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NASA SC(2)-0714 AIRFOIL (sc20714-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NASA SC(2)-0714 AIRFOIL (sc20714-il)
Reynolds number: 1,000,000
Max Cl/Cd: 81.19 at α=-0.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sc20714-il-1000000.txt
Download as CSV file: xf-sc20714-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0714 AIRFOIL                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1686   0.08321   0.07959  -0.0638   1.0000   0.0235
 -19.500  -1.1791   0.07802   0.07429  -0.0664   1.0000   0.0236
 -19.250  -1.1874   0.07324   0.06939  -0.0688   1.0000   0.0237
 -19.000  -1.1933   0.06892   0.06497  -0.0709   1.0000   0.0239
 -18.750  -1.1977   0.06495   0.06090  -0.0727   1.0000   0.0240
 -18.500  -1.1999   0.06137   0.05722  -0.0742   1.0000   0.0241
 -18.250  -1.2001   0.05816   0.05391  -0.0755   1.0000   0.0242
 -18.000  -1.1988   0.05527   0.05093  -0.0765   1.0000   0.0243
 -17.750  -1.2060   0.05161   0.04718  -0.0774   1.0000   0.0246
 -17.500  -1.2099   0.04849   0.04398  -0.0780   1.0000   0.0249
 -17.250  -1.2096   0.04596   0.04140  -0.0782   1.0000   0.0252
 -17.000  -1.2071   0.04378   0.03918  -0.0782   1.0000   0.0254
 -16.750  -1.2039   0.04183   0.03718  -0.0780   1.0000   0.0257
 -16.500  -1.1998   0.04011   0.03541  -0.0774   1.0000   0.0259
 -16.250  -1.1962   0.03848   0.03373  -0.0766   1.0000   0.0262
 -16.000  -1.1927   0.03701   0.03221  -0.0755   1.0000   0.0264
 -15.750  -1.1903   0.03564   0.03079  -0.0741   1.0000   0.0266
 -15.500  -1.1889   0.03439   0.02950  -0.0722   1.0000   0.0269
 -15.250  -1.1883   0.03322   0.02829  -0.0700   1.0000   0.0271
 -15.000  -1.1882   0.03214   0.02715  -0.0676   1.0000   0.0274
 -14.750  -1.1887   0.03112   0.02608  -0.0650   1.0000   0.0276
 -14.500  -1.1896   0.03018   0.02509  -0.0621   1.0000   0.0278
 -14.250  -1.1911   0.02929   0.02416  -0.0590   1.0000   0.0280
 -14.000  -1.1701   0.02832   0.02312  -0.0600   0.9990   0.0282
 -13.750  -1.1556   0.02668   0.02143  -0.0610   0.9972   0.0288
 -13.500  -1.1368   0.02550   0.02023  -0.0620   0.9956   0.0294
 -13.250  -1.1155   0.02457   0.01928  -0.0630   0.9942   0.0299
 -13.000  -1.0909   0.02376   0.01844  -0.0644   0.9931   0.0305
 -12.750  -1.0688   0.02299   0.01764  -0.0650   0.9910   0.0310
 -12.500  -1.0440   0.02225   0.01688  -0.0661   0.9888   0.0317
 -12.250  -1.0164   0.02160   0.01618  -0.0675   0.9871   0.0322
 -12.000  -0.9884   0.02085   0.01539  -0.0691   0.9856   0.0329
 -11.750  -0.9601   0.01985   0.01439  -0.0713   0.9843   0.0339
 -11.500  -0.9291   0.01919   0.01373  -0.0734   0.9834   0.0348
 -11.250  -0.8971   0.01863   0.01315  -0.0755   0.9827   0.0357
 -11.000  -0.8648   0.01811   0.01261  -0.0775   0.9822   0.0366
 -10.750  -0.8318   0.01768   0.01215  -0.0795   0.9816   0.0373
 -10.500  -0.7988   0.01683   0.01130  -0.0823   0.9811   0.0389
 -10.250  -0.7760   0.01634   0.01081  -0.0823   0.9776   0.0400
 -10.000  -0.7453   0.01591   0.01038  -0.0838   0.9759   0.0413
  -9.750  -0.7129   0.01552   0.00997  -0.0855   0.9747   0.0425
  -9.500  -0.6791   0.01488   0.00933  -0.0880   0.9737   0.0442
  -9.250  -0.6449   0.01442   0.00889  -0.0902   0.9729   0.0460
  -9.000  -0.6104   0.01405   0.00851  -0.0923   0.9723   0.0476
  -8.750  -0.5752   0.01367   0.00812  -0.0945   0.9718   0.0491
  -8.500  -0.5391   0.01319   0.00767  -0.0971   0.9713   0.0517
  -8.250  -0.5033   0.01286   0.00736  -0.0994   0.9709   0.0539
  -8.000  -0.4671   0.01252   0.00701  -0.1018   0.9706   0.0560
  -7.750  -0.4305   0.01211   0.00664  -0.1043   0.9702   0.0592
  -7.500  -0.3947   0.01182   0.00635  -0.1065   0.9697   0.0620
  -7.250  -0.3578   0.01144   0.00600  -0.1090   0.9693   0.0662
  -7.000  -0.3214   0.01114   0.00572  -0.1113   0.9688   0.0705
  -6.750  -0.2845   0.01079   0.00543  -0.1137   0.9682   0.0770
  -6.500  -0.2508   0.01051   0.00520  -0.1154   0.9669   0.0846
  -6.250  -0.2207   0.01029   0.00502  -0.1162   0.9644   0.0930
  -6.000  -0.1868   0.01000   0.00479  -0.1179   0.9627   0.1043
  -5.750  -0.1510   0.00964   0.00455  -0.1202   0.9615   0.1232
  -5.500  -0.1149   0.00930   0.00433  -0.1224   0.9603   0.1486
  -5.250  -0.0771   0.00888   0.00409  -0.1251   0.9594   0.1868
  -5.000  -0.0376   0.00839   0.00382  -0.1283   0.9587   0.2393
  -4.750   0.0065   0.00768   0.00348  -0.1329   0.9584   0.3330
  -4.500   0.0527   0.00690   0.00313  -0.1380   0.9583   0.4475
  -4.250   0.0935   0.00644   0.00300  -0.1413   0.9577   0.5398
  -4.000   0.1272   0.00635   0.00295  -0.1425   0.9560   0.5661
  -3.750   0.1598   0.00630   0.00290  -0.1432   0.9533   0.5815
  -3.500   0.1874   0.00624   0.00287  -0.1429   0.9475   0.5920
  -3.250   0.2175   0.00615   0.00276  -0.1430   0.9419   0.6017
  -3.000   0.2465   0.00610   0.00272  -0.1428   0.9357   0.6089
  -2.750   0.2750   0.00604   0.00264  -0.1426   0.9275   0.6136
  -2.500   0.3055   0.00603   0.00256  -0.1428   0.9216   0.6172
  -2.250   0.3335   0.00599   0.00257  -0.1425   0.9126   0.6224
  -2.000   0.3624   0.00604   0.00259  -0.1423   0.9030   0.6283
  -1.750   0.3915   0.00612   0.00264  -0.1422   0.8923   0.6338
  -1.500   0.4207   0.00611   0.00263  -0.1422   0.8812   0.6377
  -1.250   0.4495   0.00614   0.00264  -0.1420   0.8667   0.6403
  -1.000   0.4775   0.00625   0.00272  -0.1417   0.8486   0.6444
  -0.750   0.5056   0.00640   0.00280  -0.1414   0.8249   0.6486
  -0.500   0.5334   0.00657   0.00281  -0.1410   0.7892   0.6506
  -0.250   0.5582   0.00696   0.00288  -0.1401   0.7185   0.6519
   0.000   0.5788   0.00773   0.00307  -0.1385   0.5937   0.6532
   0.250   0.6005   0.00847   0.00330  -0.1374   0.4740   0.6553
   0.500   0.6239   0.00912   0.00355  -0.1365   0.3814   0.6572
   0.750   0.6476   0.00975   0.00381  -0.1357   0.2953   0.6589
   1.000   0.6727   0.01026   0.00403  -0.1352   0.2302   0.6604
   1.250   0.6985   0.01070   0.00423  -0.1348   0.1803   0.6616
   1.500   0.7252   0.01105   0.00442  -0.1345   0.1475   0.6627
   1.750   0.7525   0.01133   0.00459  -0.1343   0.1263   0.6639
   2.000   0.7798   0.01161   0.00476  -0.1341   0.1076   0.6651
   2.250   0.8071   0.01188   0.00495  -0.1339   0.0941   0.6663
   2.500   0.8347   0.01211   0.00512  -0.1338   0.0846   0.6675
   2.750   0.8621   0.01237   0.00532  -0.1336   0.0770   0.6687
   3.000   0.8893   0.01263   0.00552  -0.1333   0.0713   0.6697
   3.250   0.9168   0.01286   0.00573  -0.1332   0.0675   0.6706
   3.500   0.9442   0.01307   0.00592  -0.1330   0.0642   0.6717
   3.750   0.9709   0.01334   0.00617  -0.1326   0.0610   0.6733
   4.000   0.9984   0.01351   0.00636  -0.1324   0.0593   0.6746
   4.250   1.0252   0.01374   0.00658  -0.1321   0.0572   0.6758
   4.500   1.0514   0.01404   0.00686  -0.1317   0.0547   0.6770
   4.750   1.0778   0.01429   0.00712  -0.1313   0.0531   0.6782
   5.000   1.1044   0.01451   0.00736  -0.1309   0.0515   0.6794
   5.250   1.1306   0.01477   0.00762  -0.1304   0.0499   0.6806
   5.500   1.1556   0.01515   0.00797  -0.1298   0.0478   0.6819
   5.750   1.1815   0.01542   0.00826  -0.1293   0.0466   0.6833
   6.000   1.2074   0.01568   0.00854  -0.1287   0.0452   0.6848
   6.250   1.2327   0.01598   0.00883  -0.1282   0.0437   0.6861
   6.500   1.2561   0.01649   0.00932  -0.1272   0.0416   0.6874
   6.750   1.2818   0.01671   0.00957  -0.1267   0.0406   0.6884
   7.000   1.3068   0.01701   0.00988  -0.1260   0.0393   0.6893
   7.250   1.3312   0.01734   0.01021  -0.1253   0.0380   0.6904
   7.500   1.3533   0.01788   0.01074  -0.1242   0.0365   0.6924
   7.750   1.3775   0.01817   0.01109  -0.1234   0.0357   0.6940
   8.000   1.4012   0.01849   0.01145  -0.1225   0.0348   0.6955
   8.250   1.4243   0.01885   0.01183  -0.1215   0.0339   0.6969
   8.500   1.4466   0.01924   0.01224  -0.1204   0.0330   0.6984
   8.750   1.4667   0.01980   0.01281  -0.1189   0.0320   0.6998
   9.000   1.4869   0.02030   0.01335  -0.1174   0.0313   0.7014
   9.250   1.5081   0.02068   0.01377  -0.1160   0.0307   0.7031
   9.500   1.5283   0.02110   0.01423  -0.1145   0.0301   0.7048
   9.750   1.5477   0.02156   0.01472  -0.1129   0.0295   0.7064
  10.000   1.5661   0.02204   0.01523  -0.1111   0.0290   0.7078
  10.250   1.5805   0.02258   0.01579  -0.1086   0.0285   0.7089
  10.500   1.5942   0.02327   0.01652  -0.1061   0.0279   0.7106
  10.750   1.6060   0.02418   0.01749  -0.1033   0.0273   0.7128
  11.000   1.6227   0.02476   0.01814  -0.1014   0.0271   0.7147
  11.250   1.6383   0.02540   0.01885  -0.0993   0.0268   0.7164
  11.500   1.6534   0.02609   0.01962  -0.0972   0.0264   0.7181
  11.750   1.6676   0.02684   0.02043  -0.0950   0.0261   0.7199
  12.000   1.6813   0.02763   0.02128  -0.0929   0.0258   0.7218
  12.250   1.6944   0.02846   0.02217  -0.0907   0.0254   0.7236
  12.500   1.7070   0.02934   0.02311  -0.0884   0.0251   0.7255
  12.750   1.7183   0.03030   0.02412  -0.0861   0.0249   0.7273
  13.000   1.7286   0.03136   0.02524  -0.0838   0.0246   0.7287
  13.250   1.7370   0.03258   0.02652  -0.0814   0.0242   0.7311
  13.500   1.7408   0.03415   0.02817  -0.0785   0.0239   0.7332
  13.750   1.7397   0.03618   0.03032  -0.0753   0.0235   0.7349
  14.000   1.7486   0.03744   0.03168  -0.0732   0.0234   0.7368
  14.250   1.7563   0.03882   0.03314  -0.0712   0.0232   0.7388
  14.500   1.7627   0.04034   0.03477  -0.0692   0.0231   0.7408
  14.750   1.7678   0.04204   0.03656  -0.0672   0.0229   0.7428
  15.000   1.7714   0.04392   0.03854  -0.0653   0.0227   0.7446
  15.250   1.7735   0.04598   0.04070  -0.0635   0.0226   0.7462
  15.500   1.7747   0.04821   0.04304  -0.0618   0.0224   0.7476
  15.750   1.7743   0.05070   0.04564  -0.0604   0.0223   0.7499
  16.000   1.7734   0.05336   0.04842  -0.0592   0.0221   0.7519
  16.250   1.7707   0.05636   0.05154  -0.0583   0.0219   0.7537
  16.500   1.7672   0.05960   0.05489  -0.0577   0.0218   0.7556
  16.750   1.7617   0.06328   0.05869  -0.0575   0.0217   0.7575
  17.000   1.7551   0.06733   0.06286  -0.0578   0.0216   0.7593
  17.250   1.7466   0.07186   0.06751  -0.0585   0.0215   0.7611
  17.500   1.7358   0.07696   0.07274  -0.0598   0.0214   0.7626
  17.750   1.7224   0.08271   0.07862  -0.0618   0.0213   0.7639
  18.000   1.7070   0.08905   0.08510  -0.0644   0.0212   0.7649
  18.250   1.6882   0.09621   0.09241  -0.0677   0.0211   0.7660
  18.500   1.6675   0.10392   0.10028  -0.0717   0.0211   0.7673
  18.750   1.6434   0.11238   0.10890  -0.0763   0.0210   0.7683
  19.000   1.6181   0.12127   0.11795  -0.0814   0.0210   0.7691
  19.250   1.5917   0.13056   0.12740  -0.0871   0.0210   0.7699
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