GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL (goe322-il)
GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL - Gottingen 322 (Hansa-Brandenburg IV.1) airfoil
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(goe322-il) GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL Gottingen 322 (Hansa-Brandenburg IV.1) airfoil Max thickness 13.1% at 29.8% chord. Max camber 6% at 29.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0121400 0.0246800
0.0244300 0.0395500
0.0491100 0.0612100
0.0738700 0.0778700
0.0986800 0.0909300
0.1484500 0.1071500
0.1983000 0.1173800
0.2981800 0.1255200
0.3982100 0.1234700
0.4983700 0.1122300
0.5986300 0.0941800
0.6989800 0.0706400
0.7993100 0.0474900
0.8996300 0.0257400
0.9497899 0.0142700
1.0000000 0.0030000
0.0000000 0.0000000
0.0127000 -.0138200
0.0252300 -.0158300
0.0502400 -.0167700
0.0752200 -.0154100
0.1002000 -.0140500
0.1501500 -.0103200
0.2001200 -.0081000
0.3000700 -.0051500
0.4000600 -.0042000
0.5000600 -.0041500
0.6000600 -.0038000
0.7000600 -.0038500
0.8000500 -.0034000
0.9000500 -.0033500
0.9500500 -.0036200
1.0000000 -.0030000
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Polars for GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL (goe322-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe322-il | 50,000 | 9 | 9.2 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 50,000 | 5 | 28.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe322-il | 100,000 | 9 | 49.9 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 100,000 | 5 | 53.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe322-il | 200,000 | 9 | 75.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 200,000 | 5 | 73.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe322-il | 500,000 | 9 | 104.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 500,000 | 5 | 95.7 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe322-il | 1,000,000 | 9 | 123.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 1,000,000 | 5 | 114.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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