GOE 282 (DAIMLER XIII) AIRFOIL (goe282-il)
GOE 282 (DAIMLER XIII) AIRFOIL - Gottingen 282 (DAIMLER XIII) airfoil
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(goe282-il) GOE 282 (DAIMLER XIII) AIRFOIL Gottingen 282 (DAIMLER XIII) airfoil Max thickness 9.1% at 19.9% chord. Max camber 5% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 282 (DAIMLER XIII) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122600 0.0189600
0.0245800 0.0325200
0.0493800 0.0483400
0.0742400 0.0588600
0.0991300 0.0677800
0.1489600 0.0807200
0.1988700 0.0877700
0.2987800 0.0946500
0.3987900 0.0941400
0.4988700 0.0874400
0.5989900 0.0779300
0.6991700 0.0647200
0.7993700 0.0489100
0.8996400 0.0282100
0.9497899 0.0165500
1.0000000 0.0032000
0.0000000 0.0000000
0.0126300 -.0100400
0.0251700 -.0128800
0.0501900 -.0145500
0.0752000 -.0151300
0.1001800 -.0139100
0.1501100 -.0087600
0.2000400 -.0033200
0.2999500 0.0039700
0.3998900 0.0063200
0.4999000 0.0075500
0.5999000 0.0077400
0.6999199 0.0063300
0.7999500 0.0039200
0.8999900 0.0005100
0.9500200 -.0013400
1.0000000 -.0032000
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Polars for GOE 282 (DAIMLER XIII) AIRFOIL (goe282-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe282-il | 50,000 | 9 | 34.8 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe282-il | 50,000 | 5 | 41 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe282-il | 100,000 | 9 | 57 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe282-il | 100,000 | 5 | 59 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe282-il | 200,000 | 9 | 77.4 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe282-il | 200,000 | 5 | 75.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe282-il | 500,000 | 9 | 102.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe282-il | 500,000 | 5 | 94.8 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe282-il | 1,000,000 | 9 | 118.3 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe282-il | 1,000,000 | 5 | 105.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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