GOE 320 (HANSA-BRANDENBURG II.1) AIRFOIL (goe320-il)
GOE 320 (HANSA-BRANDENBURG II.1) AIRFOIL - Gottingen 320 (Hansa-Brandenburg II.1) airfoil
| Details | Dat file | Parser | |
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(goe320-il) GOE 320 (HANSA-BRANDENBURG II.1) AIRFOIL Gottingen 320 (Hansa-Brandenburg II.1) airfoil Max thickness 12.3% at 29.8% chord. Max camber 6.2% at 29.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 320 (HANSA-BRANDENBURG II.1) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0119100 0.0319200
0.0241400 0.0462500
0.0487200 0.0689000
0.0734200 0.0849600
0.0982000 0.0970200
0.1479500 0.1106400
0.1977900 0.1189700
0.2977100 0.1235200
0.3977400 0.1215800
0.4978900 0.1139400
0.5981900 0.0978000
0.6985800 0.0764600
0.7990400 0.0518200
0.8995000 0.0271900
0.9497300 0.0146200
1.0000000 0.0026500
0.0000000 0.0000000
0.0128700 -.0188600
0.0253800 -.0207300
0.0503500 -.0187700
0.0752900 -.0158000
0.1002300 -.0126400
0.1501300 -.0068200
0.2000600 -.0034900
0.3000000 0.0002600
0.3999800 0.0012200
0.4999800 0.0012700
0.5999900 0.0005300
0.7000100 -.0003100
0.8000200 -.0010600
0.9000400 -.0020000
0.9500500 -.0025800
1.0000000 -.0026500
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Polars for GOE 320 (HANSA-BRANDENBURG II.1) AIRFOIL (goe320-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe320-il | 50,000 | 9 | 29.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe320-il | 50,000 | 5 | 33.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe320-il | 100,000 | 9 | 52.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe320-il | 100,000 | 5 | 48.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe320-il | 200,000 | 9 | 66.1 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe320-il | 200,000 | 5 | 63.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe320-il | 500,000 | 9 | 89.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe320-il | 500,000 | 5 | 85 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe320-il | 1,000,000 | 9 | 109.1 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe320-il | 1,000,000 | 5 | 98.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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