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SIKORSKY SC1095 AIRFOIL (sc1095-il)

SIKORSKY SC1095 AIRFOIL - Sikorsky/Balch SC1095 rotorcraft airfoil


Airfoil sc1095-il
Details Dat file Parser  
(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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Lednicer format dat file
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Polars for SIKORSKY SC1095 AIRFOIL (sc1095-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   sc1095-il50,000925.3 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   sc1095-il50,000526.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   sc1095-il100,000934.2 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   sc1095-il100,000536.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   sc1095-il200,000945.3 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   sc1095-il200,000548.8 at α=10°Mach=0 Ncrit=5Xfoil predictionDetails
   sc1095-il500,000969.5 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   sc1095-il500,000570.2 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   sc1095-il1,000,000987 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   sc1095-il1,000,000585.6 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
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