Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

SIKORSKY SC1094 R8 AIRFOIL (sc1094r8-il)

SIKORSKY SC1094 R8 AIRFOIL - Sikorsky/Velkoff SC1094 R8 rotorcraft airfoil


Airfoil sc1094r8-il
Details Dat file Parser  
(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
 0.2475623 0.0679790
 0.2626617 0.0678292
 0.2777603 0.0675784
 0.2928576 0.0672485
 0.3129842 0.0667091
 0.3331099 0.0660607
 0.3532338 0.0653104
 0.3733560 0.0644619
 0.3934767 0.0635226
 0.4135959 0.0624963
 0.4337125 0.0613860
 0.4538288 0.0601917
 0.4739435 0.0589153
 0.4940568 0.0575571
 0.5141689 0.0561178
 0.5342793 0.0545975
 0.5543886 0.0529972
 0.5744953 0.0513160
 0.5946016 0.0495548
 0.6147066 0.0477136
 0.6348101 0.0457914
 0.6549124 0.0437901
 0.6750130 0.0417100
 0.6951115 0.0395518
 0.7152095 0.0373167
 0.7353065 0.0350085
 0.7554021 0.0326344
 0.7754967 0.0302003
 0.7955904 0.0277111
 0.8156822 0.0251750
 0.8357743 0.0225969
 0.8558658 0.0199808
 0.8759568 0.0173327
 0.8960472 0.0146556
 0.9161372 0.0119525
 0.9261814 0.0105875
 0.9362255 0.0092104
 0.9462701 0.0078184
 0.9563136 0.0064074
 0.9663576 0.0049763
 0.9764083 0.0039792
 0.9864605 0.0030141
 0.9965117 0.0020490
 1.0000000 0.0017117

 0.0000000 0.0000000
 0.0000687 -.0017995
 0.0007181 -.0050052
 0.0018787 -.0077289
 0.0038439 -.0105315
 0.0063221 -.0127650
 0.0088143 -.0141866
 0.0118141 -.0154040
 0.0178269 -.0170229
 0.0215446 -.0177337
 0.0275684 -.0187197
 0.0335953 -.0195277
 0.0396252 -.0201718
 0.0456570 -.0206988
 0.0516902 -.0211509
 0.0597363 -.0216590
 0.0697953 -.0221752
 0.0798571 -.0225954
 0.0899190 -.0229426
 0.0999828 -.0232348
 0.1100465 -.0234830
 0.1251442 -.0237888
 0.1402415 -.0240567
 0.1553399 -.0243225
 0.1704383 -.0245864
 0.1855357 -.0248512
 0.2006342 -.0251150
 0.2157315 -.0253799
 0.2308300 -.0256437
 0.2459284 -.0259065
 0.2610257 -.0261704
 0.2761242 -.0264332
 0.2912235 -.0266501
 0.3113556 -.0268705
 0.3314900 -.0270130
 0.3516258 -.0270845
 0.3717628 -.0270860
 0.3919010 -.0270225
 0.4120401 -.0268970
 0.4321793 -.0267115
 0.4523206 -.0264661
 0.4724628 -.0261606
 0.4926062 -.0257972
 0.5127506 -.0253747
 0.5328960 -.0248943
 0.5530424 -.0243549
 0.5731888 -.0237545
 0.5933372 -.0230941
 0.6134868 -.0223717
 0.6336375 -.0215893
 0.6537892 -.0207460
 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
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

SIKORSKY SC1094R8 AIRFOILPreviewDetails
BELL/WORTMANN FX 69-H-098 AIRFOILPreviewDetails
PW106PreviewDetails
BOEING 707 .40 SPAN AIRFOILPreviewDetails
PW75PreviewDetails
ONERA OA209 AIRFOILPreviewDetails
EH 2.0/10PreviewDetails
EH 1.5/9.0PreviewDetails
EH 2.5/10PreviewDetails
BOEING VERTOL V(1.95)3009-1.25PreviewDetails

Polars for SIKORSKY SC1094 R8 AIRFOIL (sc1094r8-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   sc1094r8-il50,000924.5 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   sc1094r8-il50,000527.1 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   sc1094r8-il100,000933.7 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sc1094r8-il100,000537.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   sc1094r8-il200,000945.6 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   sc1094r8-il200,000550.8 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   sc1094r8-il500,000967.8 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   sc1094r8-il500,000572.5 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   sc1094r8-il1,000,000988.3 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   sc1094r8-il1,000,000591.7 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit