SIKORSKY SC1095 AIRFOIL (sc1095-il)
SIKORSKY SC1095 AIRFOIL - Sikorsky/Balch SC1095 rotorcraft airfoil
| Details | Dat file | Parser | |
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(sc1095-il) SIKORSKY SC1095 AIRFOIL Sikorsky/Balch SC1095 rotorcraft airfoil Max thickness 9.5% at 26.9% chord. Max camber 0.8% at 26.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
SIKORSKY SC1095 AIRFOIL 71. 71. 0.000000 0.000000 0.000102 0.001466 0.000813 0.003959 0.002034 0.006255 0.004067 0.009133 0.006609 0.012145 0.009151 0.014727 0.012201 0.017476 0.018302 0.022201 0.024403 0.026083 0.030503 0.029338 0.036604 0.032084 0.042705 0.034427 0.050839 0.037069 0.061007 0.039788 0.071174 0.042051 0.081342 0.043977 0.091510 0.045624 0.101678 0.047049 0.116929 0.048852 0.132181 0.050333 0.147433 0.051581 0.162684 0.052648 0.177936 0.053540 0.193188 0.054258 0.208439 0.054802 0.223691 0.055178 0.238943 0.055414 0.254194 0.055527 0.269446 0.055540 0.284697 0.055472 0.305033 0.055281 0.325369 0.054980 0.345704 0.054576 0.366040 0.054074 0.386375 0.053479 0.406711 0.052796 0.427046 0.052028 0.447382 0.051176 0.467717 0.050241 0.488053 0.049223 0.508388 0.048123 0.528724 0.046942 0.549059 0.045679 0.569395 0.044336 0.589731 0.042911 0.610066 0.041404 0.630402 0.039817 0.650737 0.038149 0.671073 0.036402 0.691408 0.034577 0.711744 0.032673 0.732079 0.030696 0.752415 0.028652 0.772750 0.026547 0.793086 0.024387 0.813421 0.022180 0.833757 0.019930 0.854092 0.017642 0.874428 0.015320 0.894764 0.012970 0.915099 0.010595 0.925267 0.009393 0.935435 0.008179 0.945602 0.006950 0.955770 0.005702 0.965938 0.004433 0.976106 0.003603 0.986274 0.002805 0.996441 0.002008 1.000000 0.001729 0.000000 0.000000 0.000102 -0.001117 0.000813 -0.003219 0.002034 -0.005099 0.004067 -0.007565 0.006609 -0.010198 0.009151 -0.012360 0.012201 -0.014526 0.018302 -0.017980 0.024403 -0.020662 0.030503 -0.022933 0.036604 -0.024941 0.042705 -0.026694 0.050839 -0.028620 0.061007 -0.030480 0.071174 -0.031911 0.081342 -0.033043 0.091510 -0.033965 0.101678 -0.034760 0.116929 -0.035795 0.132181 -0.036660 0.147433 -0.037372 0.162684 -0.037948 0.177936 -0.038406 0.193188 -0.038762 0.208439 -0.039032 0.223691 -0.039225 0.238943 -0.039348 0.254194 -0.039410 0.269446 -0.039414 0.284697 -0.039368 0.305033 -0.039236 0.325369 -0.039027 0.345704 -0.038744 0.366040 -0.038392 0.386375 -0.037974 0.406711 -0.037494 0.427046 -0.036952 0.447382 -0.036350 0.467717 -0.035688 0.488053 -0.034966 0.508388 -0.034186 0.528724 -0.033347 0.549059 -0.032448 0.569395 -0.031488 0.589731 -0.030467 0.610066 -0.029384 0.630402 -0.028238 0.650737 -0.027033 0.671073 -0.025771 0.691408 -0.024452 0.711744 -0.023078 0.732079 -0.021655 0.752415 -0.020187 0.772750 -0.018679 0.793086 -0.017137 0.813421 -0.015566 0.833757 -0.013971 0.854092 -0.012355 0.874428 -0.010723 0.894764 -0.009078 0.915099 -0.007424 0.925267 -0.006589 0.935435 -0.005745 0.945602 -0.004889 0.955770 -0.004019 0.965938 -0.003131 0.976106 -0.002713 0.986274 -0.002294 0.996441 -0.001875 1.000000 -0.001729 |
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Polars for SIKORSKY SC1095 AIRFOIL (sc1095-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| sc1095-il | 50,000 | 9 | 25.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1095-il | 50,000 | 5 | 26.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1095-il | 100,000 | 9 | 34.2 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1095-il | 100,000 | 5 | 36.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1095-il | 200,000 | 9 | 45.3 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1095-il | 200,000 | 5 | 48.8 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1095-il | 500,000 | 9 | 69.5 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1095-il | 500,000 | 5 | 70.2 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1095-il | 1,000,000 | 9 | 87 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1095-il | 1,000,000 | 5 | 85.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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