SIKORSKY SC1094 R8 AIRFOIL (sc1094r8-il)
SIKORSKY SC1094 R8 AIRFOIL - Sikorsky/Velkoff SC1094 R8 rotorcraft airfoil
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(sc1094r8-il) SIKORSKY SC1094 R8 AIRFOIL Sikorsky/Velkoff SC1094 R8 rotorcraft airfoil Max thickness 9.4% at 27.8% chord. Max camber 2.1% at 21.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
SIKORSKY SC1094 R8 AIRFOIL
73. 73.
0.0000001 0.0000000
0.0001326 0.0018510
0.0009025 0.0055901
0.0021777 0.0094525
0.0042705 0.0139808
0.0068617 0.0182453
0.0094396 0.0217380
0.0125228 0.0253169
0.0186672 0.0312568
0.0224520 0.0344074
0.0285712 0.0388986
0.0346773 0.0426378
0.0407725 0.0457552
0.0468590 0.0483686
0.0529385 0.0505822
0.0610366 0.0530585
0.0711484 0.0555760
0.0812534 0.0576404
0.0913514 0.0593719
0.1014458 0.0608284
0.1115353 0.0620639
0.1266648 0.0635857
0.1417878 0.0647887
0.1569077 0.0657616
0.1720245 0.0665556
0.1871373 0.0671757
0.2022481 0.0676237
0.2173548 0.0678988
0.2324597 0.0680089
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0.2777603 0.0675784
0.2928576 0.0672485
0.3129842 0.0667091
0.3331099 0.0660607
0.3532338 0.0653104
0.3733560 0.0644619
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0.9764083 0.0039792
0.9864605 0.0030141
0.9965117 0.0020490
1.0000000 0.0017117
0.0000000 0.0000000
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0.6739418 -.0198466
0.6940945 -.0188912
0.7142490 -.0178819
0.7344044 -.0168235
0.7545605 -.0157202
0.7747174 -.0145779
0.7948748 -.0134016
0.8150318 -.0121963
0.8351902 -.0109669
0.8553490 -.0097176
0.8755080 -.0084524
0.8956673 -.0071751
0.9158267 -.0058867
0.9259060 -.0052361
0.9359855 -.0045754
0.9460661 -.0039038
0.9561460 -.0032172
0.9662273 -.0025135
0.9762995 -.0022738
0.9863726 -.0020341
0.9964448 -.0017954
1.0000000 -.0017117
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Polars for SIKORSKY SC1094 R8 AIRFOIL (sc1094r8-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| sc1094r8-il | 50,000 | 9 | 24.5 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1094r8-il | 50,000 | 5 | 27.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1094r8-il | 100,000 | 9 | 33.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1094r8-il | 100,000 | 5 | 37.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1094r8-il | 200,000 | 9 | 45.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1094r8-il | 200,000 | 5 | 50.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1094r8-il | 500,000 | 9 | 67.8 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1094r8-il | 500,000 | 5 | 72.5 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc1094r8-il | 1,000,000 | 9 | 88.3 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc1094r8-il | 1,000,000 | 5 | 91.7 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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