9499800 0.0031200
1.0000000 0.0000000
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Polars for GOE 456 AIRFOIL (goe456-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe456-il | 50,000 | 9 | 42.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe456-il | 50,000 | 5 | 42.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe456-il | 100,000 | 9 | 65.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe456-il | 100,000 | 5 | 64.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe456-il | 200,000 | 9 | 87.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe456-il | 200,000 | 5 | 86.3 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe456-il | 500,000 | 9 | 117.9 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe456-il | 500,000 | 5 | 115.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe456-il | 1,000,000 | 9 | 140.9 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe456-il | 1,000,000 | 5 | 134.3 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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