SIKORSKY SC1012R8 AIRFOIL (sc1012r8-il)
SIKORSKY SC1012R8 AIRFOIL - Sikorsky SC1012 R8 rotorcraft airfoil
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(sc1012r8-il) SIKORSKY SC1012R8 AIRFOIL Sikorsky SC1012 R8 rotorcraft airfoil Max thickness 12% at 27.8% chord. Max camber 2.7% at 21.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
SIKORSKY SC1012R8 AIRFOIL
73. 73.
0.0000000 0.0
0.0001526 0.0023631
0.0009628 0.0071345
0.0022805 0.0120628
0.0044225 0.0178414
0.0070605 0.0232845
0.0096766 0.0277409
0.0127985 0.0323080
0.0190079 0.0398884
0.0228275 0.0439090
0.0289958 0.0496395
0.0351429 0.0544112
0.0412723 0.0583893
0.0473875 0.0617245
0.0534912 0.0645500
0.0616161 0.0677098
0.0717559 0.0709216
0.0818828 0.0735571
0.0920003 0.0757663
0.1021101 0.0776243
0.1122134 0.0792010
0.1273594 0.0811430
0.1424959 0.0826792
0.1576262 0.0839201
0.1727512 0.0849331
0.1878716 0.0857247
0.2029868 0.0862958
0.2180973 0.0866479
0.2332031 0.0867885
0.2483050 0.0867503
0.2634032 0.0865582
0.2784988 0.0862389
0.2935920 0.0858184
0.3137137 0.0851294
0.3338320 0.0843022
0.3539476 0.0833442
0.3740605 0.0822620
0.3941706 0.0810630
0.4142784 0.0797535
0.4343839 0.0783362
0.4544868 0.0768125
0.4745874 0.0751832
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0.8761460 0.0221182
0.8962069 0.0187018
0.9162671 0.0152530
0.9262969 0.0135115
0.9363263 0.0117540
0.9463552 0.0099771
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0.9664114 0.0063501
0.9764516 0.0050780
0.9864928 0.0038464
0.9965338 0.0026149
1.0000000 0.0021840
0.0000000 0.0
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0.0017935 -.0098618
0.0037278 -.0134383
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0.0086584 -.0181037
0.0116444 -.0196570
0.0176395 -.0217229
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0.1852635 -.0317123
0.2003585 -.0320497
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0.2456440 -.0330600
0.2607390 -.0333960
0.2758343 -.0337313
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0.3513290 -.0345621
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0.5527750 -.0310791
0.5729286 -.0303139
0.5930842 -.0294709
0.6132417 -.0285493
0.6334006 -.0275498
0.6535614 -.0264746
0.6737238 -.0253261
0.6938877 -.0241069
0.7140532 -.0228193
0.7342201 -.0214683
0.7543880 -.0200606
0.7745572 -.0186028
0.7947274 -.0171016
0.8148985 -.0155639
0.8350701 -.0139953
0.8552424 -.0124010
0.8754151 -.0107861
0.8955882 -.0091556
0.9157615 -.0075125
0.9258484 -.0066813
0.9359356 -.0058387
0.9460230 -.0049813
0.9561108 -.0041054
0.9661992 -.0032072
0.9762744 -.0029017
0.9863496 -.0025963
0.9964249 -.0022907
1.0000000 -.0021840
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Polars for SIKORSKY SC1012R8 AIRFOIL (sc1012r8-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| sc1012r8-il | 50,000 | 9 | 23.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1012r8-il | 50,000 | 5 | 26.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1012r8-il | 100,000 | 9 | 34 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1012r8-il | 100,000 | 5 | 37.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1012r8-il | 200,000 | 9 | 46.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1012r8-il | 200,000 | 5 | 50.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1012r8-il | 500,000 | 9 | 68.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1012r8-il | 500,000 | 5 | 72.1 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1012r8-il | 1,000,000 | 9 | 88.5 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1012r8-il | 1,000,000 | 5 | 90.7 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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