GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL (goe321-il)
GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL - Gottingen 321 (Hansa-Brandenburg III.1) airfoil
| Details | Dat file | Parser | |
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(goe321-il) GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL Gottingen 321 (Hansa-Brandenburg III.1) airfoil Max thickness 11.2% at 29.9% chord. Max camber 5.1% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0121400 0.0256700
0.0244800 0.0378400
0.0492200 0.0559800
0.0740400 0.0695300
0.0988900 0.0800700
0.1487200 0.0924600
0.1986100 0.1004500
0.2985100 0.1072300
0.3985400 0.1055200
0.4987000 0.0941100
0.5989100 0.0784900
0.6991900 0.0585800
0.7994500 0.0397700
0.8997100 0.0209600
0.9498500 0.0109600
1.0000000 0.0021500
0.0000000 0.0000000
0.0127000 -.0137200
0.0252200 -.0156500
0.0502100 -.0148000
0.0751800 -.0128600
0.1001500 -.0111100
0.1501200 -.0086200
0.2000900 -.0067300
0.3000600 -.0043400
0.4000500 -.0036600
0.5000700 -.0047700
0.6000700 -.0051900
0.7000700 -.0047000
0.8000500 -.0038200
0.9000500 -.0035300
0.9500400 -.0028400
1.0000000 -.0021500
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Polars for GOE 321 (HANSA-BRANDENBURG III.1) AIRFOIL (goe321-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe321-il | 50,000 | 9 | 20.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe321-il | 50,000 | 5 | 34.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe321-il | 100,000 | 9 | 54.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe321-il | 100,000 | 5 | 55.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe321-il | 200,000 | 9 | 77.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe321-il | 200,000 | 5 | 73.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe321-il | 500,000 | 9 | 105.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe321-il | 500,000 | 5 | 90.3 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe321-il | 1,000,000 | 9 | 120.9 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe321-il | 1,000,000 | 5 | 104.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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