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FX 60-177 AIRFOIL (fx60177-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 60-177 AIRFOIL (fx60177-il)
Reynolds number: 200,000
Max Cl/Cd: 53.25 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx60177-il-200000-n5.txt
Download as CSV file: xf-fx60177-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 60-177 AIRFOIL                               
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.6487   0.09899   0.09462  -0.0676   1.0001   0.0079
 -15.250  -0.6861   0.08899   0.08434  -0.0720   1.0001   0.0078
 -15.000  -0.7123   0.08207   0.07722  -0.0742   1.0001   0.0077
 -14.750  -0.7333   0.07662   0.07158  -0.0753   1.0001   0.0077
 -14.500  -0.7494   0.07181   0.06660  -0.0764   0.9998   0.0077
 -14.250  -0.7542   0.06677   0.06136  -0.0796   0.9982   0.0077
 -14.000  -0.7561   0.06246   0.05685  -0.0822   0.9965   0.0077
 -13.750  -0.7555   0.05871   0.05292  -0.0845   0.9948   0.0078
 -13.500  -0.7537   0.05544   0.04948  -0.0860   0.9929   0.0078
 -13.250  -0.7503   0.05254   0.04642  -0.0872   0.9904   0.0079
 -13.000  -0.7441   0.04991   0.04363  -0.0883   0.9880   0.0080
 -12.750  -0.7358   0.04752   0.04109  -0.0894   0.9859   0.0081
 -12.500  -0.7250   0.04532   0.03872  -0.0906   0.9842   0.0082
 -12.250  -0.7167   0.04339   0.03667  -0.0906   0.9810   0.0083
 -12.000  -0.7069   0.04159   0.03474  -0.0907   0.9776   0.0085
 -11.750  -0.6944   0.03988   0.03290  -0.0911   0.9750   0.0087
 -11.500  -0.6792   0.03824   0.03113  -0.0917   0.9730   0.0089
 -11.250  -0.6645   0.03672   0.02949  -0.0921   0.9705   0.0092
 -11.000  -0.6569   0.03544   0.02810  -0.0908   0.9655   0.0094
 -10.750  -0.6427   0.03411   0.02663  -0.0907   0.9624   0.0097
 -10.500  -0.6255   0.03279   0.02524  -0.0912   0.9601   0.0101
 -10.250  -0.6050   0.03157   0.02395  -0.0922   0.9584   0.0107
 -10.000  -0.6024   0.03073   0.02305  -0.0892   0.9513   0.0112
  -9.750  -0.5867   0.02968   0.02191  -0.0890   0.9481   0.0120
  -9.500  -0.5673   0.02859   0.02075  -0.0894   0.9458   0.0131
  -9.250  -0.5575   0.02781   0.01991  -0.0876   0.9408   0.0143
  -9.000  -0.5484   0.02708   0.01910  -0.0855   0.9352   0.0158
  -8.750  -0.5303   0.02621   0.01820  -0.0853   0.9322   0.0179
  -8.500  -0.5077   0.02539   0.01734  -0.0857   0.9302   0.0208
  -8.250  -0.5133   0.02502   0.01694  -0.0805   0.9212   0.0224
  -8.000  -0.4925   0.02430   0.01621  -0.0805   0.9181   0.0261
  -7.750  -0.4673   0.02357   0.01547  -0.0812   0.9161   0.0316
  -7.500  -0.4629   0.02318   0.01506  -0.0779   0.9091   0.0357
  -7.250  -0.4433   0.02252   0.01440  -0.0775   0.9052   0.0419
  -7.000  -0.4176   0.02178   0.01367  -0.0783   0.9029   0.0510
  -6.500  -0.3857   0.02049   0.01256  -0.0764   0.8937   0.0850
  -6.250  -0.3635   0.01961   0.01190  -0.0768   0.8902   0.1248
  -6.000  -0.3354   0.01860   0.01115  -0.0784   0.8881   0.1813
  -5.750  -0.3035   0.01715   0.01022  -0.0815   0.8866   0.2813
  -5.500  -0.2653   0.01575   0.00944  -0.0858   0.8856   0.4125
  -5.250  -0.2485   0.01550   0.00946  -0.0846   0.8781   0.4727
  -5.000  -0.2168   0.01527   0.00938  -0.0856   0.8757   0.5188
  -4.750  -0.1850   0.01520   0.00943  -0.0863   0.8738   0.5609
  -4.500  -0.1527   0.01526   0.00953  -0.0868   0.8723   0.5917
  -4.250  -0.1167   0.01525   0.00947  -0.0884   0.8711   0.6142
  -4.000  -0.0996   0.01556   0.00976  -0.0864   0.8647   0.6267
  -3.750  -0.0719   0.01569   0.00985  -0.0860   0.8610   0.6377
  -3.500  -0.0378   0.01567   0.00977  -0.0871   0.8587   0.6488
  -3.250  -0.0027   0.01565   0.00967  -0.0882   0.8569   0.6569
  -3.000   0.0357   0.01551   0.00945  -0.0903   0.8555   0.6634
  -2.750   0.0477   0.01577   0.00971  -0.0871   0.8465   0.6676
  -2.500   0.0832   0.01561   0.00947  -0.0887   0.8437   0.6734
  -2.250   0.1197   0.01548   0.00927  -0.0904   0.8417   0.6786
  -2.000   0.1544   0.01546   0.00921  -0.0914   0.8400   0.6818
  -1.750   0.1685   0.01564   0.00938  -0.0889   0.8312   0.6861
  -1.500   0.2082   0.01534   0.00900  -0.0916   0.8280   0.6918
  -1.250   0.2454   0.01517   0.00879  -0.0932   0.8252   0.6944
  -1.000   0.2608   0.01534   0.00897  -0.0906   0.8165   0.6972
  -0.750   0.2936   0.01524   0.00885  -0.0913   0.8120   0.7007
  -0.500   0.3353   0.01502   0.00857  -0.0942   0.8091   0.7050
  -0.250   0.3566   0.01500   0.00854  -0.0933   0.7998   0.7094
   0.000   0.3912   0.01487   0.00839  -0.0944   0.7948   0.7111
   0.250   0.4118   0.01492   0.00845  -0.0928   0.7852   0.7135
   0.500   0.4496   0.01475   0.00824  -0.0946   0.7783   0.7162
   0.750   0.4743   0.01472   0.00820  -0.0942   0.7670   0.7206
   1.000   0.5105   0.01456   0.00799  -0.0961   0.7578   0.7248
   1.250   0.5397   0.01452   0.00795  -0.0963   0.7482   0.7263
   1.500   0.5636   0.01454   0.00796  -0.0954   0.7362   0.7281
   1.750   0.5910   0.01453   0.00794  -0.0953   0.7234   0.7303
   2.000   0.6202   0.01451   0.00789  -0.0956   0.7098   0.7329
   2.250   0.6511   0.01448   0.00781  -0.0965   0.6947   0.7360
   2.500   0.6863   0.01441   0.00767  -0.0984   0.6767   0.7400
   2.750   0.7101   0.01451   0.00771  -0.0975   0.6572   0.7415
   3.000   0.7332   0.01464   0.00778  -0.0965   0.6354   0.7433
   3.250   0.7554   0.01481   0.00787  -0.0954   0.6118   0.7454
   3.500   0.7778   0.01502   0.00796  -0.0944   0.5879   0.7477
   3.750   0.7994   0.01525   0.00810  -0.0935   0.5613   0.7504
   4.000   0.8227   0.01554   0.00824  -0.0931   0.5353   0.7538
   4.250   0.8446   0.01586   0.00845  -0.0924   0.5104   0.7565
   4.500   0.8618   0.01625   0.00875  -0.0906   0.4871   0.7580
   4.750   0.8795   0.01665   0.00908  -0.0889   0.4648   0.7596
   5.000   0.8979   0.01705   0.00942  -0.0875   0.4440   0.7615
   5.250   0.9169   0.01746   0.00978  -0.0862   0.4244   0.7637
   5.500   0.9367   0.01790   0.01016  -0.0852   0.4062   0.7664
   5.750   0.9577   0.01835   0.01055  -0.0846   0.3864   0.7693
   6.000   0.9792   0.01885   0.01096  -0.0842   0.3663   0.7721
   6.250   0.9948   0.01936   0.01144  -0.0824   0.3492   0.7735
   6.500   1.0115   0.01987   0.01192  -0.0809   0.3335   0.7751
   6.750   1.0295   0.02036   0.01241  -0.0796   0.3188   0.7769
   7.000   1.0472   0.02088   0.01293  -0.0783   0.3045   0.7791
   7.250   1.0649   0.02146   0.01348  -0.0772   0.2901   0.7816
   7.500   1.0836   0.02206   0.01405  -0.0763   0.2758   0.7842
   7.750   1.1035   0.02268   0.01464  -0.0759   0.2622   0.7869
   8.000   1.1206   0.02332   0.01528  -0.0747   0.2503   0.7889
   8.250   1.1368   0.02390   0.01590  -0.0733   0.2403   0.7906
   8.500   1.1528   0.02455   0.01657  -0.0719   0.2313   0.7924
   8.750   1.1684   0.02527   0.01729  -0.0706   0.2214   0.7943
   9.000   1.1858   0.02592   0.01800  -0.0697   0.2103   0.7964
   9.250   1.2022   0.02668   0.01878  -0.0687   0.1997   0.7988
   9.500   1.2180   0.02754   0.01962  -0.0678   0.1896   0.8014
   9.750   1.2359   0.02834   0.02045  -0.0672   0.1809   0.8037
  10.000   1.2478   0.02925   0.02138  -0.0656   0.1742   0.8052
  10.250   1.2634   0.02999   0.02223  -0.0644   0.1666   0.8068
  10.500   1.2753   0.03099   0.02325  -0.0630   0.1586   0.8085
  10.750   1.2897   0.03188   0.02421  -0.0619   0.1489   0.8104
  11.000   1.3022   0.03295   0.02529  -0.0607   0.1398   0.8124
  11.250   1.3128   0.03419   0.02653  -0.0595   0.1316   0.8145
  11.500   1.3267   0.03529   0.02769  -0.0588   0.1235   0.8169
  11.750   1.3372   0.03668   0.02910  -0.0578   0.1158   0.8192
  12.000   1.3477   0.03784   0.03034  -0.0565   0.1070   0.8209
  12.250   1.3556   0.03926   0.03179  -0.0551   0.0993   0.8226
  12.500   1.3632   0.04078   0.03335  -0.0538   0.0925   0.8244
  12.750   1.3716   0.04232   0.03495  -0.0528   0.0874   0.8263
  13.000   1.3804   0.04390   0.03662  -0.0519   0.0821   0.8283
  13.250   1.3865   0.04578   0.03856  -0.0510   0.0776   0.8303
  13.500   1.3957   0.04748   0.04038  -0.0504   0.0732   0.8324
  13.750   1.4023   0.04950   0.04246  -0.0499   0.0684   0.8344
  14.000   1.4056   0.05165   0.04469  -0.0490   0.0642   0.8360
  14.250   1.4079   0.05395   0.04705  -0.0481   0.0593   0.8378
  14.500   1.4075   0.05666   0.04981  -0.0474   0.0554   0.8397
  14.750   1.4113   0.05900   0.05228  -0.0470   0.0515   0.8418
  15.000   1.4128   0.06172   0.05509  -0.0467   0.0478   0.8439
  15.250   1.4123   0.06478   0.05823  -0.0467   0.0442   0.8459
  15.500   1.4135   0.06777   0.06133  -0.0469   0.0408   0.8479
  15.750   1.4121   0.07120   0.06486  -0.0473   0.0379   0.8498
  16.000   1.4088   0.07467   0.06845  -0.0475   0.0358   0.8514
  16.250   1.4050   0.07831   0.07222  -0.0479   0.0337   0.8531
  16.500   1.3992   0.08235   0.07637  -0.0486   0.0318   0.8549
  16.750   1.3904   0.08696   0.08107  -0.0496   0.0297   0.8567
  17.000   1.3860   0.09106   0.08533  -0.0507   0.0276   0.8586
  17.250   1.3792   0.09562   0.09003  -0.0521   0.0256   0.8604
  17.500   1.3707   0.10057   0.09510  -0.0539   0.0241   0.8621
  17.750   1.3636   0.10541   0.10010  -0.0558   0.0225   0.8638
  18.000   1.3557   0.11041   0.10526  -0.0578   0.0201   0.8654
  18.250   1.3433   0.11608   0.11105  -0.0602   0.0175   0.8668
  18.750   1.3139   0.12858   0.12380  -0.0661   0.0139   0.8698
  19.000   1.2976   0.13539   0.13072  -0.0697   0.0124   0.8714
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