GOE 448 AIRFOIL (goe448-il)
GOE 448 AIRFOIL - Gottingen 448 airfoil
| Details | Dat file | Parser | |
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(goe448-il) GOE 448 AIRFOIL Gottingen 448 airfoil Max thickness 12.9% at 29.8% chord. Max camber 10.5% at 39.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 448 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0121100 0.0265800
0.0243800 0.0425500
0.0490300 0.0672100
0.0737600 0.0855700
0.0985300 0.1012300
0.1482000 0.1240500
0.1979400 0.1421700
0.2976400 0.1626200
0.3975500 0.1688600
0.4976400 0.1629200
0.5978800 0.1458700
0.6982700 0.1194200
0.7987600 0.0854800
0.8993400 0.0457400
0.9496500 0.0238700
1.0000000 0.0013000
0.0000000 0.0000000
0.0126700 -.0119200
0.0252200 -.0151300
0.0502100 -.0146700
0.0751100 -.0078100
0.1000400 -.0027500
0.1498800 0.0079700
0.1997300 0.0188000
0.2995100 0.0339400
0.3994000 0.0414900
0.4993600 0.0442400
0.5994100 0.0403900
0.6995300 0.0323400
0.7996700 0.0227000
0.8998200 0.0125500
0.9499199 0.0053700
1.0000000 -.0013000
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Polars for GOE 448 AIRFOIL (goe448-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe448-il | 50,000 | 9 | 5.4 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe448-il | 50,000 | 5 | 11.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe448-il | 100,000 | 9 | 11.5 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe448-il | 100,000 | 5 | 37 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe448-il | 200,000 | 9 | 162 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe448-il | 200,000 | 5 | 74.5 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe448-il | 500,000 | 9 | 119.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe448-il | 500,000 | 5 | 102.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe448-il | 1,000,000 | 9 | 137.1 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe448-il | 1,000,000 | 5 | 123.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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