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FX 60-160 AIRFOIL (fx60160-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 60-160 AIRFOIL (fx60160-il)
Reynolds number: 1,000,000
Max Cl/Cd: 116.67 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx60160-il-1000000.txt
Download as CSV file: xf-fx60160-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 60-160 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.8351   0.08983   0.08743  -0.0749   1.0000   0.0135
 -17.750  -0.8714   0.07975   0.07719  -0.0806   1.0000   0.0134
 -17.500  -0.9025   0.07127   0.06854  -0.0853   1.0000   0.0135
 -17.250  -0.9279   0.06427   0.06139  -0.0889   1.0000   0.0136
 -17.000  -0.9456   0.05885   0.05585  -0.0914   1.0000   0.0136
 -16.750  -0.9623   0.05396   0.05086  -0.0933   1.0000   0.0139
 -16.500  -0.9735   0.05015   0.04696  -0.0944   1.0000   0.0140
 -16.250  -0.9779   0.04745   0.04420  -0.0947   1.0000   0.0142
 -16.000  -0.9823   0.04504   0.04174  -0.0945   1.0000   0.0144
 -15.750  -0.9882   0.04271   0.03934  -0.0939   1.0000   0.0145
 -15.500  -0.9928   0.04072   0.03729  -0.0930   1.0000   0.0147
 -15.250  -0.9921   0.03933   0.03587  -0.0918   1.0000   0.0149
 -15.000  -0.9994   0.03738   0.03384  -0.0902   1.0000   0.0150
 -14.750  -0.9993   0.03615   0.03257  -0.0887   1.0000   0.0153
 -14.500  -0.9848   0.03417   0.03049  -0.0908   0.9989   0.0156
 -14.250  -0.9631   0.03287   0.02911  -0.0930   0.9976   0.0161
 -14.000  -0.9412   0.03152   0.02767  -0.0953   0.9960   0.0164
 -13.750  -0.9187   0.03014   0.02618  -0.0976   0.9944   0.0166
 -13.500  -0.9089   0.02767   0.02361  -0.0995   0.9918   0.0173
 -13.250  -0.8875   0.02654   0.02244  -0.1012   0.9892   0.0177
 -13.000  -0.8620   0.02559   0.02147  -0.1033   0.9870   0.0181
 -12.750  -0.8343   0.02472   0.02056  -0.1057   0.9852   0.0186
 -12.500  -0.8062   0.02366   0.01941  -0.1083   0.9836   0.0191
 -12.250  -0.7755   0.02281   0.01849  -0.1110   0.9824   0.0197
 -12.000  -0.7576   0.02191   0.01750  -0.1113   0.9774   0.0200
 -11.750  -0.7290   0.02124   0.01676  -0.1134   0.9746   0.0203
 -11.500  -0.7038   0.01954   0.01497  -0.1156   0.9723   0.0213
 -11.250  -0.6699   0.01900   0.01442  -0.1182   0.9706   0.0219
 -11.000  -0.6416   0.01843   0.01382  -0.1195   0.9672   0.0224
 -10.750  -0.6173   0.01788   0.01321  -0.1199   0.9616   0.0230
 -10.500  -0.5873   0.01735   0.01262  -0.1213   0.9576   0.0237
 -10.250  -0.5606   0.01690   0.01211  -0.1219   0.9520   0.0242
 -10.000  -0.5374   0.01664   0.01178  -0.1216   0.9442   0.0246
  -9.750  -0.5190   0.01546   0.01050  -0.1209   0.9361   0.0255
  -9.500  -0.4974   0.01495   0.00996  -0.1204   0.9263   0.0261
  -9.250  -0.4759   0.01461   0.00959  -0.1197   0.9145   0.0267
  -9.000  -0.4526   0.01430   0.00922  -0.1192   0.9013   0.0274
  -8.750  -0.4298   0.01394   0.00878  -0.1187   0.8852   0.0281
  -8.500  -0.4075   0.01360   0.00833  -0.1180   0.8678   0.0287
  -8.250  -0.3850   0.01334   0.00796  -0.1173   0.8510   0.0293
  -8.000  -0.3613   0.01322   0.00773  -0.1168   0.8365   0.0298
  -7.750  -0.3433   0.01252   0.00692  -0.1155   0.8238   0.0306
  -7.500  -0.3224   0.01209   0.00643  -0.1147   0.8135   0.0316
  -7.250  -0.2990   0.01183   0.00612  -0.1142   0.8041   0.0323
  -7.000  -0.2747   0.01161   0.00585  -0.1138   0.7962   0.0332
  -6.750  -0.2500   0.01141   0.00559  -0.1134   0.7885   0.0341
  -6.500  -0.2250   0.01120   0.00534  -0.1131   0.7821   0.0351
  -6.250  -0.1996   0.01101   0.00510  -0.1129   0.7757   0.0358
  -6.000  -0.1758   0.01069   0.00469  -0.1125   0.7695   0.0366
  -5.750  -0.1517   0.01027   0.00426  -0.1121   0.7641   0.0384
  -5.500  -0.1258   0.01008   0.00405  -0.1120   0.7586   0.0398
  -5.250  -0.0996   0.00995   0.00386  -0.1118   0.7533   0.0414
  -5.000  -0.0728   0.00980   0.00370  -0.1118   0.7487   0.0428
  -4.750  -0.0462   0.00965   0.00351  -0.1118   0.7438   0.0439
  -4.500  -0.0209   0.00935   0.00316  -0.1115   0.7389   0.0471
  -4.250   0.0059   0.00920   0.00299  -0.1115   0.7344   0.0495
  -4.000   0.0331   0.00907   0.00285  -0.1116   0.7299   0.0520
  -3.750   0.0598   0.00890   0.00265  -0.1115   0.7252   0.0560
  -3.500   0.0865   0.00877   0.00250  -0.1114   0.7205   0.0610
  -3.250   0.1138   0.00862   0.00235  -0.1115   0.7162   0.0670
  -3.000   0.1402   0.00838   0.00220  -0.1114   0.7115   0.0901
  -2.750   0.1605   0.00733   0.00183  -0.1109   0.7070   0.2995
  -2.500   0.1840   0.00669   0.00164  -0.1107   0.7028   0.4306
  -2.250   0.2102   0.00641   0.00157  -0.1106   0.6986   0.5015
  -2.000   0.2373   0.00632   0.00156  -0.1105   0.6942   0.5369
  -1.750   0.2648   0.00631   0.00156  -0.1105   0.6898   0.5636
  -1.500   0.2929   0.00631   0.00158  -0.1106   0.6858   0.5797
  -1.250   0.3210   0.00632   0.00160  -0.1107   0.6816   0.5933
  -1.000   0.3489   0.00635   0.00163  -0.1107   0.6772   0.6050
  -0.750   0.3768   0.00642   0.00166  -0.1108   0.6727   0.6135
  -0.500   0.4051   0.00644   0.00170  -0.1109   0.6686   0.6216
  -0.250   0.4332   0.00647   0.00171  -0.1110   0.6641   0.6268
   0.000   0.4608   0.00653   0.00177  -0.1110   0.6596   0.6332
   0.250   0.4889   0.00663   0.00183  -0.1111   0.6553   0.6409
   0.500   0.5168   0.00664   0.00187  -0.1111   0.6507   0.6459
   0.750   0.5445   0.00669   0.00191  -0.1111   0.6459   0.6491
   1.000   0.5719   0.00677   0.00196  -0.1111   0.6411   0.6529
   1.250   0.6001   0.00681   0.00200  -0.1112   0.6368   0.6564
   1.500   0.6276   0.00683   0.00203  -0.1112   0.6316   0.6597
   1.750   0.6545   0.00690   0.00208  -0.1111   0.6263   0.6627
   2.000   0.6822   0.00694   0.00214  -0.1112   0.6212   0.6657
   2.250   0.7090   0.00700   0.00219  -0.1110   0.6139   0.6689
   2.500   0.7356   0.00708   0.00225  -0.1108   0.6061   0.6719
   2.750   0.7617   0.00714   0.00229  -0.1105   0.5970   0.6748
   3.000   0.7874   0.00720   0.00235  -0.1101   0.5862   0.6780
   3.250   0.8123   0.00730   0.00243  -0.1096   0.5732   0.6806
   3.500   0.8370   0.00741   0.00251  -0.1090   0.5606   0.6833
   3.750   0.8620   0.00753   0.00260  -0.1086   0.5491   0.6859
   4.000   0.8870   0.00765   0.00270  -0.1081   0.5364   0.6882
   4.250   0.9106   0.00781   0.00280  -0.1073   0.5205   0.6903
   4.500   0.9322   0.00799   0.00293  -0.1062   0.5008   0.6927
   4.750   0.9529   0.00824   0.00309  -0.1049   0.4749   0.6949
   5.000   0.9718   0.00856   0.00330  -0.1033   0.4464   0.6973
   5.250   0.9905   0.00888   0.00351  -0.1017   0.4211   0.6997
   5.500   1.0082   0.00924   0.00375  -0.0998   0.3939   0.7020
   5.750   1.0217   0.00966   0.00402  -0.0972   0.3613   0.7041
   6.000   1.0326   0.01014   0.00432  -0.0941   0.3227   0.7062
   6.250   1.0352   0.01095   0.00483  -0.0895   0.2626   0.7089
   6.500   1.0298   0.01211   0.00560  -0.0837   0.1869   0.7112
   6.750   1.0198   0.01353   0.00657  -0.0773   0.1004   0.7136
   7.000   1.0278   0.01426   0.00718  -0.0741   0.0753   0.7160
   7.250   1.0424   0.01474   0.00764  -0.0721   0.0653   0.7185
   7.500   1.0571   0.01523   0.00811  -0.0701   0.0580   0.7206
   7.750   1.0726   0.01567   0.00855  -0.0683   0.0536   0.7230
   8.000   1.0859   0.01622   0.00910  -0.0662   0.0489   0.7256
   8.250   1.1026   0.01663   0.00956  -0.0646   0.0475   0.7281
   8.500   1.1183   0.01710   0.01006  -0.0630   0.0457   0.7306
   8.750   1.1326   0.01766   0.01061  -0.0612   0.0433   0.7333
   9.000   1.1441   0.01838   0.01135  -0.0591   0.0410   0.7357
   9.250   1.1578   0.01899   0.01202  -0.0573   0.0401   0.7384
   9.500   1.1726   0.01955   0.01263  -0.0558   0.0396   0.7411
   9.750   1.1876   0.02013   0.01326  -0.0544   0.0388   0.7440
  10.000   1.2011   0.02081   0.01399  -0.0528   0.0379   0.7470
  10.250   1.2152   0.02149   0.01469  -0.0514   0.0367   0.7501
  10.500   1.2277   0.02228   0.01551  -0.0498   0.0359   0.7529
  10.750   1.2386   0.02317   0.01645  -0.0482   0.0351   0.7564
  11.000   1.2471   0.02425   0.01759  -0.0463   0.0341   0.7599
  11.250   1.2535   0.02552   0.01894  -0.0444   0.0332   0.7638
  11.500   1.2680   0.02630   0.01977  -0.0433   0.0328   0.7678
  11.750   1.2826   0.02706   0.02059  -0.0424   0.0321   0.7722
  12.000   1.2941   0.02806   0.02166  -0.0411   0.0317   0.7770
  12.250   1.3077   0.02894   0.02258  -0.0402   0.0307   0.7824
  12.500   1.3194   0.02996   0.02367  -0.0391   0.0300   0.7888
  12.750   1.3304   0.03105   0.02480  -0.0380   0.0290   0.7970
  13.000   1.3384   0.03238   0.02621  -0.0368   0.0281   0.8080
  13.250   1.3410   0.03413   0.02808  -0.0351   0.0272   0.8257
  13.500   1.3745   0.03468   0.02897  -0.0380   0.0264   0.9282
  13.750   1.4010   0.03571   0.03004  -0.0399   0.0249   1.0000
  14.000   1.4131   0.03696   0.03129  -0.0393   0.0236   1.0000
  14.250   1.4231   0.03839   0.03273  -0.0387   0.0219   1.0000
  14.500   1.4364   0.03955   0.03391  -0.0382   0.0194   1.0000
  14.750   1.4442   0.04121   0.03556  -0.0375   0.0157   1.0000
  15.000   1.4487   0.04323   0.03756  -0.0367   0.0130   1.0000
  15.250   1.4505   0.04554   0.03989  -0.0359   0.0112   1.0000
  15.500   1.4539   0.04776   0.04217  -0.0352   0.0106   1.0000
  15.750   1.4543   0.05032   0.04476  -0.0346   0.0097   1.0000
  16.000   1.4546   0.05298   0.04748  -0.0340   0.0092   1.0000
  16.250   1.4588   0.05528   0.04986  -0.0337   0.0090   1.0000
  16.500   1.4609   0.05785   0.05251  -0.0334   0.0088   1.0000
  16.750   1.4628   0.06048   0.05522  -0.0332   0.0085   1.0000
  17.000   1.4636   0.06329   0.05810  -0.0331   0.0083   1.0000
  17.250   1.4637   0.06624   0.06113  -0.0331   0.0081   1.0000
  17.500   1.4636   0.06929   0.06426  -0.0332   0.0080   1.0000
  17.750   1.4613   0.07265   0.06769  -0.0334   0.0077   1.0000
  18.000   1.4577   0.07627   0.07140  -0.0338   0.0076   1.0000
  18.250   1.4504   0.08048   0.07570  -0.0344   0.0073   1.0000
  18.500   1.4463   0.08435   0.07967  -0.0351   0.0072   1.0000
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