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SIKORSKY SSC-A07 AIRFOIL (ssca07-il)

SIKORSKY SSC-A07 AIRFOIL - Sikorsky/Flemming SSC-A07 transonic rotorcraft airfoil


Airfoil ssca07-il
Details Dat file Parser  
(ssca07-il) SIKORSKY SSC-A07 AIRFOIL
Sikorsky/Flemming SSC-A07 transonic rotorcraft airfoil
Max thickness 7% at 37.7% chord.
Max camber 0.9% at 17.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 SIKORSKY SSC-A07 AIRFOIL
       66.       66.

 0.0000000 0.0000000
 0.0001990 0.0015559
 0.0007980 0.0030688
 0.0019940 0.0050413
 0.0029910 0.0062445
 0.0044866 0.0076755
 0.0069791 0.0096378
 0.0099701 0.0116049
 0.0159522 0.0148367
 0.0219343 0.0174998
 0.0279164 0.0197906
 0.0338985 0.0218084
 0.0398806 0.0236202
 0.0458627 0.0252728
 0.0518448 0.0267935
 0.0578269 0.0281934
 0.0677969 0.0302580
 0.0777671 0.0320003
 0.0877373 0.0334570
 0.0977075 0.0346758
 0.1126626 0.0361700
 0.1276179 0.0373755
 0.1425731 0.0383797
 0.1575294 0.0392341
 0.1724845 0.0399660
 0.1874397 0.0405879
 0.2023950 0.0411130
 0.2173502 0.0415546
 0.2323054 0.0419307
 0.2472606 0.0422506
 0.2771711 0.0427453
 0.3070815 0.0430644
 0.3369920 0.0432166
 0.3768725 0.0431619
 0.4167542 0.0428085
 0.4366944 0.0425159
 0.4566347 0.0421414
 0.4765750 0.0416849
 0.4965153 0.0411434
 0.5164557 0.0405169
 0.5363959 0.0398037
 0.5563362 0.0390047
 0.5762765 0.0381183
 0.5962168 0.0371430
 0.6161571 0.0360740
 0.6360974 0.0349029
 0.6560386 0.0336154
 0.6759790 0.0321930
 0.6959193 0.0306192
 0.7158596 0.0288870
 0.7357998 0.0270034
 0.7557402 0.0249966
 0.7756805 0.0229016
 0.7956207 0.0207520
 0.8155611 0.0185664
 0.8355014 0.0163427
 0.8554416 0.0140690
 0.8753819 0.0117391
 0.8953232 0.0093733
 0.9152635 0.0070356
 0.9352039 0.0048447
 0.9551441 0.0029939
 0.9750844 0.0017798
 0.9850546 0.0015457
 0.9950247 0.0016604
 1.0000000 0.0018727

 0.0000000 0.0000000
 0.0001990 -.0011306
 0.0007980 -.0022315
 0.0019940 -.0035565
 0.0029910 -.0042361
 0.0044866 -.0050124
 0.0069791 -.0059909
 0.0099701 -.0069046
 0.0159522 -.0083254
 0.0219343 -.0094693
 0.0279164 -.0104587
 0.0338985 -.0113458
 0.0398806 -.0121573
 0.0458627 -.0129064
 0.0518448 -.0136008
 0.0578269 -.0142445
 0.0677969 -.0152199
 0.0777671 -.0160930
 0.0877373 -.0168826
 0.0977075 -.0176075
 0.1126626 -.0185968
 0.1276179 -.0194941
 0.1425731 -.0203189
 0.1575294 -.0210812
 0.1724845 -.0217881
 0.1874397 -.0224412
 0.2023950 -.0230444
 0.2173502 -.0235968
 0.2323054 -.0241016
 0.2472606 -.0245612
 0.2771711 -.0253508
 0.3070815 -.0259789
 0.3369920 -.0264502
 0.3768725 -.0268380
 0.4167542 -.0269403
 0.4366944 -.0268786
 0.4566347 -.0267366
 0.4765750 -.0265119
 0.4965153 -.0261982
 0.5164557 -.0257948
 0.5363959 -.0253024
 0.5563362 -.0247259
 0.5762765 -.0240712
 0.5962168 -.0233471
 0.6161571 -.0225575
 0.6360974 -.0217031
 0.6560386 -.0207824
 0.6759790 -.0197930
 0.6959193 -.0187350
 0.7158596 -.0176106
 0.7357998 -.0164277
 0.7557402 -.0151980
 0.7756805 -.0139363
 0.7956207 -.0126559
 0.8155611 -.0113685
 0.8355014 -.0100779
 0.8554416 -.0087803
 0.8753819 -.0074648
 0.8953232 -.0061157
 0.9152635 -.0047300
 0.9352039 -.0033364
 0.9551441 -.0020302
 0.9750844 -.0010307
 0.9850546 -.0007717
 0.9950247 -.0006711
 1.0000000 -.0006242
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Polars for SIKORSKY SSC-A07 AIRFOIL (ssca07-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ssca07-il50,000929.7 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   ssca07-il50,000528.3 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ssca07-il100,000939.4 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ssca07-il100,000537.8 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   ssca07-il200,000950.5 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ssca07-il200,000548.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ssca07-il500,000964.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ssca07-il500,000561.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ssca07-il1,000,000976 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ssca07-il1,000,000574.2 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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