GOE 277 (DAIMLER VIII) AIRFOIL (goe277-il)
GOE 277 (DAIMLER VIII) AIRFOIL - Gottingen 277 (DAIMLER VIII) airfoil
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(goe277-il) GOE 277 (DAIMLER VIII) AIRFOIL Gottingen 277 (DAIMLER VIII) airfoil Max thickness 8.3% at 29.9% chord. Max camber 4.4% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 277 (DAIMLER VIII) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123300 0.0185100
0.0247500 0.0283200
0.0496200 0.0427500
0.0745300 0.0526700
0.0994500 0.0609000
0.1493400 0.0735400
0.1992700 0.0813900
0.2992300 0.0855900
0.3992500 0.0831900
0.4993100 0.0761900
0.5994000 0.0662900
0.6995201 0.0533000
0.7996500 0.0391000
0.8998100 0.0214000
0.9498900 0.0117500
1.0000000 0.0016000
0.0000000 0.0000000
0.0125900 -.0094900
0.0250900 -.0103700
0.0500800 -.0090500
0.0750600 -.0077500
0.1000500 -.0063900
0.1500300 -.0037500
0.2000100 -.0015000
0.2999800 0.0022000
0.3999700 0.0038000
0.4999600 0.0047000
0.5999600 0.0044000
0.6999700 0.0033600
0.7999800 0.0022000
0.8999900 0.0007000
0.9500100 -.0005500
1.0000000 -.0016000
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Polars for GOE 277 (DAIMLER VIII) AIRFOIL (goe277-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe277-il | 50,000 | 9 | 34 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe277-il | 50,000 | 5 | 38.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe277-il | 100,000 | 9 | 54.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe277-il | 100,000 | 5 | 55.7 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe277-il | 200,000 | 9 | 73.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe277-il | 200,000 | 5 | 73.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe277-il | 500,000 | 9 | 100.9 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe277-il | 500,000 | 5 | 98.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe277-il | 1,000,000 | 9 | 122.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe277-il | 1,000,000 | 5 | 118.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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