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DSMA-523A AIRFOIL (dsma523a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: DSMA-523A AIRFOIL (dsma523a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 77.55 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-dsma523a-il-1000000-n5.txt
Download as CSV file: xf-dsma523a-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.9947   0.12346   0.12058  -0.0490   0.9849   0.0162
 -19.500  -1.0406   0.11093   0.10787  -0.0559   0.9852   0.0162
 -19.250  -1.0844   0.09929   0.09606  -0.0624   0.9854   0.0162
 -19.000  -1.1223   0.08893   0.08554  -0.0681   0.9857   0.0162
 -18.750  -1.1532   0.08009   0.07654  -0.0729   0.9860   0.0161
 -18.500  -1.1775   0.07257   0.06887  -0.0770   0.9864   0.0161
 -18.250  -1.1950   0.06637   0.06254  -0.0802   0.9867   0.0162
 -18.000  -1.2078   0.06118   0.05722  -0.0827   0.9871   0.0162
 -17.750  -1.2172   0.05676   0.05268  -0.0846   0.9874   0.0162
 -17.500  -1.2237   0.05295   0.04876  -0.0859   0.9877   0.0163
 -17.250  -1.2282   0.04963   0.04534  -0.0868   0.9880   0.0163
 -17.000  -1.2302   0.04678   0.04240  -0.0873   0.9883   0.0163
 -16.750  -1.2312   0.04424   0.03978  -0.0874   0.9885   0.0164
 -16.500  -1.2351   0.04172   0.03717  -0.0870   0.9887   0.0165
 -16.250  -1.2381   0.03953   0.03490  -0.0861   0.9889   0.0166
 -16.000  -1.2393   0.03761   0.03291  -0.0850   0.9891   0.0167
 -15.750  -1.2391   0.03590   0.03113  -0.0837   0.9892   0.0168
 -15.500  -1.2376   0.03435   0.02952  -0.0824   0.9894   0.0169
 -15.250  -1.2341   0.03297   0.02808  -0.0811   0.9895   0.0171
 -15.000  -1.2298   0.03167   0.02672  -0.0797   0.9896   0.0172
 -14.750  -1.2240   0.03050   0.02550  -0.0783   0.9897   0.0173
 -14.500  -1.2174   0.02940   0.02435  -0.0769   0.9898   0.0175
 -14.250  -1.2102   0.02836   0.02326  -0.0754   0.9898   0.0176
 -14.000  -1.2004   0.02740   0.02227  -0.0742   0.9897   0.0178
 -13.750  -1.1905   0.02647   0.02129  -0.0730   0.9895   0.0180
 -13.500  -1.1803   0.02558   0.02036  -0.0717   0.9893   0.0181
 -13.250  -1.1700   0.02479   0.01953  -0.0702   0.9891   0.0183
 -13.000  -1.1586   0.02402   0.01871  -0.0689   0.9887   0.0185
 -12.750  -1.1435   0.02329   0.01793  -0.0682   0.9880   0.0188
 -12.500  -1.1257   0.02257   0.01717  -0.0679   0.9873   0.0190
 -12.250  -1.1047   0.02185   0.01641  -0.0681   0.9868   0.0193
 -12.000  -1.0830   0.02118   0.01570  -0.0683   0.9864   0.0195
 -11.750  -1.0601   0.02052   0.01500  -0.0688   0.9861   0.0198
 -11.500  -1.0366   0.01979   0.01424  -0.0695   0.9857   0.0202
 -11.250  -1.0165   0.01916   0.01360  -0.0692   0.9851   0.0205
 -11.000  -0.9982   0.01859   0.01300  -0.0685   0.9841   0.0209
 -10.750  -0.9756   0.01803   0.01243  -0.0686   0.9833   0.0212
 -10.500  -0.9507   0.01751   0.01189  -0.0690   0.9825   0.0216
 -10.250  -0.9233   0.01700   0.01136  -0.0699   0.9818   0.0221
 -10.000  -0.8953   0.01652   0.01086  -0.0708   0.9812   0.0225
  -9.750  -0.8664   0.01607   0.01038  -0.0719   0.9807   0.0229
  -9.500  -0.8363   0.01564   0.00993  -0.0732   0.9803   0.0233
  -9.250  -0.8056   0.01516   0.00944  -0.0746   0.9798   0.0239
  -9.000  -0.7745   0.01472   0.00901  -0.0760   0.9795   0.0246
  -8.750  -0.7433   0.01433   0.00862  -0.0774   0.9791   0.0254
  -8.500  -0.7119   0.01398   0.00825  -0.0787   0.9789   0.0261
  -8.250  -0.6802   0.01365   0.00791  -0.0801   0.9786   0.0268
  -8.000  -0.6530   0.01334   0.00759  -0.0804   0.9776   0.0274
  -7.750  -0.6251   0.01300   0.00726  -0.0809   0.9764   0.0284
  -7.500  -0.5950   0.01269   0.00696  -0.0818   0.9757   0.0295
  -7.250  -0.5641   0.01242   0.00669  -0.0828   0.9751   0.0306
  -7.000  -0.5327   0.01216   0.00644  -0.0839   0.9747   0.0317
  -6.750  -0.5007   0.01190   0.00621  -0.0851   0.9742   0.0336
  -6.500  -0.4684   0.01167   0.00600  -0.0864   0.9739   0.0356
  -6.250  -0.4359   0.01147   0.00585  -0.0876   0.9735   0.0381
  -6.000  -0.4036   0.01129   0.00570  -0.0887   0.9732   0.0410
  -5.750  -0.3715   0.01115   0.00560  -0.0897   0.9729   0.0436
  -5.500  -0.3392   0.01102   0.00547  -0.0908   0.9726   0.0459
  -5.250  -0.3067   0.01088   0.00535  -0.0919   0.9724   0.0475
  -5.000  -0.2802   0.01077   0.00527  -0.0917   0.9706   0.0493
  -4.750  -0.2498   0.01067   0.00519  -0.0923   0.9696   0.0511
  -4.500  -0.2182   0.01058   0.00511  -0.0932   0.9690   0.0522
  -4.250  -0.1849   0.01036   0.00492  -0.0945   0.9686   0.0536
  -4.000  -0.1521   0.01020   0.00479  -0.0957   0.9682   0.0548
  -3.750  -0.1194   0.01006   0.00467  -0.0968   0.9679   0.0560
  -3.500  -0.0865   0.00992   0.00456  -0.0979   0.9676   0.0569
  -3.250  -0.0535   0.00980   0.00446  -0.0991   0.9673   0.0577
  -3.000  -0.0163   0.00964   0.00432  -0.1011   0.9670   0.0585
  -2.750  -0.0359   0.00955   0.00423  -0.0909   0.9442   0.0587
  -2.500   0.0024   0.00904   0.00375  -0.0929   0.9362   0.0601
  -2.250   0.0477   0.00854   0.00329  -0.0964   0.9322   0.0617
  -2.000   0.1103   0.00792   0.00268  -0.1035   0.9275   0.0628
  -1.750   0.1843   0.00760   0.00228  -0.1133   0.9130   0.0639
  -1.500   0.2039   0.00773   0.00217  -0.1112   0.8180   0.0646
  -1.250   0.2070   0.00940   0.00242  -0.1060   0.4730   0.0651
  -1.000   0.2318   0.00993   0.00249  -0.1055   0.3445   0.0664
  -0.750   0.2594   0.01020   0.00252  -0.1056   0.2722   0.0682
  -0.500   0.2877   0.01042   0.00254  -0.1057   0.2136   0.0710
  -0.250   0.3177   0.01057   0.00258  -0.1064   0.1577   0.1035
   0.000   0.3472   0.01073   0.00263  -0.1068   0.1131   0.1228
   0.250   0.4157   0.00915   0.00238  -0.1182   0.0845   0.6102
   0.500   0.4439   0.00934   0.00256  -0.1181   0.0756   0.6298
   0.750   0.4719   0.00952   0.00271  -0.1179   0.0699   0.6372
   1.000   0.5002   0.00969   0.00283  -0.1177   0.0646   0.6428
   1.250   0.5284   0.00984   0.00295  -0.1176   0.0609   0.6465
   1.500   0.5561   0.01004   0.00312  -0.1173   0.0566   0.6499
   1.750   0.5837   0.01024   0.00331  -0.1170   0.0537   0.6548
   2.000   0.6115   0.01044   0.00346  -0.1167   0.0507   0.6585
   2.250   0.6394   0.01064   0.00361  -0.1165   0.0479   0.6612
   2.500   0.6674   0.01081   0.00376  -0.1163   0.0462   0.6629
   2.750   0.6949   0.01099   0.00394  -0.1160   0.0443   0.6646
   3.000   0.7221   0.01121   0.00414  -0.1157   0.0425   0.6664
   3.250   0.7494   0.01143   0.00435  -0.1153   0.0410   0.6678
   3.500   0.7770   0.01161   0.00453  -0.1150   0.0400   0.6689
   3.750   0.8043   0.01181   0.00474  -0.1147   0.0389   0.6705
   4.000   0.8313   0.01204   0.00496  -0.1143   0.0378   0.6727
   4.250   0.8583   0.01229   0.00520  -0.1139   0.0366   0.6750
   4.500   0.8853   0.01255   0.00543  -0.1135   0.0352   0.6759
   4.750   0.9128   0.01274   0.00562  -0.1133   0.0345   0.6766
   5.000   0.9400   0.01294   0.00583  -0.1130   0.0336   0.6772
   5.250   0.9672   0.01316   0.00604  -0.1127   0.0326   0.6777
   5.500   0.9941   0.01339   0.00625  -0.1123   0.0316   0.6781
   5.750   1.0208   0.01366   0.00650  -0.1119   0.0306   0.6785
   6.000   1.0474   0.01393   0.00679  -0.1115   0.0299   0.6788
   6.250   1.0741   0.01417   0.00704  -0.1111   0.0294   0.6791
   6.500   1.1006   0.01443   0.00731  -0.1107   0.0288   0.6794
   6.750   1.1271   0.01468   0.00757  -0.1102   0.0281   0.6800
   7.000   1.1534   0.01494   0.00784  -0.1098   0.0274   0.6807
   7.250   1.1794   0.01522   0.00813  -0.1093   0.0268   0.6813
   7.500   1.2051   0.01554   0.00845  -0.1087   0.0262   0.6818
   7.750   1.2303   0.01592   0.00885  -0.1081   0.0255   0.6823
   8.000   1.2558   0.01622   0.00919  -0.1075   0.0252   0.6829
   8.250   1.2811   0.01655   0.00955  -0.1069   0.0249   0.6834
   8.500   1.3062   0.01688   0.00993  -0.1062   0.0244   0.6838
   8.750   1.3310   0.01724   0.01032  -0.1055   0.0240   0.6844
   9.000   1.3556   0.01760   0.01071  -0.1048   0.0236   0.6850
   9.250   1.3800   0.01798   0.01112  -0.1040   0.0232   0.6856
   9.500   1.4041   0.01837   0.01154  -0.1032   0.0228   0.6862
   9.750   1.4279   0.01878   0.01198  -0.1023   0.0225   0.6868
  10.000   1.4512   0.01923   0.01246  -0.1014   0.0220   0.6873
  10.250   1.4738   0.01976   0.01302  -0.1004   0.0216   0.6878
  10.500   1.4963   0.02026   0.01357  -0.0993   0.0213   0.6883
  10.750   1.5189   0.02071   0.01407  -0.0983   0.0211   0.6889
  11.000   1.5411   0.02118   0.01461  -0.0972   0.0209   0.6894
  11.250   1.5628   0.02168   0.01517  -0.0960   0.0207   0.6900
  11.500   1.5840   0.02221   0.01575  -0.0948   0.0204   0.6905
  11.750   1.6053   0.02269   0.01629  -0.0936   0.0201   0.6910
  12.000   1.6258   0.02322   0.01688  -0.0922   0.0198   0.6916
  12.250   1.6457   0.02377   0.01748  -0.0908   0.0196   0.6921
  12.500   1.6650   0.02435   0.01811  -0.0893   0.0193   0.6926
  12.750   1.6835   0.02496   0.01878  -0.0877   0.0191   0.6931
  13.000   1.7011   0.02561   0.01948  -0.0860   0.0188   0.6937
  13.250   1.7175   0.02631   0.02024  -0.0841   0.0187   0.6941
  13.500   1.7328   0.02704   0.02104  -0.0820   0.0185   0.6946
  13.750   1.7435   0.02780   0.02187  -0.0791   0.0183   0.6950
  14.000   1.7528   0.02866   0.02281  -0.0761   0.0181   0.6954
  14.250   1.7611   0.02964   0.02386  -0.0731   0.0179   0.6958
  14.500   1.7681   0.03071   0.02503  -0.0699   0.0178   0.6962
  14.750   1.7769   0.03166   0.02608  -0.0672   0.0177   0.6965
  15.000   1.7844   0.03272   0.02723  -0.0643   0.0176   0.6968
  15.250   1.7909   0.03385   0.02846  -0.0615   0.0176   0.6971
  15.500   1.7964   0.03509   0.02979  -0.0586   0.0175   0.6974
  15.750   1.8008   0.03643   0.03124  -0.0559   0.0174   0.6981
  16.000   1.8039   0.03793   0.03286  -0.0532   0.0173   0.6989
  16.250   1.8053   0.03961   0.03465  -0.0506   0.0173   0.6996
  16.500   1.8053   0.04150   0.03666  -0.0482   0.0172   0.7001
  16.750   1.8034   0.04365   0.03893  -0.0460   0.0171   0.7006
  17.000   1.7998   0.04608   0.04149  -0.0441   0.0171   0.7011
  17.250   1.7935   0.04900   0.04454  -0.0427   0.0170   0.7015
  17.500   1.7843   0.05247   0.04816  -0.0418   0.0169   0.7019
  17.750   1.7735   0.05653   0.05236  -0.0419   0.0169   0.7023
  18.000   1.7567   0.06196   0.05797  -0.0433   0.0168   0.7026
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