SD7034 (sd7034-il)
SD7034 - Selig/Donovan SD7034 low Reynolds number airfoil
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(sd7034-il) SD7034 Selig/Donovan SD7034 low Reynolds number airfoil Max thickness 10.5% at 26% chord. Max camber 3.6% at 39.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
SD7034 1.00000 0.0 0.99671 0.00035 0.98696 0.00152 0.97100 0.00374 0.94929 0.00716 0.92233 0.01180 0.89071 0.01761 0.85505 0.02442 0.81592 0.03199 0.77393 0.04005 0.72959 0.04828 0.68344 0.05640 0.63594 0.06411 0.58757 0.07115 0.53876 0.07731 0.48994 0.08241 0.44153 0.08630 0.39394 0.08888 0.34759 0.09010 0.30287 0.08989 0.26015 0.08826 0.21979 0.08524 0.18215 0.08085 0.14751 0.07516 0.11611 0.06824 0.08814 0.06025 0.06376 0.05139 0.04313 0.04191 0.02638 0.03212 0.01368 0.02231 0.00512 0.01280 0.00074 0.00399 0.00061 -0.00325 0.00588 -0.00890 0.01687 -0.01357 0.03299 -0.01707 0.05443 -0.01928 0.08117 -0.02044 0.11296 -0.02072 0.14945 -0.02030 0.19020 -0.01931 0.23472 -0.01783 0.28252 -0.01595 0.33306 -0.01378 0.38576 -0.01142 0.43999 -0.00898 0.49512 -0.00653 0.55052 -0.00420 0.60550 -0.00210 0.65933 -0.00033 0.71132 0.00108 0.76078 0.00209 0.80705 0.00271 0.84952 0.00295 0.88762 0.00287 0.92083 0.00252 0.94870 0.00198 0.97085 0.00133 0.98694 0.00069 0.99672 0.00019 1.00001 0.00000 |
Dat file parser warnings
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
Similar airfoils
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Polars for SD7034 (sd7034-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| sd7034-il | 50,000 | 9 | 27.8 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7034-il | 50,000 | 5 | 37.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7034-il | 100,000 | 9 | 54.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7034-il | 100,000 | 5 | 57.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7034-il | 200,000 | 9 | 77.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7034-il | 200,000 | 5 | 76.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7034-il | 500,000 | 9 | 107.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7034-il | 500,000 | 5 | 99.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7034-il | 1,000,000 | 9 | 128.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7034-il | 1,000,000 | 5 | 116.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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