GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL (goe303-il)
GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL - Gottingen 303 (Friedrichshafen G03) airfoil
| Details | Dat file | Parser | |
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(goe303-il) GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL Gottingen 303 (Friedrichshafen G03) airfoil Max thickness 9.8% at 29.9% chord. Max camber 5.9% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122400 0.0258300
0.0246200 0.0372500
0.0494600 0.0530100
0.0743400 0.0647600
0.0992400 0.0745200
0.1490900 0.0887300
0.1990100 0.0970400
0.2989100 0.1059600
0.3989100 0.1062900
0.4989800 0.0993100
0.5991000 0.0873400
0.6992700 0.0716700
0.7994600 0.0526900
0.8997000 0.0292200
0.9498300 0.0167400
1.0000000 0.0022500
0.0000000 0.0000000
0.0126200 -.0105800
0.0251300 -.0122400
0.0501200 -.0119900
0.0751000 -.0099300
0.1000800 -.0074700
0.1500300 -.0024600
0.1999800 0.0021500
0.2999200 0.0075700
0.3998800 0.0113000
0.4998700 0.0123200
0.5998900 0.0111500
0.6999100 0.0087700
0.7999400 0.0057000
0.8999900 0.0012200
0.9500100 -.0011600
1.0000000 -.0022500
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Polars for GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL (goe303-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe303-il | 50,000 | 9 | 26.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe303-il | 50,000 | 5 | 39.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe303-il | 100,000 | 9 | 58.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe303-il | 100,000 | 5 | 61.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe303-il | 200,000 | 9 | 83.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe303-il | 200,000 | 5 | 81.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe303-il | 500,000 | 9 | 114.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe303-il | 500,000 | 5 | 106.4 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe303-il | 1,000,000 | 9 | 137.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe303-il | 1,000,000 | 5 | 122.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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