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FX 84-W-150 (fx84w150-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 84-W-150 (fx84w150-il)
Reynolds number: 1,000,000
Max Cl/Cd: 133.33 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx84w150-il-1000000-n5.txt
Download as CSV file: xf-fx84w150-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 84-W-150                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.6128   0.11515   0.11305  -0.0541   0.9923   0.0106
 -16.750  -0.6710   0.09881   0.09654  -0.0649   0.9743   0.0105
 -16.500  -0.8476   0.06292   0.06016  -0.0906   0.9606   0.0100
 -16.250  -0.9180   0.04377   0.04048  -0.1080   0.9266   0.0098
 -16.000  -0.9403   0.03810   0.03456  -0.1115   0.9037   0.0099
 -15.750  -0.9563   0.03420   0.03046  -0.1128   0.8881   0.0099
 -15.500  -0.9647   0.03149   0.02759  -0.1129   0.8761   0.0100
 -15.000  -0.9711   0.02765   0.02348  -0.1112   0.8566   0.0101
 -14.750  -0.9695   0.02630   0.02201  -0.1098   0.8481   0.0103
 -14.500  -0.9672   0.02507   0.02068  -0.1080   0.8403   0.0104
 -14.250  -0.9632   0.02407   0.01957  -0.1060   0.8331   0.0106
 -14.000  -0.9588   0.02316   0.01857  -0.1035   0.8269   0.0106
 -13.750  -0.9496   0.02242   0.01772  -0.1015   0.8208   0.0108
 -13.500  -0.9360   0.02166   0.01686  -0.1001   0.8153   0.0110
 -13.250  -0.9198   0.02096   0.01607  -0.0991   0.8100   0.0112
 -13.000  -0.9024   0.02029   0.01530  -0.0981   0.8046   0.0114
 -12.500  -0.8643   0.01904   0.01387  -0.0965   0.7954   0.0117
 -12.250  -0.8436   0.01848   0.01321  -0.0958   0.7905   0.0118
 -12.000  -0.8235   0.01783   0.01248  -0.0951   0.7855   0.0121
 -11.750  -0.8022   0.01723   0.01181  -0.0945   0.7811   0.0124
 -11.500  -0.7796   0.01671   0.01124  -0.0940   0.7765   0.0128
 -11.250  -0.7565   0.01624   0.01070  -0.0936   0.7715   0.0131
 -10.750  -0.7085   0.01540   0.00972  -0.0929   0.7628   0.0139
 -10.500  -0.6838   0.01501   0.00927  -0.0927   0.7581   0.0143
 -10.250  -0.6589   0.01464   0.00883  -0.0924   0.7536   0.0146
 -10.000  -0.6343   0.01421   0.00834  -0.0921   0.7494   0.0151
  -9.750  -0.6090   0.01381   0.00791  -0.0920   0.7451   0.0157
  -9.500  -0.5833   0.01347   0.00752  -0.0918   0.7407   0.0162
  -9.250  -0.5574   0.01316   0.00715  -0.0917   0.7364   0.0168
  -9.000  -0.5312   0.01286   0.00680  -0.0916   0.7323   0.0174
  -8.750  -0.5046   0.01258   0.00646  -0.0915   0.7280   0.0179
  -8.500  -0.4784   0.01225   0.00611  -0.0914   0.7237   0.0188
  -8.250  -0.4518   0.01199   0.00581  -0.0913   0.7197   0.0197
  -8.000  -0.4248   0.01174   0.00553  -0.0913   0.7161   0.0206
  -7.750  -0.3976   0.01151   0.00526  -0.0913   0.7118   0.0214
  -7.500  -0.3706   0.01125   0.00496  -0.0913   0.7073   0.0224
  -7.250  -0.3435   0.01102   0.00471  -0.0913   0.7031   0.0236
  -7.000  -0.3159   0.01081   0.00448  -0.0914   0.6995   0.0247
  -6.750  -0.2882   0.01063   0.00426  -0.0914   0.6954   0.0258
  -6.500  -0.2608   0.01041   0.00402  -0.0915   0.6909   0.0274
  -6.000  -0.2052   0.01007   0.00363  -0.0916   0.6825   0.0303
  -5.750  -0.1774   0.00989   0.00343  -0.0917   0.6777   0.0319
  -5.500  -0.1497   0.00973   0.00325  -0.0918   0.6728   0.0339
  -5.250  -0.1216   0.00960   0.00309  -0.0919   0.6686   0.0359
  -5.000  -0.0935   0.00943   0.00292  -0.0921   0.6642   0.0385
  -4.750  -0.0654   0.00929   0.00277  -0.0922   0.6596   0.0413
  -4.500  -0.0374   0.00918   0.00263  -0.0923   0.6551   0.0444
  -4.250  -0.0091   0.00904   0.00250  -0.0925   0.6512   0.0481
  -4.000   0.0192   0.00891   0.00238  -0.0926   0.6470   0.0523
  -3.750   0.0474   0.00880   0.00227  -0.0928   0.6425   0.0574
  -3.500   0.0756   0.00870   0.00216  -0.0929   0.6382   0.0631
  -3.250   0.1041   0.00859   0.00207  -0.0931   0.6340   0.0698
  -3.000   0.1324   0.00848   0.00198  -0.0933   0.6296   0.0783
  -2.750   0.1607   0.00839   0.00190  -0.0935   0.6254   0.0880
  -2.500   0.1890   0.00829   0.00183  -0.0937   0.6213   0.0995
  -2.250   0.2175   0.00820   0.00177  -0.0939   0.6170   0.1116
  -2.000   0.2458   0.00810   0.00171  -0.0941   0.6123   0.1279
  -1.750   0.2739   0.00801   0.00166  -0.0943   0.6080   0.1477
  -1.500   0.3023   0.00790   0.00162  -0.0945   0.6040   0.1720
  -1.250   0.3306   0.00778   0.00158  -0.0948   0.5992   0.2022
  -1.000   0.3586   0.00767   0.00155  -0.0949   0.5939   0.2376
  -0.750   0.3865   0.00752   0.00153  -0.0952   0.5890   0.2855
  -0.500   0.4144   0.00732   0.00150  -0.0954   0.5839   0.3450
  -0.250   0.4420   0.00712   0.00149  -0.0956   0.5790   0.4192
   0.000   0.4695   0.00691   0.00150  -0.0958   0.5747   0.4990
   0.250   0.4974   0.00673   0.00152  -0.0960   0.5701   0.5700
   0.500   0.5253   0.00664   0.00155  -0.0962   0.5649   0.6222
   0.750   0.5531   0.00662   0.00160  -0.0963   0.5601   0.6595
   1.000   0.5814   0.00658   0.00165  -0.0964   0.5561   0.6928
   1.250   0.6095   0.00658   0.00171  -0.0966   0.5515   0.7183
   1.500   0.6373   0.00661   0.00177  -0.0966   0.5465   0.7397
   1.750   0.6652   0.00665   0.00184  -0.0967   0.5418   0.7611
   2.000   0.6927   0.00666   0.00193  -0.0967   0.5368   0.7872
   2.250   0.7200   0.00671   0.00201  -0.0966   0.5315   0.8066
   2.500   0.7476   0.00679   0.00208  -0.0967   0.5262   0.8172
   2.750   0.7753   0.00685   0.00216  -0.0967   0.5200   0.8267
   3.000   0.8023   0.00695   0.00225  -0.0967   0.5140   0.8347
   3.250   0.8299   0.00702   0.00233  -0.0967   0.5087   0.8424
   3.500   0.8573   0.00710   0.00242  -0.0968   0.5028   0.8495
   3.750   0.8837   0.00721   0.00253  -0.0966   0.4973   0.8572
   4.250   0.9372   0.00739   0.00274  -0.0964   0.4845   0.8719
   4.500   0.9634   0.00752   0.00285  -0.0963   0.4762   0.8796
   4.750   0.9885   0.00765   0.00298  -0.0959   0.4676   0.8871
   5.000   1.0141   0.00777   0.00311  -0.0956   0.4597   0.8954
   5.250   1.0385   0.00791   0.00326  -0.0951   0.4522   0.9036
   5.750   1.0865   0.00818   0.00355  -0.0939   0.4375   0.9231
   6.000   1.1093   0.00832   0.00371  -0.0930   0.4298   0.9349
   6.250   1.1297   0.00852   0.00390  -0.0917   0.4173   0.9509
   6.500   1.1517   0.00889   0.00417  -0.0911   0.3901   0.9751
   6.750   1.1727   0.00942   0.00453  -0.0904   0.3580   1.0000
   7.000   1.1891   0.00990   0.00489  -0.0887   0.3319   1.0000
   7.250   1.2004   0.01043   0.00528  -0.0861   0.3054   1.0000
   7.500   1.2097   0.01101   0.00573  -0.0831   0.2818   1.0000
   7.750   1.2196   0.01161   0.00623  -0.0804   0.2594   1.0000
   8.000   1.2291   0.01228   0.00680  -0.0778   0.2377   1.0000
   8.250   1.2367   0.01307   0.00747  -0.0750   0.2135   1.0000
   8.500   1.2436   0.01394   0.00822  -0.0723   0.1913   1.0000
   8.750   1.2514   0.01483   0.00901  -0.0698   0.1697   1.0000
   9.000   1.2563   0.01591   0.00997  -0.0671   0.1459   1.0000
   9.250   1.2621   0.01701   0.01096  -0.0646   0.1247   1.0000
   9.500   1.2686   0.01813   0.01199  -0.0624   0.1072   1.0000
   9.750   1.2764   0.01922   0.01302  -0.0604   0.0926   1.0000
  10.000   1.2844   0.02035   0.01409  -0.0586   0.0802   1.0000
  10.250   1.2930   0.02147   0.01519  -0.0569   0.0703   1.0000
  10.500   1.3016   0.02264   0.01632  -0.0553   0.0617   1.0000
  10.750   1.3111   0.02379   0.01745  -0.0538   0.0545   1.0000
  11.000   1.3206   0.02496   0.01861  -0.0525   0.0487   1.0000
  11.250   1.3293   0.02623   0.01987  -0.0511   0.0431   1.0000
  11.500   1.3381   0.02752   0.02115  -0.0499   0.0384   1.0000
  11.750   1.3484   0.02873   0.02239  -0.0488   0.0358   1.0000
  12.000   1.3574   0.03009   0.02375  -0.0477   0.0325   1.0000
  12.250   1.3668   0.03145   0.02513  -0.0467   0.0300   1.0000
  12.500   1.3764   0.03283   0.02654  -0.0458   0.0281   1.0000
  12.750   1.3846   0.03436   0.02808  -0.0449   0.0260   1.0000
  13.000   1.3941   0.03582   0.02958  -0.0441   0.0245   1.0000
  13.250   1.4027   0.03739   0.03118  -0.0434   0.0231   1.0000
  13.500   1.4106   0.03907   0.03288  -0.0427   0.0219   1.0000
  13.750   1.4189   0.04074   0.03459  -0.0420   0.0211   1.0000
  14.000   1.4275   0.04240   0.03630  -0.0415   0.0200   1.0000
  14.250   1.4350   0.04422   0.03817  -0.0410   0.0193   1.0000
  14.500   1.4419   0.04613   0.04011  -0.0405   0.0185   1.0000
  14.750   1.4476   0.04822   0.04224  -0.0401   0.0176   1.0000
  15.000   1.4553   0.05012   0.04419  -0.0397   0.0171   1.0000
  15.250   1.4622   0.05213   0.04626  -0.0395   0.0165   1.0000
  15.500   1.4681   0.05431   0.04849  -0.0393   0.0159   1.0000
  15.750   1.4737   0.05654   0.05076  -0.0391   0.0153   1.0000
  16.000   1.4778   0.05899   0.05326  -0.0390   0.0147   1.0000
  16.250   1.4820   0.06146   0.05578  -0.0390   0.0143   1.0000
  16.500   1.4876   0.06381   0.05820  -0.0391   0.0139   1.0000
  16.750   1.4919   0.06637   0.06082  -0.0392   0.0135   1.0000
  17.000   1.4964   0.06892   0.06344  -0.0394   0.0131   1.0000
  17.250   1.4994   0.07172   0.06630  -0.0397   0.0126   1.0000
  17.500   1.5022   0.07457   0.06920  -0.0401   0.0122   1.0000
  17.750   1.5040   0.07759   0.07228  -0.0405   0.0119   1.0000
  18.000   1.5044   0.08086   0.07561  -0.0411   0.0115   1.0000
  18.250   1.5074   0.08379   0.07861  -0.0417   0.0113   1.0000
  18.500   1.5091   0.08697   0.08187  -0.0424   0.0110   1.0000
  18.750   1.5106   0.09018   0.08516  -0.0432   0.0108   1.0000
  19.000   1.5115   0.09352   0.08858  -0.0440   0.0105   1.0000
  19.250   1.5112   0.09708   0.09221  -0.0450   0.0102   1.0000
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