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DSMA-523A AIRFOIL (dsma523a-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: DSMA-523A AIRFOIL (dsma523a-il)
Reynolds number: 500,000
Max Cl/Cd: 59.35 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-dsma523a-il-500000-n5.txt
Download as CSV file: xf-dsma523a-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -1.0926   0.08958   0.08577  -0.0409   1.0000   0.0204
 -16.750  -1.1193   0.08064   0.07664  -0.0461   1.0000   0.0204
 -16.500  -1.1380   0.07351   0.06934  -0.0502   1.0000   0.0205
 -16.250  -1.1521   0.06754   0.06322  -0.0534   1.0000   0.0205
 -16.000  -1.1619   0.06258   0.05813  -0.0558   1.0000   0.0206
 -15.750  -1.1690   0.05836   0.05379  -0.0575   1.0000   0.0207
 -15.500  -1.1741   0.05466   0.04997  -0.0587   1.0000   0.0208
 -15.250  -1.1777   0.05142   0.04662  -0.0595   1.0000   0.0209
 -15.000  -1.1802   0.04854   0.04364  -0.0598   1.0000   0.0211
 -14.750  -1.1816   0.04599   0.04097  -0.0597   1.0000   0.0212
 -14.500  -1.1821   0.04366   0.03854  -0.0594   1.0000   0.0213
 -14.250  -1.1811   0.04157   0.03635  -0.0588   1.0000   0.0214
 -14.000  -1.1792   0.03965   0.03433  -0.0581   1.0000   0.0216
 -13.750  -1.1766   0.03788   0.03247  -0.0571   1.0000   0.0218
 -13.500  -1.1729   0.03627   0.03077  -0.0560   1.0000   0.0219
 -13.250  -1.1691   0.03476   0.02917  -0.0547   1.0000   0.0221
 -13.000  -1.1643   0.03340   0.02772  -0.0532   1.0000   0.0223
 -12.750  -1.1600   0.03212   0.02636  -0.0515   1.0000   0.0225
 -12.500  -1.1561   0.03095   0.02511  -0.0495   1.0000   0.0226
 -12.250  -1.1539   0.02989   0.02397  -0.0470   1.0000   0.0228
 -12.000  -1.1539   0.02891   0.02293  -0.0440   1.0000   0.0230
 -11.750  -1.1409   0.02788   0.02181  -0.0433   0.9995   0.0232
 -11.500  -1.1193   0.02678   0.02064  -0.0442   0.9984   0.0234
 -11.250  -1.0964   0.02562   0.01943  -0.0454   0.9969   0.0238
 -11.000  -1.0709   0.02464   0.01842  -0.0469   0.9956   0.0242
 -10.750  -1.0442   0.02378   0.01753  -0.0483   0.9946   0.0245
 -10.500  -1.0167   0.02301   0.01670  -0.0497   0.9938   0.0250
 -10.250  -0.9924   0.02223   0.01588  -0.0504   0.9922   0.0254
 -10.000  -0.9663   0.02151   0.01511  -0.0514   0.9909   0.0260
  -9.750  -0.9391   0.02082   0.01436  -0.0524   0.9897   0.0265
  -9.500  -0.9109   0.02018   0.01367  -0.0536   0.9887   0.0270
  -9.250  -0.8819   0.01953   0.01297  -0.0550   0.9878   0.0276
  -9.000  -0.8519   0.01888   0.01232  -0.0565   0.9870   0.0283
  -8.750  -0.8210   0.01834   0.01177  -0.0580   0.9864   0.0291
  -8.500  -0.7897   0.01785   0.01125  -0.0596   0.9858   0.0299
  -8.250  -0.7612   0.01737   0.01073  -0.0605   0.9847   0.0308
  -8.000  -0.7329   0.01691   0.01023  -0.0613   0.9834   0.0316
  -7.750  -0.7033   0.01646   0.00980  -0.0623   0.9824   0.0328
  -7.500  -0.6730   0.01610   0.00945  -0.0634   0.9816   0.0340
  -7.250  -0.6424   0.01577   0.00911  -0.0645   0.9809   0.0356
  -7.000  -0.6112   0.01548   0.00885  -0.0656   0.9803   0.0373
  -6.750  -0.5796   0.01528   0.00866  -0.0667   0.9797   0.0392
  -6.500  -0.5474   0.01503   0.00841  -0.0680   0.9791   0.0413
  -6.250  -0.5153   0.01488   0.00828  -0.0691   0.9787   0.0432
  -6.000  -0.4859   0.01470   0.00809  -0.0697   0.9776   0.0456
  -5.750  -0.4568   0.01449   0.00788  -0.0702   0.9764   0.0473
  -5.500  -0.4264   0.01431   0.00772  -0.0710   0.9755   0.0492
  -5.250  -0.3956   0.01417   0.00756  -0.0718   0.9747   0.0515
  -5.000  -0.3635   0.01392   0.00733  -0.0730   0.9741   0.0532
  -4.750  -0.3306   0.01367   0.00709  -0.0744   0.9736   0.0549
  -4.500  -0.2975   0.01347   0.00690  -0.0757   0.9731   0.0569
  -4.250  -0.2647   0.01334   0.00676  -0.0769   0.9726   0.0584
  -4.000  -0.2303   0.01297   0.00644  -0.0787   0.9724   0.0602
  -3.750  -0.1992   0.01275   0.00625  -0.0797   0.9714   0.0617
  -3.500  -0.1684   0.01257   0.00609  -0.0805   0.9702   0.0634
  -3.250  -0.1362   0.01243   0.00596  -0.0816   0.9693   0.0647
  -3.000  -0.1025   0.01224   0.00581  -0.0830   0.9686   0.0664
  -2.750  -0.0685   0.01205   0.00566  -0.0845   0.9681   0.0691
  -2.500  -0.0350   0.01192   0.00556  -0.0858   0.9677   0.0714
  -2.250   0.0000   0.01179   0.00549  -0.0874   0.9671   0.0742
  -2.000   0.0414   0.01140   0.00522  -0.0902   0.9627   0.0844
  -1.750   0.0583   0.01097   0.00490  -0.0878   0.9483   0.1113
  -1.500   0.0924   0.01044   0.00451  -0.0890   0.9384   0.1380
  -1.250   0.1399   0.00968   0.00394  -0.0929   0.9317   0.1795
  -1.000   0.2110   0.00842   0.00305  -0.1021   0.9233   0.2783
  -0.750   0.3015   0.00756   0.00248  -0.1163   0.6864   0.6084
  -0.500   0.3105   0.00924   0.00308  -0.1123   0.4208   0.6336
  -0.250   0.3341   0.00997   0.00339  -0.1112   0.3208   0.6482
   0.000   0.3588   0.01052   0.00365  -0.1104   0.2488   0.6536
   0.250   0.3852   0.01098   0.00381  -0.1100   0.1819   0.6575
   0.500   0.4128   0.01140   0.00392  -0.1100   0.1238   0.6615
   0.750   0.4388   0.01176   0.00416  -0.1094   0.0975   0.6644
   1.000   0.4645   0.01209   0.00445  -0.1086   0.0860   0.6674
   1.250   0.4909   0.01240   0.00471  -0.1080   0.0776   0.6708
   1.500   0.5185   0.01263   0.00491  -0.1077   0.0720   0.6741
   1.750   0.5468   0.01285   0.00505  -0.1077   0.0667   0.6763
   2.000   0.5756   0.01304   0.00520  -0.1077   0.0631   0.6781
   2.250   0.6044   0.01323   0.00535  -0.1078   0.0596   0.6795
   2.500   0.6313   0.01346   0.00554  -0.1074   0.0561   0.6805
   2.750   0.6579   0.01367   0.00577  -0.1069   0.0539   0.6819
   3.000   0.6840   0.01392   0.00604  -0.1062   0.0517   0.6836
   3.250   0.7097   0.01423   0.00633  -0.1055   0.0496   0.6857
   3.500   0.7359   0.01453   0.00663  -0.1050   0.0476   0.6876
   3.750   0.7631   0.01476   0.00687  -0.1047   0.0460   0.6890
   4.000   0.7908   0.01498   0.00708  -0.1045   0.0445   0.6897
   4.250   0.8182   0.01522   0.00731  -0.1043   0.0431   0.6904
   4.500   0.8452   0.01553   0.00759  -0.1041   0.0417   0.6911
   4.750   0.8723   0.01583   0.00790  -0.1038   0.0406   0.6918
   5.000   0.8995   0.01610   0.00818  -0.1035   0.0396   0.6925
   5.250   0.9266   0.01636   0.00846  -0.1033   0.0383   0.6931
   5.500   0.9535   0.01665   0.00874  -0.1030   0.0372   0.6940
   5.750   0.9801   0.01698   0.00905  -0.1027   0.0362   0.6948
   6.000   1.0058   0.01743   0.00949  -0.1022   0.0352   0.6956
   6.250   1.0323   0.01775   0.00986  -0.1018   0.0345   0.6961
   6.500   1.0585   0.01809   0.01023  -0.1014   0.0336   0.6966
   6.750   1.0846   0.01843   0.01059  -0.1010   0.0327   0.6971
   7.000   1.1104   0.01878   0.01096  -0.1005   0.0319   0.6975
   7.250   1.1359   0.01914   0.01133  -0.1000   0.0311   0.6981
   7.500   1.1604   0.01960   0.01180  -0.0993   0.0305   0.6987
   7.750   1.1845   0.02012   0.01237  -0.0986   0.0299   0.6992
   8.000   1.2090   0.02057   0.01290  -0.0978   0.0294   0.6997
   8.250   1.2331   0.02106   0.01345  -0.0970   0.0289   0.7002
   8.500   1.2569   0.02156   0.01402  -0.0962   0.0283   0.7008
   8.750   1.2804   0.02207   0.01460  -0.0954   0.0278   0.7013
   9.000   1.3037   0.02258   0.01517  -0.0945   0.0274   0.7018
   9.250   1.3266   0.02311   0.01575  -0.0936   0.0269   0.7024
   9.500   1.3491   0.02365   0.01635  -0.0926   0.0265   0.7030
   9.750   1.3707   0.02427   0.01701  -0.0915   0.0262   0.7037
  10.000   1.3912   0.02499   0.01779  -0.0902   0.0257   0.7045
  10.250   1.4108   0.02583   0.01870  -0.0888   0.0254   0.7052
  10.500   1.4311   0.02656   0.01955  -0.0875   0.0252   0.7058
  10.750   1.4505   0.02734   0.02044  -0.0861   0.0249   0.7064
  11.000   1.4692   0.02816   0.02138  -0.0846   0.0246   0.7070
  11.250   1.4869   0.02903   0.02237  -0.0829   0.0243   0.7076
  11.500   1.5037   0.02992   0.02338  -0.0812   0.0240   0.7083
  11.750   1.5198   0.03079   0.02436  -0.0794   0.0237   0.7089
  12.000   1.5347   0.03171   0.02538  -0.0774   0.0234   0.7095
  12.250   1.5485   0.03261   0.02638  -0.0753   0.0232   0.7101
  12.500   1.5579   0.03350   0.02738  -0.0724   0.0229   0.7108
  12.750   1.5666   0.03450   0.02849  -0.0695   0.0227   0.7114
  13.000   1.5753   0.03554   0.02961  -0.0668   0.0225   0.7120
  13.250   1.5820   0.03674   0.03093  -0.0640   0.0224   0.7125
  13.500   1.5873   0.03805   0.03235  -0.0611   0.0222   0.7131
  13.750   1.5910   0.03948   0.03389  -0.0582   0.0221   0.7136
  14.000   1.5929   0.04110   0.03562  -0.0553   0.0219   0.7141
  14.250   1.5924   0.04296   0.03761  -0.0525   0.0218   0.7145
  14.500   1.5894   0.04513   0.03990  -0.0498   0.0217   0.7149
  14.750   1.5835   0.04768   0.04258  -0.0475   0.0215   0.7153
  15.000   1.5739   0.05079   0.04584  -0.0455   0.0214   0.7156
  15.250   1.5644   0.05421   0.04945  -0.0443   0.0213   0.7160
  15.500   1.5520   0.05835   0.05380  -0.0441   0.0213   0.7164
  15.750   1.5350   0.06370   0.05937  -0.0454   0.0212   0.7169
  16.000   1.5128   0.07085   0.06675  -0.0489   0.0211   0.7174
  16.250   1.4793   0.08162   0.07780  -0.0563   0.0212   0.7176
  16.500   1.4173   0.10018   0.09671  -0.0696   0.0213   0.7175
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