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DSMA-523A AIRFOIL (dsma523a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: DSMA-523A AIRFOIL (dsma523a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.31 at α=-0.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-dsma523a-il-1000000.txt
Download as CSV file: xf-dsma523a-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DSMA-523A 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
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -1.0825   0.10607   0.10340  -0.0327   1.0000   0.0204
 -17.750  -1.1336   0.09218   0.08927  -0.0409   1.0000   0.0203
 -17.500  -1.1647   0.08261   0.07952  -0.0465   1.0000   0.0203
 -17.250  -1.1877   0.07483   0.07157  -0.0509   1.0000   0.0203
 -17.000  -1.2052   0.06838   0.06497  -0.0543   1.0000   0.0203
 -16.750  -1.2181   0.06298   0.05944  -0.0569   1.0000   0.0204
 -16.500  -1.2274   0.05842   0.05475  -0.0588   1.0000   0.0205
 -16.250  -1.2348   0.05441   0.05062  -0.0602   1.0000   0.0205
 -16.000  -1.2403   0.05090   0.04699  -0.0611   1.0000   0.0206
 -15.750  -1.2434   0.04790   0.04389  -0.0615   1.0000   0.0207
 -15.500  -1.2455   0.04520   0.04108  -0.0615   1.0000   0.0209
 -15.250  -1.2466   0.04279   0.03857  -0.0612   1.0000   0.0210
 -15.000  -1.2460   0.04068   0.03637  -0.0607   1.0000   0.0211
 -14.750  -1.2444   0.03875   0.03434  -0.0600   1.0000   0.0212
 -14.500  -1.2419   0.03698   0.03249  -0.0591   1.0000   0.0213
 -14.250  -1.2379   0.03540   0.03083  -0.0581   1.0000   0.0214
 -14.000  -1.2336   0.03394   0.02929  -0.0569   1.0000   0.0215
 -13.750  -1.2270   0.03272   0.02799  -0.0556   1.0000   0.0217
 -13.500  -1.2209   0.03157   0.02678  -0.0542   1.0000   0.0217
 -13.250  -1.2235   0.02982   0.02493  -0.0519   1.0000   0.0220
 -13.000  -1.2271   0.02834   0.02339  -0.0491   1.0000   0.0222
 -12.750  -1.2316   0.02729   0.02229  -0.0455   1.0000   0.0225
 -12.500  -1.2322   0.02630   0.02127  -0.0425   1.0000   0.0226
 -12.250  -1.2239   0.02540   0.02034  -0.0408   1.0000   0.0229
 -12.000  -1.2120   0.02453   0.01943  -0.0397   1.0000   0.0231
 -11.750  -1.1907   0.02369   0.01856  -0.0402   0.9996   0.0235
 -11.500  -1.1638   0.02285   0.01767  -0.0417   0.9986   0.0238
 -11.250  -1.1367   0.02203   0.01680  -0.0431   0.9977   0.0242
 -11.000  -1.1088   0.02126   0.01598  -0.0446   0.9967   0.0245
 -10.750  -1.0796   0.02057   0.01523  -0.0461   0.9959   0.0249
 -10.500  -1.0491   0.01995   0.01456  -0.0478   0.9951   0.0253
 -10.250  -1.0179   0.01942   0.01398  -0.0495   0.9945   0.0255
 -10.000  -0.9875   0.01827   0.01280  -0.0519   0.9940   0.0263
  -9.750  -0.9583   0.01760   0.01212  -0.0533   0.9931   0.0269
  -9.500  -0.9301   0.01705   0.01155  -0.0543   0.9921   0.0275
  -9.250  -0.9005   0.01655   0.01103  -0.0555   0.9912   0.0281
  -9.000  -0.8703   0.01609   0.01054  -0.0568   0.9904   0.0288
  -8.750  -0.8397   0.01570   0.01011  -0.0580   0.9897   0.0294
  -8.500  -0.8081   0.01512   0.00951  -0.0596   0.9891   0.0302
  -8.250  -0.7760   0.01464   0.00904  -0.0612   0.9886   0.0313
  -8.000  -0.7435   0.01430   0.00869  -0.0626   0.9880   0.0324
  -7.750  -0.7109   0.01399   0.00836  -0.0640   0.9875   0.0335
  -7.500  -0.6782   0.01363   0.00800  -0.0656   0.9871   0.0348
  -7.250  -0.6457   0.01335   0.00776  -0.0669   0.9868   0.0364
  -7.000  -0.6132   0.01315   0.00756  -0.0682   0.9864   0.0380
  -6.750  -0.5805   0.01295   0.00738  -0.0695   0.9861   0.0399
  -6.500  -0.5482   0.01287   0.00734  -0.0706   0.9858   0.0419
  -6.250  -0.5156   0.01277   0.00724  -0.0718   0.9855   0.0440
  -6.000  -0.4831   0.01274   0.00725  -0.0729   0.9852   0.0460
  -5.750  -0.4576   0.01263   0.00715  -0.0725   0.9831   0.0481
  -5.500  -0.4267   0.01248   0.00701  -0.0733   0.9820   0.0500
  -5.250  -0.3957   0.01239   0.00695  -0.0740   0.9812   0.0520
  -5.000  -0.3648   0.01237   0.00693  -0.0747   0.9804   0.0542
  -4.750  -0.3311   0.01209   0.00666  -0.0763   0.9801   0.0564
  -4.500  -0.2978   0.01188   0.00649  -0.0777   0.9797   0.0584
  -4.250  -0.2645   0.01175   0.00636  -0.0790   0.9793   0.0602
  -4.000  -0.2297   0.01151   0.00614  -0.0807   0.9789   0.0620
  -3.750  -0.1940   0.01124   0.00589  -0.0827   0.9787   0.0641
  -3.500  -0.1596   0.01107   0.00574  -0.0842   0.9784   0.0656
  -3.250  -0.1255   0.01095   0.00563  -0.0857   0.9781   0.0669
  -3.000  -0.0906   0.01082   0.00553  -0.0873   0.9778   0.0685
  -2.750  -0.0548   0.01059   0.00533  -0.0889   0.9751   0.0703
  -2.500  -0.0028   0.01010   0.00489  -0.0938   0.9715   0.0731
  -2.250   0.0425   0.00969   0.00454  -0.0972   0.9677   0.0778
  -2.000   0.0915   0.00914   0.00418  -0.1016   0.9657   0.1124
  -1.750   0.1467   0.00852   0.00373  -0.1073   0.9644   0.1470
  -1.500   0.1512   0.00821   0.00352  -0.1022   0.9472   0.1698
  -1.250   0.1889   0.00753   0.00306  -0.1042   0.9364   0.2281
  -1.000   0.2521   0.00637   0.00229  -0.1120   0.9288   0.3426
  -0.750   0.3445   0.00490   0.00160  -0.1269   0.9083   0.6153
  -0.500   0.3535   0.00618   0.00180  -0.1222   0.6352   0.6287
  -0.250   0.3700   0.00734   0.00214  -0.1199   0.4266   0.6413
   0.000   0.3926   0.00813   0.00248  -0.1186   0.3125   0.6548
   0.250   0.4150   0.00885   0.00291  -0.1171   0.2298   0.6627
   0.500   0.4390   0.00949   0.00323  -0.1161   0.1501   0.6678
   0.750   0.4649   0.00999   0.00347  -0.1156   0.0976   0.6709
   1.000   0.4924   0.01027   0.00365  -0.1153   0.0837   0.6731
   1.250   0.5189   0.01048   0.00386  -0.1147   0.0768   0.6755
   1.500   0.5453   0.01074   0.00410  -0.1141   0.0706   0.6773
   1.750   0.5723   0.01096   0.00430  -0.1136   0.0660   0.6790
   2.000   0.5992   0.01122   0.00453  -0.1131   0.0613   0.6807
   2.250   0.6267   0.01141   0.00471  -0.1128   0.0587   0.6824
   2.500   0.6540   0.01165   0.00490  -0.1124   0.0556   0.6841
   2.750   0.6810   0.01192   0.00516  -0.1120   0.0529   0.6859
   3.000   0.7081   0.01216   0.00540  -0.1116   0.0512   0.6881
   3.250   0.7352   0.01242   0.00564  -0.1111   0.0494   0.6901
   3.500   0.7616   0.01262   0.00584  -0.1106   0.0474   0.6928
   3.750   0.7877   0.01294   0.00617  -0.1100   0.0457   0.6939
   4.000   0.8149   0.01312   0.00637  -0.1097   0.0447   0.6949
   4.250   0.8412   0.01337   0.00663  -0.1091   0.0435   0.6964
   4.500   0.8678   0.01360   0.00685  -0.1086   0.0422   0.6978
   4.750   0.8946   0.01389   0.00711  -0.1083   0.0405   0.6985
   5.000   0.9213   0.01420   0.00744  -0.1079   0.0392   0.6991
   5.250   0.9488   0.01438   0.00763  -0.1077   0.0384   0.6997
   5.500   0.9760   0.01460   0.00785  -0.1074   0.0374   0.7003
   5.750   1.0031   0.01483   0.00808  -0.1072   0.0364   0.7009
   6.000   1.0299   0.01510   0.00834  -0.1068   0.0354   0.7015
   6.250   1.0542   0.01573   0.00897  -0.1060   0.0341   0.7022
   6.500   1.0809   0.01596   0.00923  -0.1057   0.0336   0.7030
   6.750   1.1074   0.01623   0.00952  -0.1053   0.0330   0.7037
   7.000   1.1338   0.01651   0.00983  -0.1048   0.0323   0.7042
   7.250   1.1599   0.01681   0.01014  -0.1044   0.0316   0.7047
   7.500   1.1858   0.01712   0.01046  -0.1039   0.0310   0.7052
   7.750   1.2112   0.01748   0.01082  -0.1033   0.0303   0.7057
   8.000   1.2350   0.01806   0.01141  -0.1025   0.0296   0.7061
   8.250   1.2578   0.01879   0.01220  -0.1015   0.0290   0.7066
   8.500   1.2829   0.01914   0.01259  -0.1008   0.0287   0.7069
   8.750   1.3075   0.01953   0.01303  -0.1001   0.0283   0.7073
   9.000   1.3317   0.01997   0.01352  -0.0993   0.0278   0.7076
   9.250   1.3564   0.02036   0.01395  -0.0987   0.0274   0.7084
   9.500   1.3806   0.02077   0.01439  -0.0980   0.0269   0.7093
   9.750   1.4042   0.02120   0.01486  -0.0972   0.0265   0.7100
  10.000   1.4271   0.02165   0.01536  -0.0963   0.0261   0.7107
  10.250   1.4492   0.02219   0.01593  -0.0952   0.0258   0.7115
  10.500   1.4698   0.02287   0.01665  -0.0939   0.0254   0.7122
  10.750   1.4853   0.02426   0.01815  -0.0918   0.0248   0.7128
  11.000   1.5059   0.02487   0.01885  -0.0905   0.0246   0.7133
  11.250   1.5270   0.02536   0.01941  -0.0893   0.0243   0.7139
  11.500   1.5475   0.02588   0.02000  -0.0880   0.0241   0.7145
  11.750   1.5665   0.02653   0.02074  -0.0865   0.0238   0.7151
  12.000   1.5843   0.02726   0.02156  -0.0848   0.0235   0.7157
  12.250   1.6017   0.02795   0.02233  -0.0831   0.0232   0.7163
  12.500   1.6179   0.02870   0.02316  -0.0812   0.0230   0.7169
  12.750   1.6325   0.02953   0.02407  -0.0791   0.0228   0.7175
  13.000   1.6452   0.03032   0.02494  -0.0767   0.0226   0.7181
  13.250   1.6536   0.03109   0.02578  -0.0735   0.0224   0.7187
  13.500   1.6616   0.03210   0.02688  -0.0704   0.0223   0.7193
  13.750   1.6699   0.03306   0.02792  -0.0676   0.0221   0.7199
  14.000   1.6773   0.03410   0.02904  -0.0647   0.0219   0.7205
  14.250   1.6816   0.03540   0.03043  -0.0616   0.0218   0.7211
  14.500   1.6851   0.03677   0.03189  -0.0585   0.0217   0.7217
  14.750   1.6871   0.03829   0.03350  -0.0555   0.0215   0.7222
  15.000   1.6856   0.04016   0.03550  -0.0524   0.0214   0.7226
  15.250   1.6801   0.04247   0.03794  -0.0494   0.0213   0.7231
  15.500   1.6714   0.04521   0.04082  -0.0466   0.0212   0.7236
  15.750   1.6592   0.04851   0.04428  -0.0444   0.0211   0.7240
  16.000   1.6402   0.05287   0.04883  -0.0429   0.0210   0.7244
  16.250   1.6170   0.05834   0.05451  -0.0429   0.0209   0.7247
  16.500   1.5944   0.06466   0.06103  -0.0448   0.0209   0.7249
  16.750   1.5670   0.07289   0.06948  -0.0492   0.0209   0.7250
  17.000   1.5407   0.08234   0.07913  -0.0555   0.0209   0.7251
  17.250   1.5091   0.09370   0.09070  -0.0635   0.0210   0.7252
  17.500   1.4557   0.10980   0.10704  -0.0743   0.0211   0.7251
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