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DSMA-523B AIRFOIL (dsma523b-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: DSMA-523B AIRFOIL (dsma523b-il)
Reynolds number: 500,000
Max Cl/Cd: 60.04 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-dsma523b-il-500000-n5.txt
Download as CSV file: xf-dsma523b-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -1.0667   0.09496   0.09136  -0.0362   1.0000   0.0209
 -16.750  -1.1068   0.08304   0.07919  -0.0433   1.0000   0.0209
 -16.500  -1.1318   0.07453   0.07049  -0.0483   1.0000   0.0209
 -16.250  -1.1494   0.06785   0.06363  -0.0520   1.0000   0.0210
 -16.000  -1.1626   0.06232   0.05795  -0.0547   1.0000   0.0210
 -15.750  -1.1728   0.05769   0.05316  -0.0566   1.0000   0.0211
 -15.500  -1.1802   0.05382   0.04915  -0.0577   1.0000   0.0212
 -15.250  -1.1866   0.05043   0.04563  -0.0583   1.0000   0.0213
 -15.000  -1.1908   0.04749   0.04256  -0.0585   1.0000   0.0214
 -14.750  -1.1935   0.04488   0.03983  -0.0582   1.0000   0.0215
 -14.500  -1.1948   0.04255   0.03738  -0.0577   1.0000   0.0217
 -14.250  -1.1955   0.04042   0.03514  -0.0568   1.0000   0.0218
 -14.000  -1.1950   0.03853   0.03314  -0.0557   1.0000   0.0219
 -13.750  -1.1946   0.03680   0.03130  -0.0542   1.0000   0.0221
 -13.500  -1.1953   0.03523   0.02964  -0.0523   1.0000   0.0222
 -13.250  -1.1987   0.03380   0.02813  -0.0495   1.0000   0.0223
 -13.000  -1.1929   0.03239   0.02662  -0.0483   1.0000   0.0224
 -12.750  -1.1833   0.03088   0.02504  -0.0477   1.0000   0.0226
 -12.500  -1.1701   0.02944   0.02355  -0.0477   1.0000   0.0228
 -12.250  -1.1534   0.02820   0.02225  -0.0480   1.0000   0.0231
 -12.000  -1.1303   0.02705   0.02105  -0.0493   0.9996   0.0234
 -11.750  -1.1034   0.02601   0.01995  -0.0511   0.9989   0.0237
 -11.500  -1.0756   0.02504   0.01893  -0.0530   0.9982   0.0241
 -11.250  -1.0471   0.02413   0.01795  -0.0548   0.9975   0.0245
 -11.000  -1.0178   0.02328   0.01703  -0.0567   0.9968   0.0249
 -10.750  -0.9878   0.02247   0.01616  -0.0585   0.9962   0.0254
 -10.500  -0.9574   0.02173   0.01534  -0.0604   0.9957   0.0258
 -10.250  -0.9263   0.02105   0.01459  -0.0622   0.9951   0.0262
 -10.000  -0.8944   0.02029   0.01380  -0.0643   0.9947   0.0268
  -9.750  -0.8621   0.01966   0.01316  -0.0663   0.9942   0.0275
  -9.500  -0.8298   0.01912   0.01259  -0.0681   0.9939   0.0282
  -9.250  -0.7984   0.01862   0.01206  -0.0697   0.9933   0.0289
  -9.000  -0.7677   0.01815   0.01155  -0.0710   0.9927   0.0298
  -8.750  -0.7365   0.01771   0.01106  -0.0724   0.9920   0.0306
  -8.500  -0.7046   0.01724   0.01060  -0.0739   0.9914   0.0317
  -8.250  -0.6729   0.01688   0.01025  -0.0753   0.9908   0.0329
  -8.000  -0.6410   0.01655   0.00990  -0.0767   0.9902   0.0343
  -7.750  -0.6088   0.01623   0.00959  -0.0781   0.9897   0.0359
  -7.500  -0.5768   0.01601   0.00940  -0.0793   0.9891   0.0375
  -7.250  -0.5443   0.01578   0.00916  -0.0807   0.9885   0.0392
  -7.000  -0.5114   0.01556   0.00895  -0.0821   0.9880   0.0409
  -6.750  -0.4789   0.01540   0.00881  -0.0834   0.9875   0.0427
  -6.500  -0.4463   0.01523   0.00862  -0.0846   0.9871   0.0451
  -6.250  -0.4137   0.01508   0.00848  -0.0859   0.9867   0.0469
  -6.000  -0.3813   0.01496   0.00837  -0.0871   0.9863   0.0492
  -5.750  -0.3487   0.01486   0.00824  -0.0882   0.9859   0.0512
  -5.500  -0.3149   0.01462   0.00803  -0.0899   0.9857   0.0529
  -5.250  -0.2816   0.01447   0.00789  -0.0913   0.9854   0.0549
  -5.000  -0.2512   0.01435   0.00777  -0.0920   0.9843   0.0567
  -4.750  -0.2175   0.01409   0.00753  -0.0936   0.9836   0.0584
  -4.500  -0.1836   0.01387   0.00735  -0.0952   0.9829   0.0599
  -4.250  -0.1504   0.01372   0.00721  -0.0965   0.9824   0.0618
  -4.000  -0.1175   0.01361   0.00711  -0.0978   0.9818   0.0632
  -3.750  -0.0837   0.01346   0.00700  -0.0993   0.9813   0.0647
  -3.500  -0.0496   0.01332   0.00689  -0.1008   0.9810   0.0667
  -3.250  -0.0158   0.01321   0.00681  -0.1023   0.9805   0.0690
  -3.000   0.0181   0.01312   0.00675  -0.1037   0.9800   0.0710
  -2.750   0.0525   0.01304   0.00673  -0.1052   0.9796   0.0740
  -2.500   0.0963   0.01268   0.00655  -0.1088   0.9786   0.1023
  -2.250   0.1505   0.01194   0.00594  -0.1143   0.9730   0.1279
  -2.000   0.1994   0.01135   0.00552  -0.1189   0.9687   0.1626
  -1.750   0.2516   0.01066   0.00505  -0.1242   0.9640   0.2160
  -1.250   0.3882   0.00846   0.00310  -0.1426   0.6896   0.5647
  -1.000   0.3992   0.01041   0.00383  -0.1389   0.3797   0.6134
  -0.750   0.4241   0.01112   0.00416  -0.1381   0.2831   0.6336
  -0.500   0.4500   0.01170   0.00443  -0.1375   0.2113   0.6445
  -0.250   0.4768   0.01219   0.00465  -0.1372   0.1509   0.6503
   0.000   0.5029   0.01265   0.00490  -0.1366   0.1061   0.6533
   0.250   0.5300   0.01296   0.00512  -0.1362   0.0889   0.6563
   0.500   0.5578   0.01321   0.00532  -0.1359   0.0800   0.6594
   0.750   0.5861   0.01346   0.00551  -0.1358   0.0735   0.6629
   1.000   0.6151   0.01369   0.00568  -0.1359   0.0684   0.6659
   1.250   0.6432   0.01390   0.00585  -0.1357   0.0639   0.6680
   1.500   0.6700   0.01417   0.00610  -0.1352   0.0599   0.6698
   1.750   0.6972   0.01438   0.00633  -0.1348   0.0573   0.6715
   2.000   0.7243   0.01464   0.00657  -0.1344   0.0546   0.6733
   2.250   0.7516   0.01492   0.00681  -0.1341   0.0520   0.6749
   2.500   0.7792   0.01516   0.00706  -0.1338   0.0501   0.6768
   2.750   0.8068   0.01540   0.00730  -0.1335   0.0481   0.6788
   3.000   0.8345   0.01567   0.00754  -0.1333   0.0463   0.6811
   3.250   0.8621   0.01598   0.00781  -0.1331   0.0444   0.6823
   3.500   0.8901   0.01622   0.00805  -0.1330   0.0431   0.6833
   3.750   0.9180   0.01647   0.00830  -0.1329   0.0417   0.6840
   4.000   0.9456   0.01673   0.00856  -0.1327   0.0405   0.6846
   4.250   0.9730   0.01703   0.00885  -0.1324   0.0393   0.6851
   4.500   0.9998   0.01741   0.00920  -0.1321   0.0381   0.6856
   4.750   1.0267   0.01772   0.00953  -0.1318   0.0373   0.6862
   5.000   1.0535   0.01801   0.00986  -0.1314   0.0363   0.6868
   5.250   1.0801   0.01831   0.01019  -0.1310   0.0353   0.6873
   5.500   1.1065   0.01863   0.01053  -0.1305   0.0343   0.6878
   5.750   1.1327   0.01896   0.01086  -0.1301   0.0334   0.6883
   6.000   1.1581   0.01943   0.01134  -0.1295   0.0324   0.6889
   6.250   1.1840   0.01979   0.01174  -0.1289   0.0317   0.6894
   6.500   1.2096   0.02016   0.01217  -0.1283   0.0309   0.6900
   6.750   1.2350   0.02057   0.01263  -0.1277   0.0302   0.6905
   7.000   1.2601   0.02100   0.01310  -0.1270   0.0296   0.6912
   7.250   1.2850   0.02142   0.01356  -0.1263   0.0290   0.6919
   7.500   1.3095   0.02187   0.01404  -0.1256   0.0284   0.6927
   7.750   1.3335   0.02240   0.01460  -0.1247   0.0279   0.6934
   8.000   1.3565   0.02306   0.01529  -0.1237   0.0274   0.6940
   8.250   1.3803   0.02359   0.01590  -0.1228   0.0270   0.6946
   8.500   1.4034   0.02417   0.01658  -0.1218   0.0266   0.6952
   8.750   1.4262   0.02478   0.01726  -0.1207   0.0262   0.6958
   9.000   1.4486   0.02540   0.01797  -0.1196   0.0258   0.6965
   9.250   1.4705   0.02605   0.01869  -0.1184   0.0254   0.6971
   9.500   1.4920   0.02669   0.01941  -0.1172   0.0250   0.6978
   9.750   1.5130   0.02735   0.02015  -0.1159   0.0247   0.6984
  10.000   1.5334   0.02802   0.02089  -0.1145   0.0244   0.6991
  10.250   1.5531   0.02872   0.02166  -0.1130   0.0241   0.6997
  10.500   1.5718   0.02947   0.02248  -0.1113   0.0238   0.7004
  10.750   1.5892   0.03031   0.02339  -0.1095   0.0236   0.7010
  11.000   1.6043   0.03129   0.02444  -0.1073   0.0233   0.7016
  11.250   1.6179   0.03236   0.02563  -0.1048   0.0230   0.7022
  11.500   1.6316   0.03333   0.02674  -0.1024   0.0229   0.7028
  11.750   1.6432   0.03440   0.02795  -0.0996   0.0227   0.7035
  12.000   1.6532   0.03553   0.02922  -0.0967   0.0225   0.7041
  12.250   1.6603   0.03672   0.03056  -0.0933   0.0223   0.7047
  12.500   1.6635   0.03798   0.03197  -0.0893   0.0222   0.7054
  12.750   1.6674   0.03940   0.03355  -0.0857   0.0220   0.7060
  13.000   1.6704   0.04095   0.03526  -0.0821   0.0218   0.7066
  13.250   1.6718   0.04264   0.03711  -0.0786   0.0216   0.7072
  13.500   1.6719   0.04448   0.03911  -0.0752   0.0215   0.7077
  13.750   1.6703   0.04648   0.04127  -0.0718   0.0213   0.7083
  14.000   1.6671   0.04872   0.04368  -0.0687   0.0212   0.7088
  14.250   1.6611   0.05134   0.04646  -0.0658   0.0211   0.7094
  14.500   1.6522   0.05440   0.04971  -0.0632   0.0210   0.7098
  14.750   1.6430   0.05774   0.05322  -0.0614   0.0209   0.7103
  15.000   1.6284   0.06203   0.05771  -0.0603   0.0208   0.7108
  15.250   1.6126   0.06705   0.06291  -0.0606   0.0207   0.7112
  15.500   1.5863   0.07462   0.07073  -0.0633   0.0207   0.7116
  15.750   1.5456   0.08695   0.08338  -0.0713   0.0207   0.7117
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