SIKORSKY SC2110 AIRFOIL (sc2110-il)
SIKORSKY SC2110 AIRFOIL - Sikorsky/Lednicer & Owen SC2110 rotorcraft airfoil (SC5410)
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(sc2110-il) SIKORSKY SC2110 AIRFOIL Sikorsky/Lednicer & Owen SC2110 rotorcraft airfoil (SC5410) Max thickness 9.9% at 37.7% chord. Max camber 1.9% at 15.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
SIKORSKY SC2110 AIRFOIL
41. 47.
0.0 0.0000000
0.0041792 0.0122162
0.0065891 0.0158434
0.0114686 0.0216807
0.0238180 0.0321074
0.0486772 0.0449249
0.0736368 0.0526535
0.0986465 0.0576708
0.1487162 0.0633128
0.1988561 0.0658160
0.2490259 0.0667050
0.2992060 0.0667340
0.3375290 0.0664244
0.3774060 0.0658768
0.4172812 0.0650583
0.4372171 0.0645115
0.4571522 0.0638477
0.4770852 0.0630549
0.4970183 0.0621352
0.5368804 0.0599266
0.5568104 0.0586409
0.5767395 0.0572281
0.5966676 0.0556763
0.6365188 0.0521118
0.6564451 0.0500760
0.6763662 0.0478612
0.6962884 0.0454614
0.7361247 0.0401158
0.7560418 0.0371861
0.7759559 0.0341053
0.7958711 0.0308945
0.8356976 0.0241659
0.8556108 0.0206912
0.8755220 0.0171784
0.8954352 0.0136696
0.9352626 0.0070730
0.9551798 0.0043813
0.9751059 0.0025825
0.9850739 0.0022181
0.9950449 0.0023647
1.0000000 0.0026760
0.0 0.0000000
0.0022484 -.0061159
0.0048475 -.0081437
0.0104667 -.0104373
0.0226118 -.0130796
0.0347099 -.0149399
0.0407510 -.0157545
0.0528190 -.0171948
0.0789273 -.0196542
0.0989823 -.0211369
0.1290354 -.0229861
0.1573386 -.0245304
0.1722866 -.0253165
0.2021857 -.0268727
0.2320818 -.0283878
0.2470309 -.0291099
0.2769289 -.0304381
0.3068300 -.0315753
0.3367340 -.0324964
0.3766071 -.0333630
0.4164851 -.0337986
0.4364251 -.0338504
0.4563661 -.0337911
0.4763082 -.0336169
0.4962491 -.0333226
0.5361381 -.0323672
0.5560830 -.0317080
0.5760300 -.0309348
0.5959779 -.0300546
0.6358737 -.0279932
0.6558247 -.0268179
0.6757756 -.0255517
0.6957266 -.0241985
0.7356305 -.0212521
0.7555832 -.0196779
0.7755351 -.0180517
0.7954900 -.0163834
0.8353968 -.0129550
0.8553527 -.0112028
0.8753066 -.0094236
0.8952615 -.0076154
0.9351713 -.0040499
0.9551232 -.0024657
0.9750731 -.0012615
0.9850470 -.0009119
0.9950181 -.0008203
1.0000000 -.0008990
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Polars for SIKORSKY SC2110 AIRFOIL (sc2110-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| sc2110-il | 50,000 | 9 | 26.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc2110-il | 50,000 | 5 | 27.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc2110-il | 100,000 | 9 | 34.7 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc2110-il | 100,000 | 5 | 38.9 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc2110-il | 200,000 | 9 | 47.6 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc2110-il | 200,000 | 5 | 52.8 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc2110-il | 500,000 | 9 | 71.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc2110-il | 500,000 | 5 | 74.3 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc2110-il | 1,000,000 | 9 | 91.7 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc2110-il | 1,000,000 | 5 | 92.1 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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