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SM701 (sm701-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: SM701 (sm701-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.6 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sm701-il-1000000-n5.txt
Download as CSV file: xf-sm701-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SM701                                           
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.7432   0.08807   0.08554  -0.0777   0.9978   0.0094
 -16.750  -0.7846   0.07536   0.07259  -0.0864   0.9971   0.0094
 -16.500  -0.8004   0.06767   0.06474  -0.0922   0.9963   0.0094
 -16.250  -0.8071   0.06185   0.05880  -0.0970   0.9954   0.0095
 -16.000  -0.8171   0.05592   0.05271  -0.1017   0.9945   0.0095
 -15.750  -0.8194   0.05136   0.04802  -0.1056   0.9936   0.0096
 -15.500  -0.8213   0.04782   0.04438  -0.1077   0.9923   0.0096
 -15.250  -0.8212   0.04457   0.04101  -0.1097   0.9908   0.0097
 -15.000  -0.8202   0.04136   0.03769  -0.1119   0.9892   0.0098
 -14.750  -0.8052   0.03960   0.03587  -0.1138   0.9879   0.0100
 -14.500  -0.7940   0.03737   0.03355  -0.1158   0.9866   0.0101
 -14.250  -0.7862   0.03466   0.03071  -0.1182   0.9853   0.0102
 -14.000  -0.7734   0.03245   0.02839  -0.1203   0.9842   0.0102
 -13.750  -0.7556   0.03089   0.02674  -0.1222   0.9834   0.0104
 -13.500  -0.7448   0.02933   0.02510  -0.1227   0.9813   0.0105
 -13.250  -0.7347   0.02779   0.02347  -0.1229   0.9784   0.0106
 -13.000  -0.7178   0.02643   0.02202  -0.1240   0.9762   0.0107
 -12.750  -0.6971   0.02518   0.02070  -0.1255   0.9746   0.0107
 -12.500  -0.6725   0.02411   0.01955  -0.1274   0.9732   0.0109
 -12.250  -0.6515   0.02244   0.01779  -0.1295   0.9718   0.0110
 -12.000  -0.6378   0.02130   0.01659  -0.1294   0.9677   0.0112
 -11.750  -0.6219   0.02033   0.01558  -0.1292   0.9630   0.0113
 -11.500  -0.6000   0.01940   0.01459  -0.1300   0.9596   0.0114
 -11.250  -0.5793   0.01866   0.01381  -0.1303   0.9555   0.0116
 -11.000  -0.5678   0.01800   0.01310  -0.1287   0.9472   0.0117
 -10.750  -0.5509   0.01733   0.01238  -0.1280   0.9399   0.0118
 -10.500  -0.5354   0.01673   0.01172  -0.1269   0.9293   0.0120
 -10.250  -0.5156   0.01624   0.01118  -0.1263   0.9166   0.0123
 -10.000  -0.4932   0.01567   0.01053  -0.1261   0.9019   0.0124
  -9.750  -0.4712   0.01519   0.00993  -0.1257   0.8852   0.0127
  -9.250  -0.4310   0.01438   0.00890  -0.1240   0.8548   0.0130
  -9.000  -0.4106   0.01400   0.00843  -0.1231   0.8427   0.0132
  -8.750  -0.3895   0.01366   0.00801  -0.1223   0.8321   0.0133
  -8.500  -0.3680   0.01332   0.00759  -0.1215   0.8220   0.0135
  -8.250  -0.3453   0.01301   0.00721  -0.1209   0.8137   0.0136
  -8.000  -0.3222   0.01273   0.00686  -0.1204   0.8060   0.0138
  -7.750  -0.2999   0.01230   0.00638  -0.1198   0.7994   0.0141
  -7.500  -0.2766   0.01192   0.00595  -0.1193   0.7928   0.0144
  -7.250  -0.2525   0.01162   0.00561  -0.1189   0.7867   0.0147
  -7.000  -0.2272   0.01135   0.00532  -0.1187   0.7811   0.0150
  -6.750  -0.2017   0.01111   0.00504  -0.1185   0.7752   0.0154
  -6.500  -0.1761   0.01090   0.00479  -0.1183   0.7702   0.0158
  -6.250  -0.1496   0.01067   0.00454  -0.1183   0.7658   0.0163
  -6.000  -0.1230   0.01046   0.00429  -0.1182   0.7612   0.0166
  -5.750  -0.0965   0.01027   0.00406  -0.1181   0.7565   0.0169
  -5.500  -0.0695   0.01009   0.00385  -0.1181   0.7525   0.0172
  -5.250  -0.0424   0.00984   0.00359  -0.1182   0.7483   0.0179
  -5.000  -0.0151   0.00965   0.00338  -0.1182   0.7442   0.0186
  -4.750   0.0123   0.00950   0.00320  -0.1183   0.7400   0.0193
  -4.500   0.0399   0.00936   0.00304  -0.1184   0.7356   0.0202
  -4.250   0.0678   0.00922   0.00289  -0.1185   0.7303   0.0211
  -4.000   0.0951   0.00908   0.00273  -0.1185   0.7239   0.0235
  -3.750   0.1227   0.00893   0.00258  -0.1185   0.7178   0.0286
  -3.500   0.1501   0.00870   0.00243  -0.1187   0.7107   0.0512
  -3.250   0.1773   0.00850   0.00229  -0.1188   0.7038   0.0757
  -3.000   0.2055   0.00826   0.00216  -0.1191   0.6976   0.1095
  -2.750   0.2335   0.00802   0.00204  -0.1194   0.6916   0.1513
  -2.500   0.2617   0.00770   0.00190  -0.1198   0.6863   0.2151
  -2.250   0.2908   0.00716   0.00172  -0.1207   0.6806   0.3265
  -2.000   0.3198   0.00666   0.00158  -0.1215   0.6743   0.4486
  -1.750   0.3487   0.00657   0.00157  -0.1218   0.6685   0.4885
  -1.500   0.3776   0.00652   0.00158  -0.1221   0.6618   0.5204
  -1.250   0.4057   0.00653   0.00161  -0.1222   0.6548   0.5456
  -1.000   0.4345   0.00654   0.00165  -0.1223   0.6473   0.5652
  -0.750   0.4622   0.00660   0.00167  -0.1223   0.6382   0.5736
  -0.500   0.4903   0.00664   0.00168  -0.1223   0.6278   0.5763
  -0.250   0.5178   0.00670   0.00169  -0.1223   0.6160   0.5788
   0.000   0.5444   0.00680   0.00171  -0.1220   0.5995   0.5813
   0.250   0.5702   0.00693   0.00174  -0.1216   0.5782   0.5839
   0.500   0.5946   0.00713   0.00180  -0.1209   0.5502   0.5860
   0.750   0.6187   0.00735   0.00189  -0.1203   0.5224   0.5885
   1.000   0.6424   0.00760   0.00201  -0.1195   0.4937   0.5909
   1.250   0.6666   0.00783   0.00213  -0.1189   0.4667   0.5935
   1.500   0.6910   0.00806   0.00225  -0.1183   0.4450   0.5963
   1.750   0.7156   0.00828   0.00237  -0.1177   0.4235   0.5992
   2.000   0.7398   0.00851   0.00250  -0.1171   0.4019   0.6019
   2.250   0.7642   0.00873   0.00263  -0.1165   0.3830   0.6043
   2.500   0.7889   0.00891   0.00276  -0.1160   0.3675   0.6071
   2.750   0.8132   0.00912   0.00290  -0.1154   0.3515   0.6100
   3.000   0.8371   0.00934   0.00304  -0.1147   0.3351   0.6130
   3.250   0.8615   0.00953   0.00319  -0.1142   0.3229   0.6162
   3.500   0.8855   0.00973   0.00333  -0.1135   0.3116   0.6193
   4.000   0.9323   0.01012   0.00365  -0.1120   0.2877   0.6260
   4.250   0.9547   0.01031   0.00380  -0.1111   0.2780   0.6295
   4.500   0.9766   0.01051   0.00397  -0.1100   0.2681   0.6331
   4.750   0.9987   0.01070   0.00414  -0.1090   0.2593   0.6363
   5.000   1.0201   0.01094   0.00434  -0.1080   0.2496   0.6398
   5.250   1.0427   0.01114   0.00453  -0.1071   0.2419   0.6438
   5.500   1.0641   0.01139   0.00476  -0.1060   0.2342   0.6481
   5.750   1.0863   0.01161   0.00497  -0.1051   0.2267   0.6525
   6.000   1.1072   0.01188   0.00522  -0.1040   0.2185   0.6568
   6.250   1.1295   0.01210   0.00544  -0.1031   0.2126   0.6615
   6.500   1.1502   0.01238   0.00571  -0.1020   0.2059   0.6662
   6.750   1.1716   0.01263   0.00596  -0.1010   0.1999   0.6707
   7.000   1.1924   0.01291   0.00624  -0.0999   0.1934   0.6754
   7.250   1.2130   0.01320   0.00654  -0.0988   0.1879   0.6807
   7.500   1.2341   0.01346   0.00682  -0.0978   0.1836   0.6861
   7.750   1.2540   0.01378   0.00714  -0.0966   0.1780   0.6912
   8.000   1.2739   0.01411   0.00747  -0.0955   0.1726   0.6975
   8.250   1.2943   0.01441   0.00780  -0.0945   0.1684   0.7040
   8.500   1.3135   0.01476   0.00817  -0.0933   0.1638   0.7105
   8.750   1.3322   0.01514   0.00857  -0.0920   0.1590   0.7176
   9.000   1.3521   0.01548   0.00894  -0.0909   0.1551   0.7241
   9.250   1.3706   0.01587   0.00936  -0.0897   0.1507   0.7314
   9.500   1.3881   0.01633   0.00983  -0.0883   0.1460   0.7389
   9.750   1.4070   0.01672   0.01026  -0.0872   0.1427   0.7467
  10.000   1.4249   0.01716   0.01074  -0.0860   0.1388   0.7553
  10.250   1.4418   0.01767   0.01128  -0.0846   0.1346   0.7647
  10.500   1.4585   0.01819   0.01184  -0.0833   0.1302   0.7745
  10.750   1.4752   0.01872   0.01240  -0.0820   0.1256   0.7857
  11.000   1.4898   0.01937   0.01308  -0.0805   0.1201   0.7968
  11.250   1.5057   0.01996   0.01372  -0.0792   0.1161   0.8087
  11.500   1.5206   0.02062   0.01441  -0.0778   0.1112   0.8223
  11.750   1.5334   0.02141   0.01523  -0.0762   0.1055   0.8378
  12.000   1.5470   0.02212   0.01601  -0.0747   0.1004   0.8569
  12.250   1.5579   0.02294   0.01689  -0.0729   0.0954   0.8862
  12.500   1.5649   0.02356   0.01766  -0.0702   0.0917   1.0000
  12.750   1.5776   0.02450   0.01861  -0.0689   0.0869   1.0000
  13.000   1.5887   0.02558   0.01968  -0.0676   0.0820   1.0000
  13.250   1.6015   0.02656   0.02069  -0.0664   0.0784   1.0000
  13.500   1.6114   0.02778   0.02190  -0.0651   0.0734   1.0000
  13.750   1.6217   0.02899   0.02312  -0.0639   0.0690   1.0000
  14.000   1.6314   0.03028   0.02443  -0.0627   0.0649   1.0000
  14.250   1.6399   0.03170   0.02585  -0.0615   0.0608   1.0000
  14.500   1.6482   0.03318   0.02734  -0.0604   0.0563   1.0000
  14.750   1.6531   0.03497   0.02912  -0.0592   0.0509   1.0000
  15.000   1.6570   0.03691   0.03107  -0.0580   0.0456   1.0000
  15.250   1.6625   0.03876   0.03294  -0.0570   0.0415   1.0000
  15.500   1.6643   0.04101   0.03520  -0.0559   0.0368   1.0000
  15.750   1.6663   0.04330   0.03750  -0.0551   0.0327   1.0000
  16.000   1.6681   0.04570   0.03994  -0.0543   0.0292   1.0000
  16.250   1.6685   0.04833   0.04259  -0.0537   0.0262   1.0000
  16.500   1.6703   0.05088   0.04520  -0.0532   0.0237   1.0000
  16.750   1.6686   0.05389   0.04825  -0.0529   0.0210   1.0000
  17.000   1.6672   0.05697   0.05139  -0.0527   0.0186   1.0000
  17.250   1.6655   0.06020   0.05469  -0.0527   0.0169   1.0000
  17.500   1.6603   0.06400   0.05854  -0.0529   0.0146   1.0000
  17.750   1.6560   0.06778   0.06240  -0.0534   0.0128   1.0000
  18.000   1.6482   0.07218   0.06688  -0.0541   0.0108   1.0000
  18.250   1.6388   0.07698   0.07176  -0.0552   0.0090   1.0000
  18.750   1.6178   0.08737   0.08234  -0.0582   0.0065   1.0000
  19.000   1.6054   0.09308   0.08817  -0.0602   0.0058   1.0000
  19.250   1.5939   0.09880   0.09400  -0.0623   0.0053   1.0000
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