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DSMA-523B AIRFOIL (dsma523b-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: DSMA-523B AIRFOIL (dsma523b-il)
Reynolds number: 1,000,000
Max Cl/Cd: 77.27 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-dsma523b-il-1000000-n5.txt
Download as CSV file: xf-dsma523b-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DSMA-523B 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  -1.0242   0.11704   0.11412  -0.0527   0.9847   0.0166
 -19.500  -1.0762   0.10358   0.10048  -0.0601   0.9849   0.0166
 -19.250  -1.1218   0.09165   0.08836  -0.0668   0.9852   0.0165
 -19.000  -1.1576   0.08177   0.07830  -0.0723   0.9856   0.0165
 -18.750  -1.1833   0.07387   0.07025  -0.0766   0.9859   0.0165
 -18.500  -1.2031   0.06721   0.06346  -0.0802   0.9863   0.0166
 -18.250  -1.2170   0.06172   0.05784  -0.0830   0.9866   0.0166
 -18.000  -1.2278   0.05700   0.05301  -0.0851   0.9869   0.0167
 -17.750  -1.2347   0.05310   0.04900  -0.0865   0.9872   0.0167
 -17.500  -1.2401   0.04964   0.04544  -0.0875   0.9875   0.0168
 -17.250  -1.2434   0.04666   0.04237  -0.0880   0.9877   0.0169
 -17.000  -1.2454   0.04410   0.03973  -0.0880   0.9880   0.0170
 -16.750  -1.2485   0.04184   0.03739  -0.0873   0.9881   0.0171
 -16.500  -1.2506   0.03985   0.03533  -0.0863   0.9882   0.0172
 -16.250  -1.2512   0.03808   0.03349  -0.0851   0.9884   0.0173
 -16.000  -1.2516   0.03637   0.03171  -0.0838   0.9885   0.0174
 -15.750  -1.2501   0.03483   0.03010  -0.0824   0.9887   0.0175
 -15.500  -1.2473   0.03345   0.02866  -0.0810   0.9888   0.0176
 -15.250  -1.2441   0.03213   0.02727  -0.0794   0.9889   0.0177
 -15.000  -1.2407   0.03087   0.02595  -0.0778   0.9889   0.0179
 -14.750  -1.2359   0.02977   0.02480  -0.0760   0.9890   0.0180
 -14.500  -1.2331   0.02868   0.02365  -0.0739   0.9889   0.0182
 -14.250  -1.2314   0.02771   0.02263  -0.0713   0.9888   0.0183
 -14.000  -1.2226   0.02668   0.02154  -0.0700   0.9886   0.0185
 -13.750  -1.2051   0.02565   0.02045  -0.0702   0.9882   0.0186
 -13.500  -1.1874   0.02475   0.01950  -0.0702   0.9880   0.0187
 -13.250  -1.1678   0.02384   0.01853  -0.0707   0.9878   0.0189
 -13.000  -1.1456   0.02279   0.01744  -0.0718   0.9875   0.0192
 -12.750  -1.1209   0.02189   0.01650  -0.0730   0.9872   0.0195
 -12.500  -1.0958   0.02110   0.01567  -0.0742   0.9870   0.0198
 -12.250  -1.0693   0.02039   0.01493  -0.0754   0.9869   0.0201
 -12.000  -1.0411   0.01971   0.01423  -0.0769   0.9867   0.0204
 -11.750  -1.0118   0.01908   0.01356  -0.0785   0.9865   0.0207
 -11.500  -0.9817   0.01849   0.01294  -0.0801   0.9863   0.0211
 -11.250  -0.9515   0.01793   0.01235  -0.0817   0.9862   0.0215
 -11.000  -0.9213   0.01741   0.01179  -0.0832   0.9861   0.0218
 -10.750  -0.8907   0.01692   0.01127  -0.0847   0.9860   0.0221
 -10.500  -0.8599   0.01647   0.01079  -0.0862   0.9859   0.0224
 -10.250  -0.8286   0.01595   0.01026  -0.0878   0.9858   0.0230
 -10.000  -0.7973   0.01552   0.00982  -0.0893   0.9857   0.0236
  -9.750  -0.7661   0.01513   0.00943  -0.0907   0.9856   0.0242
  -9.500  -0.7347   0.01478   0.00907  -0.0920   0.9855   0.0249
  -9.250  -0.7032   0.01445   0.00872  -0.0934   0.9854   0.0255
  -9.000  -0.6718   0.01416   0.00841  -0.0946   0.9853   0.0261
  -8.750  -0.6433   0.01385   0.00811  -0.0952   0.9849   0.0267
  -8.500  -0.6136   0.01354   0.00780  -0.0960   0.9844   0.0276
  -8.250  -0.5832   0.01326   0.00753  -0.0970   0.9840   0.0285
  -8.000  -0.5525   0.01301   0.00728  -0.0979   0.9837   0.0295
  -7.750  -0.5215   0.01278   0.00705  -0.0989   0.9833   0.0304
  -7.500  -0.4898   0.01254   0.00682  -0.1001   0.9829   0.0319
  -7.250  -0.4580   0.01232   0.00663  -0.1012   0.9826   0.0336
  -7.000  -0.4260   0.01212   0.00645  -0.1024   0.9822   0.0352
  -6.750  -0.3938   0.01195   0.00632  -0.1035   0.9818   0.0379
  -6.500  -0.3616   0.01181   0.00622  -0.1046   0.9814   0.0408
  -6.250  -0.3298   0.01170   0.00614  -0.1056   0.9811   0.0439
  -6.000  -0.2978   0.01159   0.00604  -0.1066   0.9808   0.0460
  -5.750  -0.2659   0.01150   0.00599  -0.1076   0.9804   0.0481
  -5.500  -0.2341   0.01142   0.00592  -0.1085   0.9801   0.0500
  -5.250  -0.2021   0.01134   0.00585  -0.1095   0.9798   0.0510
  -5.000  -0.1687   0.01117   0.00570  -0.1109   0.9796   0.0523
  -4.750  -0.1357   0.01105   0.00561  -0.1121   0.9794   0.0536
  -4.500  -0.1026   0.01093   0.00552  -0.1133   0.9792   0.0549
  -4.250  -0.0692   0.01082   0.00543  -0.1146   0.9789   0.0559
  -4.000  -0.0359   0.01072   0.00535  -0.1158   0.9787   0.0566
  -3.750  -0.0026   0.01062   0.00527  -0.1171   0.9785   0.0574
  -3.500   0.0324   0.01046   0.00514  -0.1187   0.9783   0.0588
  -3.250   0.0726   0.01011   0.00483  -0.1214   0.9750   0.0599
  -3.000   0.1554   0.00915   0.00389  -0.1336   0.9726   0.0621
  -2.750   0.0907   0.01023   0.00499  -0.1128   0.9392   0.0615
  -2.500   0.1376   0.00965   0.00444  -0.1167   0.9338   0.0627
  -2.250   0.2506   0.00819   0.00294  -0.1353   0.9252   0.0641
  -2.000   0.2892   0.00807   0.00277  -0.1376   0.8953   0.0653
  -1.750   0.2918   0.01043   0.00312  -0.1320   0.4100   0.0660
  -1.500   0.3196   0.01083   0.00318  -0.1321   0.3129   0.0674
  -1.250   0.3484   0.01113   0.00323  -0.1323   0.2406   0.0695
  -0.750   0.4095   0.01150   0.00334  -0.1337   0.1341   0.1166
  -0.500   0.4424   0.01158   0.00341  -0.1350   0.0946   0.1683
  -0.250   0.4973   0.01064   0.00331  -0.1426   0.0800   0.4816
   0.000   0.5324   0.01057   0.00358  -0.1443   0.0722   0.6188
   0.250   0.5611   0.01074   0.00370  -0.1443   0.0673   0.6293
   0.500   0.5893   0.01094   0.00388  -0.1441   0.0618   0.6353
   0.750   0.6176   0.01112   0.00403  -0.1440   0.0580   0.6403
   1.000   0.6460   0.01130   0.00417  -0.1438   0.0545   0.6441
   1.250   0.6744   0.01149   0.00431  -0.1437   0.0514   0.6471
   1.500   0.7027   0.01166   0.00447  -0.1436   0.0495   0.6500
   1.750   0.7303   0.01187   0.00468  -0.1433   0.0469   0.6536
   2.000   0.7581   0.01210   0.00487  -0.1430   0.0443   0.6556
   2.250   0.7862   0.01227   0.00503  -0.1428   0.0429   0.6571
   2.500   0.8142   0.01245   0.00520  -0.1427   0.0411   0.6586
   2.750   0.8420   0.01267   0.00539  -0.1424   0.0393   0.6604
   3.000   0.8697   0.01290   0.00560  -0.1422   0.0378   0.6622
   3.250   0.8976   0.01309   0.00578  -0.1420   0.0369   0.6635
   3.500   0.9253   0.01330   0.00599  -0.1417   0.0358   0.6652
   3.750   0.9529   0.01352   0.00619  -0.1414   0.0346   0.6662
   4.000   0.9805   0.01375   0.00640  -0.1412   0.0336   0.6668
   4.250   1.0079   0.01400   0.00663  -0.1409   0.0324   0.6672
   4.500   1.0355   0.01420   0.00684  -0.1406   0.0319   0.6678
   4.750   1.0629   0.01441   0.00706  -0.1403   0.0312   0.6684
   5.000   1.0901   0.01464   0.00730  -0.1400   0.0305   0.6690
   5.250   1.1172   0.01487   0.00754  -0.1397   0.0297   0.6695
   5.500   1.1441   0.01513   0.00780  -0.1393   0.0289   0.6700
   5.750   1.1708   0.01541   0.00808  -0.1389   0.0281   0.6705
   6.000   1.1973   0.01572   0.00839  -0.1384   0.0273   0.6710
   6.250   1.2238   0.01599   0.00868  -0.1379   0.0269   0.6716
   6.500   1.2501   0.01627   0.00899  -0.1374   0.0264   0.6722
   6.750   1.2763   0.01657   0.00932  -0.1369   0.0259   0.6728
   7.000   1.3023   0.01687   0.00964  -0.1363   0.0253   0.6734
   7.250   1.3281   0.01719   0.00997  -0.1357   0.0248   0.6740
   7.500   1.3537   0.01752   0.01032  -0.1351   0.0242   0.6745
   7.750   1.3790   0.01789   0.01070  -0.1344   0.0237   0.6750
   8.000   1.4038   0.01831   0.01114  -0.1337   0.0232   0.6755
   8.250   1.4288   0.01868   0.01155  -0.1329   0.0229   0.6761
   8.500   1.4535   0.01907   0.01198  -0.1322   0.0226   0.6766
   8.750   1.4779   0.01945   0.01241  -0.1313   0.0223   0.6772
   9.000   1.5021   0.01986   0.01286  -0.1305   0.0220   0.6777
   9.250   1.5260   0.02028   0.01332  -0.1295   0.0217   0.6783
   9.500   1.5496   0.02071   0.01379  -0.1286   0.0214   0.6789
   9.750   1.5729   0.02116   0.01428  -0.1276   0.0211   0.6794
  10.000   1.5958   0.02162   0.01479  -0.1265   0.0208   0.6800
  10.250   1.6183   0.02211   0.01531  -0.1254   0.0205   0.6806
  10.500   1.6405   0.02261   0.01585  -0.1242   0.0203   0.6811
  10.750   1.6620   0.02315   0.01643  -0.1229   0.0199   0.6817
  11.000   1.6825   0.02376   0.01709  -0.1214   0.0195   0.6822
  11.250   1.7024   0.02440   0.01778  -0.1198   0.0192   0.6827
  11.500   1.7225   0.02495   0.01840  -0.1183   0.0191   0.6833
  11.750   1.7417   0.02553   0.01905  -0.1166   0.0189   0.6839
  12.000   1.7605   0.02611   0.01969  -0.1149   0.0187   0.6844
  12.250   1.7779   0.02675   0.02041  -0.1129   0.0185   0.6848
  12.500   1.7944   0.02741   0.02115  -0.1107   0.0184   0.6852
  12.750   1.8098   0.02811   0.02192  -0.1084   0.0182   0.6855
  13.000   1.8244   0.02883   0.02272  -0.1060   0.0180   0.6860
  13.250   1.8379   0.02958   0.02355  -0.1035   0.0179   0.6867
  13.500   1.8499   0.03039   0.02444  -0.1007   0.0177   0.6875
  13.750   1.8583   0.03120   0.02535  -0.0972   0.0175   0.6882
  14.000   1.8664   0.03212   0.02635  -0.0939   0.0174   0.6889
  14.250   1.8742   0.03313   0.02745  -0.0906   0.0173   0.6896
  14.500   1.8816   0.03420   0.02862  -0.0874   0.0172   0.6902
  14.750   1.8884   0.03533   0.02983  -0.0842   0.0170   0.6908
  15.000   1.8936   0.03660   0.03120  -0.0810   0.0169   0.6915
  15.250   1.8982   0.03794   0.03263  -0.0778   0.0167   0.6921
  15.500   1.9007   0.03947   0.03427  -0.0745   0.0167   0.6927
  15.750   1.9020   0.04114   0.03604  -0.0713   0.0165   0.6933
  16.000   1.9014   0.04303   0.03804  -0.0682   0.0164   0.6939
  16.250   1.8987   0.04519   0.04032  -0.0653   0.0163   0.6944
  16.500   1.8940   0.04765   0.04291  -0.0625   0.0162   0.6950
  16.750   1.8860   0.05060   0.04599  -0.0601   0.0161   0.6955
  17.000   1.8754   0.05405   0.04958  -0.0582   0.0160   0.6960
  17.250   1.8618   0.05817   0.05385  -0.0571   0.0159   0.6964
  17.500   1.8419   0.06367   0.05952  -0.0573   0.0158   0.6968
  17.750   1.8202   0.07034   0.06638  -0.0594   0.0158   0.6972
  18.000   1.7901   0.07964   0.07591  -0.0643   0.0158   0.6975
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