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LWK 79-100 (lwk79100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: LWK 79-100 (lwk79100-il)
Reynolds number: 1,000,000
Max Cl/Cd: 72.56 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-lwk79100-il-1000000.txt
Download as CSV file: xf-lwk79100-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: LWK 79-100                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -1.0586   0.12116   0.11899   0.0220   1.0000   0.0080
 -17.000  -1.0929   0.10918   0.10685   0.0150   1.0000   0.0079
 -16.750  -1.1217   0.09883   0.09637   0.0090   1.0000   0.0079
 -16.500  -1.1513   0.08867   0.08605   0.0031   1.0000   0.0078
 -16.250  -1.1747   0.08007   0.07731  -0.0020   1.0000   0.0077
 -16.000  -1.1952   0.07243   0.06952  -0.0065   1.0000   0.0077
 -15.750  -1.2167   0.06490   0.06186  -0.0110   1.0000   0.0078
 -15.500  -1.2333   0.05853   0.05536  -0.0147   1.0000   0.0077
 -15.250  -1.2515   0.05227   0.04895  -0.0182   1.0000   0.0078
 -15.000  -1.2611   0.04758   0.04413  -0.0207   1.0000   0.0078
 -14.750  -1.2730   0.04288   0.03929  -0.0229   1.0000   0.0078
 -14.500  -1.2804   0.03900   0.03529  -0.0245   1.0000   0.0079
 -14.250  -1.2849   0.03571   0.03189  -0.0256   1.0000   0.0081
 -14.000  -1.2834   0.03332   0.02941  -0.0261   1.0000   0.0082
 -13.750  -1.2834   0.03109   0.02708  -0.0261   1.0000   0.0083
 -13.500  -1.2851   0.02915   0.02503  -0.0250   1.0000   0.0084
 -13.250  -1.2833   0.02779   0.02358  -0.0231   1.0000   0.0086
 -13.000  -1.2814   0.02655   0.02223  -0.0204   1.0000   0.0087
 -12.750  -1.2698   0.02560   0.02121  -0.0189   1.0000   0.0090
 -12.500  -1.2565   0.02462   0.02013  -0.0176   1.0000   0.0092
 -12.250  -1.2427   0.02356   0.01897  -0.0163   1.0000   0.0094
 -12.000  -1.2253   0.02276   0.01808  -0.0153   1.0000   0.0097
 -11.750  -1.2075   0.02192   0.01715  -0.0143   1.0000   0.0099
 -11.500  -1.1881   0.02120   0.01635  -0.0134   1.0000   0.0100
 -11.250  -1.1771   0.01944   0.01443  -0.0117   1.0000   0.0105
 -11.000  -1.1583   0.01850   0.01341  -0.0108   1.0000   0.0111
 -10.750  -1.1369   0.01785   0.01271  -0.0101   1.0000   0.0115
 -10.500  -1.1145   0.01728   0.01210  -0.0095   1.0000   0.0120
 -10.250  -1.0919   0.01670   0.01146  -0.0088   1.0000   0.0126
 -10.000  -1.0686   0.01620   0.01089  -0.0082   1.0000   0.0131
  -9.750  -1.0460   0.01556   0.01019  -0.0076   1.0000   0.0137
  -9.500  -1.0244   0.01477   0.00935  -0.0068   1.0000   0.0150
  -9.250  -0.9998   0.01439   0.00896  -0.0064   1.0000   0.0161
  -9.000  -0.9750   0.01402   0.00856  -0.0059   1.0000   0.0171
  -8.750  -0.9504   0.01361   0.00810  -0.0054   1.0000   0.0179
  -8.500  -0.9274   0.01293   0.00739  -0.0048   1.0000   0.0199
  -8.250  -0.9021   0.01260   0.00705  -0.0044   1.0000   0.0213
  -8.000  -0.8765   0.01231   0.00673  -0.0040   1.0000   0.0225
  -7.750  -0.8516   0.01189   0.00626  -0.0035   1.0000   0.0239
  -7.500  -0.8271   0.01141   0.00578  -0.0030   1.0000   0.0263
  -7.250  -0.8015   0.01111   0.00546  -0.0026   1.0000   0.0281
  -7.000  -0.7754   0.01087   0.00521  -0.0022   1.0000   0.0295
  -6.750  -0.7504   0.01045   0.00475  -0.0017   1.0000   0.0321
  -6.500  -0.7251   0.01009   0.00442  -0.0012   1.0000   0.0351
  -6.250  -0.6991   0.00985   0.00416  -0.0008   1.0000   0.0376
  -6.000  -0.6737   0.00950   0.00382  -0.0003   1.0000   0.0426
  -5.750  -0.6481   0.00921   0.00355   0.0002   1.0000   0.0476
  -5.500  -0.6228   0.00887   0.00327   0.0007   1.0000   0.0575
  -5.250  -0.5976   0.00855   0.00301   0.0012   1.0000   0.0715
  -5.000  -0.5726   0.00821   0.00277   0.0018   1.0000   0.0905
  -4.750  -0.5378   0.00787   0.00254   0.0001   0.9870   0.1137
  -4.500  -0.4874   0.00759   0.00227  -0.0048   0.8870   0.1488
  -4.250  -0.4652   0.00763   0.00209  -0.0034   0.8016   0.1731
  -4.000  -0.4397   0.00749   0.00193  -0.0029   0.7691   0.2002
  -3.750  -0.4136   0.00729   0.00177  -0.0026   0.7484   0.2321
  -3.500  -0.3873   0.00705   0.00161  -0.0023   0.7329   0.2720
  -3.250  -0.3608   0.00680   0.00147  -0.0020   0.7203   0.3150
  -3.000  -0.3340   0.00658   0.00136  -0.0018   0.7096   0.3589
  -2.750  -0.3072   0.00639   0.00127  -0.0015   0.7000   0.3995
  -2.500  -0.2800   0.00620   0.00119  -0.0014   0.6911   0.4378
  -2.250  -0.2525   0.00609   0.00113  -0.0012   0.6833   0.4676
  -2.000  -0.2248   0.00600   0.00109  -0.0010   0.6753   0.4936
  -1.750  -0.1970   0.00593   0.00106  -0.0009   0.6680   0.5161
  -1.500  -0.1689   0.00589   0.00104  -0.0007   0.6603   0.5343
  -1.250  -0.1409   0.00587   0.00102  -0.0006   0.6520   0.5501
  -1.000  -0.1129   0.00586   0.00100  -0.0004   0.6420   0.5638
  -0.750  -0.0847   0.00583   0.00099  -0.0003   0.6330   0.5756
  -0.500  -0.0566   0.00584   0.00099  -0.0002   0.6244   0.5865
  -0.250  -0.0282   0.00583   0.00098  -0.0001   0.6152   0.5974
   0.000   0.0000   0.00583   0.00098   0.0000   0.6069   0.6071
   0.250   0.0282   0.00583   0.00098   0.0001   0.5973   0.6152
   0.500   0.0566   0.00584   0.00099   0.0002   0.5865   0.6244
   0.750   0.0847   0.00583   0.00099   0.0003   0.5756   0.6330
   1.000   0.1129   0.00586   0.00100   0.0004   0.5638   0.6421
   1.250   0.1409   0.00587   0.00102   0.0006   0.5501   0.6520
   1.500   0.1689   0.00589   0.00104   0.0007   0.5342   0.6603
   1.750   0.1970   0.00593   0.00106   0.0009   0.5163   0.6680
   2.000   0.2248   0.00599   0.00110   0.0010   0.4938   0.6753
   2.250   0.2525   0.00608   0.00113   0.0012   0.4677   0.6833
   2.500   0.2800   0.00620   0.00119   0.0014   0.4375   0.6912
   2.750   0.3072   0.00639   0.00127   0.0015   0.3995   0.7001
   3.000   0.3340   0.00658   0.00136   0.0018   0.3583   0.7096
   3.250   0.3608   0.00680   0.00147   0.0020   0.3151   0.7203
   3.500   0.3873   0.00705   0.00161   0.0023   0.2715   0.7329
   3.750   0.4136   0.00729   0.00177   0.0026   0.2322   0.7485
   4.000   0.4397   0.00749   0.00193   0.0029   0.2002   0.7692
   4.250   0.4653   0.00763   0.00209   0.0034   0.1729   0.8014
   4.500   0.4874   0.00759   0.00227   0.0048   0.1488   0.8868
   4.750   0.5379   0.00787   0.00254  -0.0002   0.1137   0.9872
   5.000   0.5725   0.00821   0.00277  -0.0017   0.0906   1.0000
   5.250   0.5975   0.00855   0.00301  -0.0012   0.0716   1.0000
   5.500   0.6228   0.00887   0.00326  -0.0007   0.0575   1.0000
   5.750   0.6480   0.00921   0.00355  -0.0002   0.0476   1.0000
   6.000   0.6737   0.00950   0.00382   0.0003   0.0426   1.0000
   6.250   0.6991   0.00985   0.00416   0.0008   0.0376   1.0000
   6.500   0.7251   0.01009   0.00442   0.0012   0.0351   1.0000
   6.750   0.7504   0.01045   0.00476   0.0017   0.0321   1.0000
   7.000   0.7754   0.01087   0.00521   0.0022   0.0295   1.0000
   7.250   0.8015   0.01111   0.00547   0.0026   0.0281   1.0000
   7.500   0.8272   0.01140   0.00577   0.0029   0.0262   1.0000
   7.750   0.8517   0.01190   0.00627   0.0035   0.0238   1.0000
   8.000   0.8766   0.01231   0.00673   0.0040   0.0225   1.0000
   8.250   0.9022   0.01260   0.00704   0.0044   0.0213   1.0000
   8.500   0.9275   0.01293   0.00740   0.0048   0.0199   1.0000
   8.750   0.9502   0.01366   0.00814   0.0055   0.0178   1.0000
   9.000   0.9751   0.01403   0.00857   0.0059   0.0171   1.0000
   9.250   0.9999   0.01441   0.00898   0.0064   0.0161   1.0000
   9.500   1.0245   0.01478   0.00936   0.0068   0.0150   1.0000
   9.750   1.0464   0.01554   0.01016   0.0075   0.0137   1.0000
  10.000   1.0687   0.01622   0.01092   0.0082   0.0131   1.0000
  10.250   1.0922   0.01671   0.01146   0.0088   0.0126   1.0000
  10.500   1.1149   0.01727   0.01208   0.0094   0.0120   1.0000
  10.750   1.1374   0.01783   0.01269   0.0100   0.0115   1.0000
  11.000   1.1588   0.01849   0.01340   0.0107   0.0110   1.0000
  11.250   1.1774   0.01947   0.01445   0.0117   0.0105   1.0000
  11.500   1.1890   0.02118   0.01632   0.0133   0.0100   1.0000
  11.750   1.2084   0.02190   0.01713   0.0141   0.0098   1.0000
  12.000   1.2261   0.02276   0.01808   0.0152   0.0097   1.0000
  12.250   1.2427   0.02364   0.01906   0.0162   0.0094   1.0000
  12.500   1.2591   0.02446   0.01996   0.0173   0.0092   1.0000
  12.750   1.2714   0.02555   0.02115   0.0187   0.0089   1.0000
  13.000   1.2819   0.02661   0.02230   0.0203   0.0087   1.0000
  13.250   1.2862   0.02770   0.02348   0.0227   0.0086   1.0000
  13.500   1.2859   0.02919   0.02508   0.0249   0.0084   1.0000
  13.750   1.2871   0.03089   0.02686   0.0259   0.0083   1.0000
  14.000   1.2859   0.03321   0.02930   0.0260   0.0082   1.0000
  14.250   1.2848   0.03588   0.03208   0.0254   0.0081   1.0000
  14.500   1.2826   0.03893   0.03522   0.0243   0.0079   1.0000
  14.750   1.2747   0.04288   0.03930   0.0227   0.0079   1.0000
  15.000   1.2636   0.04751   0.04404   0.0204   0.0077   1.0000
  15.250   1.2517   0.05252   0.04919   0.0178   0.0077   1.0000
  15.500   1.2368   0.05831   0.05512   0.0145   0.0077   1.0000
  15.750   1.2192   0.06484   0.06180   0.0107   0.0078   1.0000
  16.000   1.1964   0.07258   0.06969   0.0061   0.0078   1.0000
  16.250   1.1765   0.08013   0.07738   0.0017   0.0078   1.0000
  16.500   1.1515   0.08904   0.08644  -0.0036   0.0078   1.0000
  16.750   1.1242   0.09876   0.09630  -0.0093   0.0079   1.0000
  17.000   1.0933   0.10953   0.10721  -0.0155   0.0079   1.0000
  17.250   1.0588   0.12157   0.11942  -0.0225   0.0081   1.0000
  17.500   1.0023   0.13976   0.13782  -0.0331   0.0082   1.0000
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