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SC(2)-0714 Supercritical airfoil (coordinates from Raymer w/ one correction) (nasasc2-0714-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: SC(2)-0714 Supercritical airfoil (coordinates from Raymer w/ one correction) (nasasc2-0714-il)
Reynolds number: 500,000
Max Cl/Cd: 63.97 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-nasasc2-0714-il-500000-n5.txt
Download as CSV file: xf-nasasc2-0714-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SC(2)-0714 Supercritical airfoil (coordinates fr
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0210   0.10796   0.10407  -0.0505   1.0000   0.0237
 -19.500  -1.0451   0.09970   0.09566  -0.0550   1.0000   0.0239
 -19.250  -1.0647   0.09246   0.08828  -0.0589   1.0000   0.0240
 -19.000  -1.0805   0.08602   0.08170  -0.0624   1.0000   0.0241
 -18.750  -1.0933   0.08028   0.07584  -0.0654   1.0000   0.0243
 -18.500  -1.1035   0.07509   0.07051  -0.0680   1.0000   0.0244
 -18.250  -1.1113   0.07044   0.06575  -0.0703   1.0000   0.0246
 -18.000  -1.1172   0.06623   0.06142  -0.0722   1.0000   0.0248
 -17.750  -1.1212   0.06245   0.05753  -0.0737   1.0000   0.0250
 -17.500  -1.1236   0.05902   0.05399  -0.0750   1.0000   0.0252
 -17.250  -1.1249   0.05589   0.05076  -0.0759   1.0000   0.0254
 -17.000  -1.1250   0.05308   0.04784  -0.0766   1.0000   0.0256
 -16.750  -1.1238   0.05054   0.04519  -0.0770   1.0000   0.0259
 -16.500  -1.1220   0.04823   0.04278  -0.0770   1.0000   0.0261
 -16.250  -1.1219   0.04591   0.04040  -0.0769   1.0000   0.0263
 -16.000  -1.1214   0.04377   0.03821  -0.0765   1.0000   0.0266
 -15.750  -1.1195   0.04191   0.03630  -0.0759   1.0000   0.0269
 -15.500  -1.1173   0.04023   0.03457  -0.0750   1.0000   0.0271
 -15.250  -1.1149   0.03873   0.03303  -0.0738   1.0000   0.0274
 -15.000  -1.1128   0.03737   0.03162  -0.0723   1.0000   0.0277
 -14.750  -1.1111   0.03611   0.03031  -0.0705   1.0000   0.0280
 -14.500  -1.1095   0.03496   0.02911  -0.0685   1.0000   0.0283
 -14.250  -1.1088   0.03385   0.02795  -0.0662   1.0000   0.0287
 -14.000  -1.1071   0.03281   0.02687  -0.0639   0.9999   0.0290
 -13.750  -1.0891   0.03158   0.02556  -0.0648   0.9986   0.0295
 -13.500  -1.0707   0.03045   0.02435  -0.0656   0.9970   0.0300
 -13.250  -1.0511   0.02940   0.02323  -0.0664   0.9954   0.0304
 -13.000  -1.0318   0.02822   0.02200  -0.0675   0.9938   0.0310
 -12.750  -1.0122   0.02718   0.02095  -0.0683   0.9921   0.0316
 -12.500  -0.9949   0.02631   0.02004  -0.0684   0.9892   0.0323
 -12.250  -0.9749   0.02550   0.01920  -0.0688   0.9866   0.0330
 -12.000  -0.9523   0.02470   0.01836  -0.0696   0.9844   0.0337
 -11.750  -0.9265   0.02391   0.01752  -0.0709   0.9829   0.0345
 -11.500  -0.8992   0.02317   0.01672  -0.0725   0.9818   0.0352
 -11.250  -0.8767   0.02241   0.01592  -0.0731   0.9795   0.0359
 -11.000  -0.8560   0.02162   0.01514  -0.0734   0.9762   0.0367
 -10.750  -0.8296   0.02095   0.01445  -0.0746   0.9741   0.0377
 -10.500  -0.8010   0.02034   0.01382  -0.0760   0.9725   0.0387
 -10.250  -0.7715   0.01975   0.01321  -0.0776   0.9713   0.0398
 -10.000  -0.7410   0.01919   0.01260  -0.0794   0.9703   0.0408
  -9.750  -0.7098   0.01856   0.01194  -0.0813   0.9695   0.0418
  -9.500  -0.6779   0.01793   0.01133  -0.0834   0.9688   0.0432
  -9.250  -0.6453   0.01741   0.01081  -0.0855   0.9682   0.0447
  -9.000  -0.6220   0.01698   0.01036  -0.0855   0.9648   0.0459
  -8.750  -0.5936   0.01654   0.00990  -0.0865   0.9624   0.0471
  -8.500  -0.5620   0.01604   0.00939  -0.0882   0.9608   0.0486
  -8.250  -0.5293   0.01555   0.00892  -0.0902   0.9595   0.0506
  -8.000  -0.4962   0.01513   0.00851  -0.0921   0.9584   0.0528
  -7.750  -0.4628   0.01475   0.00811  -0.0939   0.9575   0.0548
  -7.500  -0.4286   0.01430   0.00769  -0.0960   0.9566   0.0575
  -7.250  -0.3942   0.01392   0.00733  -0.0981   0.9559   0.0609
  -7.000  -0.3594   0.01355   0.00698  -0.1002   0.9551   0.0649
  -6.750  -0.3241   0.01318   0.00665  -0.1024   0.9544   0.0706
  -6.500  -0.2886   0.01283   0.00634  -0.1045   0.9537   0.0769
  -6.000  -0.2283   0.01228   0.00588  -0.1065   0.9485   0.0930
  -5.750  -0.1952   0.01198   0.00564  -0.1081   0.9466   0.1027
  -5.500  -0.1613   0.01170   0.00540  -0.1098   0.9450   0.1130
  -5.250  -0.1265   0.01139   0.00517  -0.1117   0.9436   0.1266
  -5.000  -0.0903   0.01102   0.00492  -0.1140   0.9424   0.1499
  -4.750  -0.0530   0.01060   0.00466  -0.1167   0.9414   0.1846
  -4.500  -0.0141   0.01011   0.00438  -0.1198   0.9405   0.2327
  -4.250   0.0289   0.00942   0.00402  -0.1241   0.9399   0.3130
  -4.000   0.0747   0.00863   0.00363  -0.1292   0.9395   0.4176
  -3.750   0.1173   0.00808   0.00354  -0.1331   0.9389   0.5266
  -3.500   0.1491   0.00806   0.00360  -0.1339   0.9365   0.5658
  -3.250   0.1779   0.00807   0.00365  -0.1339   0.9324   0.5798
  -3.000   0.2088   0.00805   0.00365  -0.1344   0.9286   0.5888
  -2.750   0.2418   0.00797   0.00355  -0.1352   0.9247   0.5982
  -2.500   0.2716   0.00797   0.00359  -0.1353   0.9193   0.6079
  -2.250   0.3010   0.00798   0.00359  -0.1352   0.9118   0.6184
  -2.000   0.3311   0.00798   0.00359  -0.1352   0.9026   0.6264
  -1.750   0.3615   0.00790   0.00344  -0.1353   0.8854   0.6320
  -1.500   0.3906   0.00783   0.00331  -0.1351   0.8619   0.6341
  -1.250   0.4195   0.00784   0.00324  -0.1349   0.8338   0.6362
  -1.000   0.4478   0.00794   0.00322  -0.1346   0.8027   0.6388
  -0.750   0.4742   0.00816   0.00321  -0.1338   0.7459   0.6410
  -0.500   0.4955   0.00874   0.00332  -0.1322   0.6485   0.6430
  -0.250   0.5159   0.00946   0.00354  -0.1306   0.5457   0.6451
   0.000   0.5375   0.01019   0.00379  -0.1295   0.4429   0.6470
   0.250   0.5614   0.01079   0.00400  -0.1288   0.3607   0.6485
   0.500   0.5862   0.01134   0.00419  -0.1283   0.2888   0.6499
   1.000   0.6374   0.01213   0.00459  -0.1274   0.1977   0.6525
   1.250   0.6633   0.01251   0.00480  -0.1270   0.1623   0.6538
   1.500   0.6897   0.01283   0.00500  -0.1267   0.1382   0.6549
   1.750   0.7165   0.01312   0.00520  -0.1264   0.1204   0.6562
   2.000   0.7434   0.01340   0.00539  -0.1262   0.1067   0.6575
   2.250   0.7704   0.01365   0.00559  -0.1260   0.0958   0.6588
   2.500   0.7974   0.01391   0.00580  -0.1257   0.0861   0.6604
   2.750   0.8243   0.01418   0.00602  -0.1254   0.0782   0.6622
   3.000   0.8510   0.01446   0.00625  -0.1252   0.0719   0.6641
   3.250   0.8780   0.01472   0.00648  -0.1249   0.0678   0.6658
   3.500   0.9047   0.01501   0.00672  -0.1246   0.0640   0.6673
   3.750   0.9310   0.01528   0.00699  -0.1242   0.0614   0.6685
   4.000   0.9572   0.01553   0.00727  -0.1238   0.0592   0.6697
   4.250   0.9829   0.01583   0.00756  -0.1233   0.0568   0.6708
   4.500   1.0081   0.01618   0.00790  -0.1227   0.0545   0.6720
   4.750   1.0337   0.01648   0.00822  -0.1222   0.0529   0.6734
   5.000   1.0592   0.01677   0.00855  -0.1216   0.0513   0.6749
   5.250   1.0844   0.01710   0.00889  -0.1210   0.0497   0.6764
   5.500   1.1092   0.01746   0.00924  -0.1204   0.0480   0.6779
   5.750   1.1334   0.01787   0.00965  -0.1196   0.0464   0.6794
   6.000   1.1584   0.01817   0.00999  -0.1190   0.0450   0.6808
   6.250   1.1830   0.01851   0.01035  -0.1183   0.0435   0.6823
   6.500   1.2072   0.01887   0.01073  -0.1176   0.0422   0.6838
   6.750   1.2308   0.01928   0.01113  -0.1168   0.0410   0.6851
   7.000   1.2536   0.01972   0.01159  -0.1157   0.0399   0.6864
   7.250   1.2765   0.02011   0.01204  -0.1147   0.0389   0.6876
   7.500   1.2991   0.02051   0.01249  -0.1137   0.0378   0.6889
   7.750   1.3213   0.02092   0.01293  -0.1126   0.0367   0.6903
   8.000   1.3428   0.02137   0.01340  -0.1114   0.0357   0.6917
   8.250   1.3629   0.02192   0.01396  -0.1100   0.0348   0.6932
   8.500   1.3831   0.02241   0.01451  -0.1086   0.0341   0.6948
   8.750   1.4025   0.02291   0.01507  -0.1070   0.0334   0.6964
   9.000   1.4207   0.02343   0.01565  -0.1052   0.0328   0.6981
   9.250   1.4367   0.02396   0.01623  -0.1031   0.0321   0.6998
   9.500   1.4536   0.02453   0.01684  -0.1011   0.0315   0.7015
   9.750   1.4706   0.02515   0.01749  -0.0993   0.0309   0.7032
  10.000   1.4867   0.02584   0.01822  -0.0973   0.0303   0.7047
  10.250   1.5011   0.02665   0.01909  -0.0952   0.0297   0.7063
  10.500   1.5173   0.02733   0.01987  -0.0933   0.0293   0.7079
  10.750   1.5328   0.02806   0.02069  -0.0914   0.0288   0.7096
  11.000   1.5475   0.02885   0.02156  -0.0894   0.0284   0.7113
  11.250   1.5615   0.02969   0.02247  -0.0874   0.0279   0.7131
  11.500   1.5749   0.03057   0.02344  -0.0853   0.0275   0.7149
  11.750   1.5878   0.03150   0.02443  -0.0833   0.0271   0.7167
  12.000   1.5999   0.03249   0.02549  -0.0812   0.0268   0.7185
  12.250   1.6109   0.03356   0.02662  -0.0791   0.0264   0.7201
  12.500   1.6207   0.03473   0.02787  -0.0770   0.0261   0.7217
  12.750   1.6287   0.03604   0.02927  -0.0747   0.0258   0.7232
  13.000   1.6344   0.03757   0.03088  -0.0723   0.0255   0.7249
  13.250   1.6411   0.03906   0.03248  -0.0701   0.0253   0.7267
  13.500   1.6480   0.04057   0.03411  -0.0681   0.0251   0.7287
  13.750   1.6538   0.04221   0.03587  -0.0661   0.0249   0.7307
  14.000   1.6585   0.04399   0.03778  -0.0643   0.0247   0.7326
  14.250   1.6622   0.04593   0.03984  -0.0625   0.0245   0.7345
  14.500   1.6645   0.04805   0.04207  -0.0609   0.0243   0.7363
  14.750   1.6656   0.05036   0.04451  -0.0594   0.0240   0.7378
  15.000   1.6656   0.05286   0.04714  -0.0581   0.0239   0.7393
  15.250   1.6642   0.05561   0.05003  -0.0570   0.0237   0.7408
  15.500   1.6614   0.05867   0.05323  -0.0563   0.0235   0.7425
  15.750   1.6577   0.06200   0.05670  -0.0559   0.0233   0.7442
  16.000   1.6528   0.06570   0.06053  -0.0559   0.0232   0.7460
  16.250   1.6463   0.06983   0.06480  -0.0564   0.0230   0.7477
  16.500   1.6383   0.07441   0.06953  -0.0575   0.0229   0.7494
  16.750   1.6277   0.07962   0.07489  -0.0591   0.0228   0.7509
  17.000   1.6154   0.08538   0.08080  -0.0614   0.0226   0.7522
  17.250   1.5998   0.09200   0.08758  -0.0644   0.0225   0.7534
  17.500   1.5818   0.09931   0.09506  -0.0681   0.0224   0.7545
  17.750   1.5605   0.10741   0.10333  -0.0725   0.0224   0.7554
  18.000   1.5357   0.11642   0.11252  -0.0778   0.0223   0.7561
  18.250   1.5085   0.12615   0.12244  -0.0837   0.0223   0.7567
  18.500   1.4793   0.13653   0.13299  -0.0904   0.0222   0.7573
  18.750   1.4478   0.14771   0.14436  -0.0980   0.0221   0.7577
  19.000   1.4141   0.15991   0.15674  -0.1067   0.0220   0.7581
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