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NASA SC(2)-0710 AIRFOIL (sc20710-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0710 AIRFOIL (sc20710-il)
Reynolds number: 1,000,000
Max Cl/Cd: 79.1 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20710-il-1000000-n5.txt
Download as CSV file: xf-sc20710-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0710 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
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -1.0358   0.09589   0.09331  -0.0376   1.0000   0.0104
 -17.750  -1.0994   0.07908   0.07624  -0.0473   1.0000   0.0102
 -17.500  -1.1354   0.06780   0.06475  -0.0544   1.0000   0.0102
 -17.250  -1.1585   0.05960   0.05637  -0.0598   1.0000   0.0102
 -17.000  -1.1749   0.05330   0.04992  -0.0637   1.0000   0.0102
 -16.750  -1.1869   0.04836   0.04484  -0.0664   1.0000   0.0102
 -16.500  -1.1951   0.04434   0.04070  -0.0681   1.0000   0.0103
 -16.250  -1.2006   0.04098   0.03723  -0.0692   1.0000   0.0104
 -16.000  -1.2035   0.03818   0.03432  -0.0696   1.0000   0.0104
 -15.750  -1.2045   0.03582   0.03187  -0.0696   1.0000   0.0105
 -15.500  -1.2046   0.03379   0.02976  -0.0690   1.0000   0.0106
 -15.250  -1.2041   0.03202   0.02791  -0.0680   1.0000   0.0107
 -15.000  -1.2044   0.03048   0.02629  -0.0663   1.0000   0.0108
 -14.750  -1.2081   0.02916   0.02490  -0.0637   1.0000   0.0109
 -14.500  -1.2142   0.02796   0.02364  -0.0603   1.0000   0.0109
 -14.250  -1.2091   0.02672   0.02232  -0.0589   1.0000   0.0110
 -14.000  -1.1905   0.02538   0.02089  -0.0600   0.9993   0.0111
 -13.750  -1.1654   0.02411   0.01952  -0.0621   0.9983   0.0113
 -13.500  -1.1391   0.02293   0.01826  -0.0643   0.9973   0.0114
 -13.250  -1.1116   0.02186   0.01709  -0.0664   0.9964   0.0116
 -13.000  -1.0833   0.02088   0.01601  -0.0684   0.9956   0.0118
 -12.750  -1.0545   0.01999   0.01504  -0.0702   0.9949   0.0119
 -12.500  -1.0252   0.01918   0.01415  -0.0720   0.9943   0.0121
 -12.250  -0.9963   0.01843   0.01332  -0.0735   0.9936   0.0123
 -12.000  -0.9684   0.01775   0.01257  -0.0746   0.9925   0.0124
 -11.750  -0.9395   0.01712   0.01187  -0.0759   0.9913   0.0126
 -11.500  -0.9102   0.01649   0.01119  -0.0772   0.9903   0.0127
 -11.250  -0.8803   0.01574   0.01037  -0.0787   0.9894   0.0131
 -11.000  -0.8500   0.01514   0.00973  -0.0801   0.9885   0.0135
 -10.750  -0.8193   0.01462   0.00919  -0.0815   0.9877   0.0139
 -10.500  -0.7882   0.01415   0.00869  -0.0829   0.9870   0.0143
 -10.250  -0.7569   0.01372   0.00822  -0.0843   0.9864   0.0148
 -10.000  -0.7252   0.01329   0.00776  -0.0857   0.9858   0.0152
  -9.750  -0.6932   0.01289   0.00732  -0.0871   0.9853   0.0156
  -9.500  -0.6611   0.01250   0.00690  -0.0886   0.9849   0.0161
  -9.250  -0.6286   0.01208   0.00647  -0.0901   0.9845   0.0170
  -9.000  -0.5961   0.01173   0.00612  -0.0916   0.9841   0.0180
  -8.750  -0.5633   0.01141   0.00578  -0.0931   0.9837   0.0191
  -8.500  -0.5333   0.01111   0.00547  -0.0940   0.9824   0.0204
  -8.250  -0.5034   0.01082   0.00520  -0.0948   0.9807   0.0222
  -8.000  -0.4722   0.01057   0.00494  -0.0958   0.9794   0.0238
  -7.750  -0.4402   0.01029   0.00468  -0.0971   0.9783   0.0259
  -7.500  -0.4078   0.01005   0.00444  -0.0984   0.9774   0.0280
  -7.250  -0.3753   0.00983   0.00422  -0.0997   0.9765   0.0297
  -7.000  -0.3423   0.00957   0.00398  -0.1011   0.9757   0.0322
  -6.750  -0.3096   0.00935   0.00377  -0.1024   0.9748   0.0343
  -6.500  -0.2769   0.00915   0.00357  -0.1037   0.9740   0.0359
  -6.250  -0.2440   0.00893   0.00337  -0.1050   0.9733   0.0390
  -6.000  -0.2112   0.00873   0.00319  -0.1063   0.9726   0.0422
  -5.750  -0.1782   0.00852   0.00302  -0.1076   0.9720   0.0478
  -5.500  -0.1463   0.00833   0.00287  -0.1087   0.9708   0.0544
  -5.250  -0.1158   0.00815   0.00274  -0.1095   0.9687   0.0615
  -5.000  -0.0843   0.00797   0.00261  -0.1104   0.9670   0.0711
  -4.750  -0.0524   0.00779   0.00248  -0.1115   0.9654   0.0821
  -4.500  -0.0200   0.00759   0.00236  -0.1126   0.9640   0.0991
  -4.250   0.0124   0.00740   0.00224  -0.1138   0.9627   0.1158
  -4.000   0.0461   0.00714   0.00212  -0.1154   0.9615   0.1514
  -3.750   0.0806   0.00684   0.00199  -0.1171   0.9601   0.1963
  -3.500   0.1161   0.00651   0.00185  -0.1191   0.9582   0.2527
  -3.250   0.1490   0.00615   0.00174  -0.1205   0.9532   0.3228
  -3.000   0.1851   0.00566   0.00159  -0.1228   0.9487   0.4237
  -2.750   0.2214   0.00522   0.00146  -0.1249   0.9414   0.5258
  -2.500   0.2521   0.00509   0.00140  -0.1254   0.9270   0.5663
  -2.250   0.2818   0.00504   0.00140  -0.1256   0.9132   0.5948
  -2.000   0.3109   0.00505   0.00140  -0.1256   0.8965   0.6164
  -1.750   0.3388   0.00512   0.00139  -0.1254   0.8683   0.6261
  -1.500   0.3650   0.00533   0.00137  -0.1247   0.8098   0.6309
  -1.250   0.3816   0.00658   0.00161  -0.1223   0.5725   0.6342
  -1.000   0.4051   0.00737   0.00182  -0.1215   0.4238   0.6387
  -0.750   0.4307   0.00793   0.00198  -0.1212   0.3208   0.6455
  -0.500   0.4575   0.00832   0.00213  -0.1210   0.2531   0.6521
  -0.250   0.4847   0.00867   0.00228  -0.1209   0.1984   0.6588
   0.000   0.5121   0.00897   0.00241  -0.1208   0.1554   0.6645
   0.250   0.5395   0.00925   0.00257  -0.1207   0.1202   0.6690
   0.500   0.5672   0.00950   0.00270  -0.1206   0.0960   0.6717
   0.750   0.5952   0.00970   0.00283  -0.1206   0.0806   0.6739
   1.000   0.6232   0.00990   0.00296  -0.1206   0.0688   0.6761
   1.500   0.6790   0.01026   0.00326  -0.1204   0.0533   0.6806
   1.750   0.7068   0.01046   0.00342  -0.1203   0.0468   0.6828
   2.000   0.7345   0.01066   0.00359  -0.1202   0.0420   0.6849
   2.250   0.7622   0.01085   0.00377  -0.1201   0.0385   0.6871
   2.500   0.7899   0.01105   0.00395  -0.1200   0.0360   0.6896
   2.750   0.8173   0.01127   0.00415  -0.1198   0.0334   0.6920
   3.000   0.8449   0.01147   0.00435  -0.1197   0.0318   0.6941
   3.250   0.8724   0.01167   0.00456  -0.1195   0.0302   0.6960
   3.500   0.8996   0.01190   0.00478  -0.1193   0.0283   0.6980
   3.750   0.9266   0.01215   0.00504  -0.1191   0.0264   0.7001
   4.000   0.9538   0.01236   0.00527  -0.1188   0.0250   0.7022
   4.250   0.9807   0.01261   0.00551  -0.1186   0.0230   0.7044
   4.500   1.0074   0.01289   0.00578  -0.1183   0.0213   0.7066
   4.750   1.0341   0.01315   0.00605  -0.1180   0.0197   0.7087
   5.000   1.0605   0.01346   0.00634  -0.1176   0.0182   0.7107
   5.250   1.0867   0.01376   0.00668  -0.1172   0.0173   0.7128
   5.500   1.1129   0.01407   0.00702  -0.1168   0.0166   0.7150
   5.750   1.1389   0.01440   0.00737  -0.1164   0.0158   0.7174
   6.000   1.1646   0.01476   0.00774  -0.1159   0.0152   0.7199
   6.250   1.1900   0.01516   0.00816  -0.1153   0.0146   0.7222
   6.500   1.2152   0.01559   0.00862  -0.1148   0.0141   0.7243
   6.750   1.2405   0.01597   0.00904  -0.1142   0.0139   0.7261
   7.000   1.2655   0.01637   0.00950  -0.1136   0.0136   0.7280
   7.250   1.2903   0.01679   0.00998  -0.1130   0.0134   0.7300
   7.500   1.3148   0.01724   0.01048  -0.1123   0.0131   0.7320
   7.750   1.3390   0.01770   0.01099  -0.1115   0.0129   0.7341
   8.000   1.3630   0.01818   0.01152  -0.1108   0.0126   0.7363
   8.250   1.3867   0.01867   0.01207  -0.1100   0.0124   0.7384
   8.500   1.4102   0.01919   0.01262  -0.1092   0.0121   0.7404
   8.750   1.4331   0.01975   0.01323  -0.1083   0.0118   0.7422
   9.000   1.4553   0.02039   0.01393  -0.1072   0.0116   0.7441
   9.250   1.4763   0.02114   0.01478  -0.1060   0.0113   0.7460
   9.500   1.4966   0.02196   0.01568  -0.1047   0.0111   0.7481
   9.750   1.5179   0.02259   0.01640  -0.1035   0.0111   0.7504
  10.000   1.5386   0.02325   0.01715  -0.1023   0.0110   0.7527
  10.250   1.5586   0.02396   0.01795  -0.1009   0.0109   0.7548
  10.500   1.5780   0.02471   0.01880  -0.0995   0.0108   0.7569
  10.750   1.5966   0.02549   0.01967  -0.0980   0.0107   0.7588
  11.000   1.6142   0.02632   0.02061  -0.0963   0.0106   0.7609
  11.250   1.6308   0.02719   0.02160  -0.0945   0.0105   0.7631
  11.500   1.6463   0.02811   0.02263  -0.0925   0.0104   0.7653
  11.750   1.6604   0.02909   0.02372  -0.0903   0.0103   0.7676
  12.000   1.6730   0.03009   0.02484  -0.0879   0.0101   0.7699
  12.250   1.6828   0.03116   0.02602  -0.0851   0.0101   0.7720
  12.500   1.6892   0.03224   0.02722  -0.0817   0.0100   0.7739
  12.750   1.6930   0.03338   0.02848  -0.0780   0.0099   0.7758
  13.000   1.6968   0.03470   0.02992  -0.0746   0.0098   0.7777
  13.250   1.7000   0.03611   0.03146  -0.0713   0.0098   0.7797
  13.500   1.7014   0.03770   0.03319  -0.0680   0.0097   0.7818
  13.750   1.7023   0.03941   0.03503  -0.0650   0.0096   0.7840
  14.000   1.7014   0.04134   0.03708  -0.0620   0.0096   0.7862
  14.250   1.7001   0.04339   0.03926  -0.0594   0.0095   0.7882
  14.750   1.6913   0.04845   0.04459  -0.0549   0.0094   0.7917
  15.000   1.6840   0.05153   0.04781  -0.0533   0.0093   0.7935
  15.250   1.6735   0.05525   0.05169  -0.0523   0.0093   0.7952
  15.500   1.6582   0.06002   0.05662  -0.0523   0.0092   0.7969
  15.750   1.6384   0.06607   0.06286  -0.0538   0.0092   0.7985
  16.000   1.6108   0.07464   0.07164  -0.0581   0.0092   0.7999
  16.250   1.5592   0.09045   0.08777  -0.0689   0.0093   0.8004
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