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NASA SC(2)-0712 AIRFOIL (sc20712-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0712 AIRFOIL (sc20712-il)
Reynolds number: 1,000,000
Max Cl/Cd: 80.21 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20712-il-1000000-n5.txt
Download as CSV file: xf-sc20712-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0712 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1395   0.09761   0.09444  -0.0430   1.0000   0.0141
 -19.500  -1.1797   0.08649   0.08314  -0.0492   1.0000   0.0141
 -19.250  -1.2093   0.07749   0.07397  -0.0543   1.0000   0.0141
 -19.000  -1.2303   0.07016   0.06649  -0.0585   1.0000   0.0142
 -18.750  -1.2445   0.06421   0.06041  -0.0618   1.0000   0.0142
 -18.500  -1.2581   0.05861   0.05467  -0.0649   1.0000   0.0143
 -18.250  -1.2683   0.05384   0.04979  -0.0673   1.0000   0.0144
 -18.000  -1.2744   0.04985   0.04570  -0.0691   1.0000   0.0145
 -17.750  -1.2781   0.04638   0.04212  -0.0704   1.0000   0.0146
 -17.500  -1.2790   0.04342   0.03908  -0.0714   1.0000   0.0147
 -17.250  -1.2780   0.04085   0.03643  -0.0720   1.0000   0.0149
 -17.000  -1.2756   0.03857   0.03407  -0.0724   1.0000   0.0150
 -16.750  -1.2718   0.03652   0.03195  -0.0725   1.0000   0.0152
 -16.500  -1.2667   0.03468   0.03004  -0.0725   1.0000   0.0153
 -16.250  -1.2608   0.03302   0.02832  -0.0722   1.0000   0.0155
 -16.000  -1.2547   0.03151   0.02675  -0.0716   1.0000   0.0156
 -15.750  -1.2489   0.03013   0.02531  -0.0707   1.0000   0.0158
 -15.500  -1.2438   0.02886   0.02398  -0.0695   1.0000   0.0160
 -15.250  -1.2396   0.02770   0.02278  -0.0678   1.0000   0.0162
 -15.000  -1.2379   0.02667   0.02168  -0.0655   1.0000   0.0163
 -14.750  -1.2423   0.02574   0.02071  -0.0619   1.0000   0.0164
 -14.500  -1.2387   0.02479   0.01971  -0.0597   0.9995   0.0166
 -14.250  -1.2143   0.02374   0.01860  -0.0613   0.9982   0.0168
 -14.000  -1.1889   0.02277   0.01757  -0.0630   0.9968   0.0171
 -13.750  -1.1622   0.02187   0.01660  -0.0648   0.9956   0.0173
 -13.500  -1.1350   0.02086   0.01556  -0.0669   0.9945   0.0178
 -13.250  -1.1062   0.02003   0.01469  -0.0689   0.9937   0.0182
 -13.000  -1.0780   0.01928   0.01392  -0.0706   0.9925   0.0187
 -12.750  -1.0501   0.01860   0.01320  -0.0721   0.9909   0.0192
 -12.500  -1.0209   0.01796   0.01252  -0.0737   0.9894   0.0197
 -12.250  -0.9908   0.01737   0.01189  -0.0754   0.9882   0.0202
 -12.000  -0.9601   0.01683   0.01131  -0.0771   0.9871   0.0207
 -11.750  -0.9289   0.01620   0.01066  -0.0790   0.9861   0.0214
 -11.500  -0.8972   0.01566   0.01011  -0.0808   0.9853   0.0221
 -11.250  -0.8650   0.01517   0.00961  -0.0827   0.9846   0.0228
 -11.000  -0.8327   0.01473   0.00914  -0.0844   0.9840   0.0236
 -10.750  -0.8003   0.01432   0.00870  -0.0861   0.9834   0.0242
 -10.500  -0.7676   0.01389   0.00825  -0.0878   0.9829   0.0249
 -10.250  -0.7348   0.01346   0.00781  -0.0896   0.9825   0.0259
 -10.000  -0.7033   0.01308   0.00744  -0.0910   0.9814   0.0269
  -9.750  -0.6741   0.01275   0.00709  -0.0918   0.9791   0.0278
  -9.500  -0.6431   0.01244   0.00675  -0.0930   0.9774   0.0287
  -9.250  -0.6112   0.01208   0.00640  -0.0943   0.9759   0.0299
  -9.000  -0.5790   0.01174   0.00607  -0.0958   0.9747   0.0313
  -8.750  -0.5466   0.01144   0.00577  -0.0972   0.9734   0.0326
  -8.500  -0.5140   0.01117   0.00548  -0.0986   0.9722   0.0337
  -8.250  -0.4811   0.01086   0.00519  -0.1001   0.9711   0.0356
  -8.000  -0.4479   0.01058   0.00493  -0.1016   0.9699   0.0378
  -7.750  -0.4162   0.01034   0.00469  -0.1027   0.9681   0.0397
  -7.500  -0.3858   0.01009   0.00447  -0.1035   0.9653   0.0427
  -7.250  -0.3547   0.00988   0.00427  -0.1045   0.9627   0.0454
  -7.000  -0.3228   0.00964   0.00406  -0.1056   0.9604   0.0485
  -6.750  -0.2905   0.00943   0.00385  -0.1068   0.9584   0.0516
  -6.500  -0.2581   0.00923   0.00366  -0.1079   0.9565   0.0547
  -6.250  -0.2258   0.00902   0.00348  -0.1091   0.9547   0.0587
  -6.000  -0.1951   0.00885   0.00333  -0.1099   0.9517   0.0622
  -5.750  -0.1637   0.00865   0.00318  -0.1108   0.9486   0.0679
  -5.500  -0.1320   0.00847   0.00303  -0.1118   0.9457   0.0745
  -5.250  -0.1000   0.00829   0.00288  -0.1129   0.9431   0.0826
  -5.000  -0.0677   0.00810   0.00274  -0.1140   0.9407   0.0932
  -4.750  -0.0358   0.00792   0.00262  -0.1150   0.9379   0.1057
  -4.500  -0.0036   0.00770   0.00250  -0.1162   0.9348   0.1271
  -4.250   0.0293   0.00745   0.00237  -0.1175   0.9315   0.1584
  -4.000   0.0637   0.00710   0.00222  -0.1192   0.9283   0.2078
  -3.750   0.0983   0.00677   0.00208  -0.1210   0.9248   0.2640
  -3.500   0.1319   0.00648   0.00197  -0.1226   0.9196   0.3139
  -3.250   0.1657   0.00618   0.00185  -0.1241   0.9129   0.3703
  -3.000   0.2003   0.00583   0.00170  -0.1258   0.9023   0.4428
  -2.750   0.2337   0.00556   0.00162  -0.1271   0.8881   0.5150
  -2.500   0.2644   0.00550   0.00160  -0.1277   0.8726   0.5504
  -2.250   0.2945   0.00550   0.00162  -0.1280   0.8584   0.5767
  -2.000   0.3231   0.00557   0.00162  -0.1279   0.8314   0.5892
  -1.750   0.3508   0.00574   0.00162  -0.1276   0.7919   0.5998
  -1.500   0.3771   0.00604   0.00169  -0.1271   0.7247   0.6098
  -1.250   0.4009   0.00669   0.00183  -0.1261   0.6079   0.6158
  -1.000   0.4251   0.00740   0.00205  -0.1255   0.4845   0.6208
  -0.750   0.4509   0.00795   0.00224  -0.1252   0.3919   0.6259
  -0.500   0.4774   0.00842   0.00239  -0.1249   0.3159   0.6291
  -0.250   0.5036   0.00892   0.00255  -0.1247   0.2368   0.6321
   0.000   0.5309   0.00927   0.00270  -0.1246   0.1890   0.6359
   0.250   0.5587   0.00954   0.00285  -0.1245   0.1556   0.6397
   0.500   0.5866   0.00979   0.00299  -0.1245   0.1287   0.6424
   0.750   0.6148   0.00999   0.00312  -0.1245   0.1129   0.6442
   1.000   0.6429   0.01019   0.00324  -0.1245   0.0994   0.6461
   1.250   0.6710   0.01039   0.00338  -0.1244   0.0873   0.6479
   1.500   0.6991   0.01059   0.00352  -0.1244   0.0780   0.6498
   2.000   0.7552   0.01097   0.00383  -0.1242   0.0651   0.6539
   2.250   0.7831   0.01116   0.00400  -0.1242   0.0595   0.6560
   2.500   0.8108   0.01137   0.00417  -0.1240   0.0543   0.6579
   2.750   0.8386   0.01157   0.00436  -0.1239   0.0506   0.6598
   3.000   0.8662   0.01178   0.00455  -0.1237   0.0470   0.6618
   3.250   0.8937   0.01200   0.00474  -0.1236   0.0440   0.6638
   3.500   0.9211   0.01222   0.00495  -0.1234   0.0411   0.6656
   3.750   0.9483   0.01246   0.00517  -0.1231   0.0388   0.6673
   4.000   0.9756   0.01269   0.00538  -0.1229   0.0370   0.6688
   4.250   1.0026   0.01293   0.00562  -0.1227   0.0350   0.6708
   4.500   1.0294   0.01320   0.00589  -0.1223   0.0334   0.6728
   4.750   1.0563   0.01343   0.00614  -0.1221   0.0324   0.6747
   5.000   1.0830   0.01368   0.00641  -0.1217   0.0312   0.6767
   5.250   1.1094   0.01396   0.00669  -0.1213   0.0299   0.6788
   5.500   1.1354   0.01428   0.00700  -0.1209   0.0285   0.6808
   5.750   1.1617   0.01454   0.00729  -0.1205   0.0278   0.6829
   6.000   1.1878   0.01483   0.00759  -0.1201   0.0270   0.6848
   6.500   1.2392   0.01545   0.00824  -0.1190   0.0252   0.6891
   6.750   1.2642   0.01583   0.00863  -0.1184   0.0243   0.6915
   7.000   1.2896   0.01614   0.00899  -0.1179   0.0238   0.6940
   7.250   1.3146   0.01648   0.00935  -0.1172   0.0232   0.6965
   7.500   1.3394   0.01682   0.00973  -0.1166   0.0225   0.6992
   7.750   1.3639   0.01719   0.01011  -0.1159   0.0218   0.7016
   8.000   1.3881   0.01759   0.01051  -0.1151   0.0211   0.7037
   8.250   1.4115   0.01804   0.01099  -0.1143   0.0203   0.7060
   8.500   1.4354   0.01842   0.01142  -0.1135   0.0200   0.7082
   8.750   1.4588   0.01883   0.01188  -0.1126   0.0195   0.7104
   9.000   1.4818   0.01925   0.01235  -0.1116   0.0191   0.7127
   9.250   1.5044   0.01970   0.01283  -0.1106   0.0186   0.7151
   9.500   1.5266   0.02017   0.01334  -0.1096   0.0182   0.7174
   9.750   1.5482   0.02067   0.01386  -0.1084   0.0178   0.7195
  10.000   1.5690   0.02122   0.01444  -0.1071   0.0173   0.7214
  10.250   1.5889   0.02183   0.01511  -0.1057   0.0169   0.7236
  10.500   1.6091   0.02235   0.01570  -0.1043   0.0167   0.7259
  10.750   1.6285   0.02290   0.01632  -0.1028   0.0165   0.7283
  11.000   1.6470   0.02347   0.01696  -0.1012   0.0163   0.7307
  11.250   1.6643   0.02408   0.01763  -0.0993   0.0160   0.7332
  11.500   1.6806   0.02470   0.01831  -0.0973   0.0158   0.7357
  11.750   1.6956   0.02535   0.01902  -0.0951   0.0156   0.7380
  12.000   1.7074   0.02602   0.01976  -0.0923   0.0153   0.7403
  12.250   1.7194   0.02675   0.02057  -0.0897   0.0151   0.7427
  12.500   1.7316   0.02755   0.02144  -0.0872   0.0149   0.7451
  12.750   1.7431   0.02840   0.02237  -0.0847   0.0148   0.7474
  13.000   1.7537   0.02934   0.02338  -0.0821   0.0146   0.7498
  13.250   1.7634   0.03036   0.02447  -0.0796   0.0144   0.7523
  13.500   1.7714   0.03152   0.02571  -0.0769   0.0142   0.7547
  13.750   1.7769   0.03288   0.02716  -0.0741   0.0139   0.7569
  14.000   1.7844   0.03412   0.02850  -0.0716   0.0138   0.7592
  14.250   1.7919   0.03538   0.02987  -0.0693   0.0138   0.7616
  14.500   1.7983   0.03676   0.03135  -0.0670   0.0136   0.7640
  14.750   1.8033   0.03830   0.03299  -0.0647   0.0136   0.7664
  15.000   1.8067   0.04003   0.03482  -0.0625   0.0135   0.7687
  15.250   1.8092   0.04188   0.03678  -0.0604   0.0134   0.7709
  15.500   1.8104   0.04394   0.03896  -0.0584   0.0133   0.7729
  15.750   1.8099   0.04624   0.04138  -0.0567   0.0132   0.7751
  16.000   1.8082   0.04876   0.04403  -0.0551   0.0131   0.7772
  16.250   1.8045   0.05161   0.04700  -0.0538   0.0130   0.7793
  16.500   1.7990   0.05484   0.05037  -0.0529   0.0130   0.7814
  16.750   1.7915   0.05850   0.05416  -0.0524   0.0129   0.7834
  17.000   1.7820   0.06268   0.05848  -0.0525   0.0128   0.7853
  17.250   1.7694   0.06765   0.06360  -0.0534   0.0128   0.7871
  17.750   1.7313   0.08105   0.07734  -0.0586   0.0127   0.7899
  18.000   1.7009   0.09065   0.08715  -0.0636   0.0127   0.7909
  18.250   1.6548   0.10405   0.10080  -0.0716   0.0127   0.7913
  18.500   1.5745   0.12499   0.12208  -0.0844   0.0129   0.7902
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