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FX 60-177 AIRFOIL (fx60177-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: FX 60-177 AIRFOIL (fx60177-il)
Reynolds number: 200,000
Max Cl/Cd: 49.25 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx60177-il-200000.txt
Download as CSV file: xf-fx60177-il-200000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.4669   0.10926   0.10606  -0.0512   1.0001   0.0249
 -13.250  -0.4590   0.10983   0.10670  -0.0491   1.0001   0.0253
 -13.000  -0.6353   0.08724   0.08332  -0.0677   1.0001   0.0238
 -12.750  -0.6566   0.08273   0.07876  -0.0679   1.0001   0.0236
 -12.500  -0.6803   0.07848   0.07443  -0.0677   1.0001   0.0234
 -12.250  -0.7046   0.07460   0.07045  -0.0668   1.0001   0.0232
 -12.000  -0.7291   0.07105   0.06681  -0.0653   1.0001   0.0229
 -11.750  -0.7539   0.06779   0.06343  -0.0633   1.0001   0.0227
 -11.500  -0.7791   0.06475   0.06026  -0.0606   1.0001   0.0224
 -11.250  -0.8051   0.06188   0.05724  -0.0573   1.0001   0.0221
 -11.000  -0.8789   0.05496   0.04941  -0.0517   0.9966   0.0199
 -10.750  -0.8812   0.05307   0.04720  -0.0511   0.9918   0.0196
 -10.500  -0.8735   0.04969   0.04361  -0.0509   0.9882   0.0195
 -10.250  -0.8622   0.04666   0.04031  -0.0511   0.9852   0.0193
 -10.000  -0.8487   0.04399   0.03735  -0.0510   0.9818   0.0192
  -9.750  -0.8353   0.04167   0.03475  -0.0501   0.9775   0.0192
  -9.500  -0.8141   0.03957   0.03236  -0.0502   0.9746   0.0193
  -9.250  -0.7882   0.03782   0.03035  -0.0508   0.9725   0.0195
  -9.000  -0.7664   0.03624   0.02862  -0.0500   0.9699   0.0198
  -8.750  -0.7492   0.03487   0.02726  -0.0484   0.9662   0.0204
  -8.500  -0.7261   0.03381   0.02619  -0.0483   0.9629   0.0212
  -8.250  -0.6988   0.03281   0.02514  -0.0490   0.9603   0.0224
  -8.000  -0.6690   0.03190   0.02410  -0.0500   0.9584   0.0242
  -7.750  -0.6656   0.03066   0.02293  -0.0469   0.9515   0.0257
  -7.500  -0.6407   0.02966   0.02188  -0.0476   0.9477   0.0300
  -7.250  -0.6111   0.02860   0.02083  -0.0496   0.9452   0.0372
  -7.000  -0.5976   0.02778   0.02004  -0.0484   0.9397   0.0428
  -6.750  -0.5750   0.02690   0.01917  -0.0490   0.9353   0.0504
  -6.500  -0.5434   0.02604   0.01834  -0.0511   0.9325   0.0625
  -6.250  -0.5075   0.02500   0.01743  -0.0543   0.9305   0.0852
  -6.000  -0.4854   0.02376   0.01659  -0.0554   0.9261   0.1411
  -5.750  -0.4392   0.02104   0.01522  -0.0639   0.9245   0.3720
  -5.500  -0.3981   0.02026   0.01514  -0.0680   0.9221   0.5087
  -5.250  -0.3650   0.02046   0.01556  -0.0688   0.9189   0.5726
  -5.000  -0.3271   0.02091   0.01600  -0.0703   0.9164   0.6142
  -4.750  -0.3073   0.02142   0.01649  -0.0684   0.9101   0.6327
  -4.500  -0.2775   0.02181   0.01679  -0.0684   0.9052   0.6472
  -4.250  -0.2439   0.02239   0.01729  -0.0687   0.9022   0.6617
  -3.750  -0.2083   0.02390   0.01876  -0.0629   0.8903   0.6795
  -3.500  -0.1802   0.02462   0.01944  -0.0612   0.8870   0.6856
  -3.250  -0.1593   0.02504   0.01979  -0.0597   0.8803   0.6947
  -3.000  -0.1409   0.02572   0.02046  -0.0564   0.8747   0.6989
  -2.750  -0.1022   0.02583   0.02047  -0.0584   0.8723   0.7092
  -2.500  -0.0895   0.02643   0.02107  -0.0546   0.8658   0.7120
  -2.250  -0.0680   0.02676   0.02136  -0.0526   0.8603   0.7160
  -2.000  -0.0230   0.02637   0.02086  -0.0567   0.8578   0.7250
  -1.750   0.0112   0.02633   0.02078  -0.0567   0.8557   0.7270
  -1.500   0.0194   0.02670   0.02115  -0.0526   0.8454   0.7308
  -1.250   0.0661   0.02623   0.02058  -0.0571   0.8429   0.7402
  -1.000   0.0987   0.02605   0.02038  -0.0567   0.8409   0.7421
  -0.750   0.1093   0.02628   0.02061  -0.0532   0.8308   0.7452
  -0.500   0.1461   0.02588   0.02018  -0.0544   0.8279   0.7491
  -0.250   0.1961   0.02516   0.01939  -0.0595   0.8263   0.7564
   0.000   0.2069   0.02535   0.01960  -0.0556   0.8173   0.7590
   0.250   0.2375   0.02500   0.01924  -0.0551   0.8136   0.7624
   0.500   0.2784   0.02432   0.01854  -0.0571   0.8116   0.7671
   0.750   0.3334   0.02328   0.01745  -0.0627   0.8106   0.7725
   1.000   0.3754   0.02250   0.01667  -0.0642   0.8093   0.7742
   1.250   0.3835   0.02247   0.01666  -0.0601   0.7976   0.7774
   1.500   0.4273   0.02176   0.01595  -0.0626   0.7955   0.7805
   1.750   0.4728   0.02112   0.01530  -0.0661   0.7916   0.7852
   2.000   0.4982   0.02073   0.01492  -0.0657   0.7821   0.7897
   2.250   0.5433   0.02009   0.01428  -0.0682   0.7786   0.7919
   2.500   0.5578   0.01989   0.01410  -0.0654   0.7669   0.7956
   2.750   0.6033   0.01934   0.01354  -0.0688   0.7601   0.7986
   3.000   0.6420   0.01891   0.01310  -0.0717   0.7487   0.8027
   3.250   0.6622   0.01860   0.01281  -0.0700   0.7353   0.8055
   3.500   0.6840   0.01834   0.01256  -0.0684   0.7215   0.8081
   3.750   0.7099   0.01810   0.01231  -0.0679   0.7063   0.8110
   4.000   0.7398   0.01787   0.01204  -0.0685   0.6888   0.8142
   4.250   0.7772   0.01771   0.01180  -0.0710   0.6690   0.8180
   4.500   0.7964   0.01761   0.01166  -0.0694   0.6476   0.8208
   4.750   0.8128   0.01759   0.01159  -0.0670   0.6248   0.8235
   5.000   0.8335   0.01765   0.01154  -0.0657   0.6011   0.8266
   5.250   0.8548   0.01779   0.01160  -0.0649   0.5759   0.8297
   5.500   0.8804   0.01803   0.01173  -0.0653   0.5501   0.8329
   5.750   0.9013   0.01830   0.01188  -0.0645   0.5254   0.8358
   6.000   0.9142   0.01858   0.01209  -0.0618   0.5016   0.8382
   6.250   0.9301   0.01894   0.01235  -0.0601   0.4779   0.8407
   6.500   0.9477   0.01935   0.01269  -0.0589   0.4540   0.8433
   6.750   0.9670   0.01982   0.01307  -0.0582   0.4307   0.8461
   7.000   0.9901   0.02039   0.01353  -0.0584   0.4093   0.8491
   7.250   1.0047   0.02082   0.01392  -0.0566   0.3899   0.8516
   7.500   1.0174   0.02126   0.01433  -0.0544   0.3713   0.8540
   7.750   1.0327   0.02180   0.01480  -0.0529   0.3534   0.8565
   8.000   1.0503   0.02238   0.01534  -0.0520   0.3366   0.8590
   8.250   1.0700   0.02299   0.01593  -0.0516   0.3205   0.8615
   8.500   1.0920   0.02368   0.01660  -0.0518   0.3054   0.8643
   8.750   1.1067   0.02423   0.01713  -0.0502   0.2928   0.8667
   9.000   1.1196   0.02484   0.01769  -0.0484   0.2809   0.8691
   9.250   1.1344   0.02549   0.01835  -0.0470   0.2682   0.8716
   9.500   1.1508   0.02616   0.01907  -0.0461   0.2557   0.8744
   9.750   1.1685   0.02694   0.01986  -0.0456   0.2439   0.8773
  10.000   1.1877   0.02785   0.02072  -0.0456   0.2333   0.8796
  10.250   1.2013   0.02853   0.02147  -0.0442   0.2237   0.8817
  10.500   1.2148   0.02928   0.02227  -0.0428   0.2148   0.8840
  10.750   1.2269   0.03013   0.02312  -0.0414   0.2058   0.8867
  11.000   1.2408   0.03099   0.02408  -0.0404   0.1959   0.8895
  11.250   1.2542   0.03206   0.02515  -0.0397   0.1867   0.8921
  11.500   1.2687   0.03321   0.02633  -0.0394   0.1773   0.8942
  11.750   1.2795   0.03422   0.02742  -0.0381   0.1688   0.8963
  12.000   1.2875   0.03538   0.02860  -0.0366   0.1608   0.8986
  12.250   1.2985   0.03648   0.02983  -0.0356   0.1523   0.9011
  12.500   1.3061   0.03794   0.03127  -0.0345   0.1446   0.9035
  12.750   1.3179   0.03925   0.03271  -0.0340   0.1361   0.9062
  13.000   1.3263   0.04099   0.03444  -0.0335   0.1294   0.9087
  13.250   1.3343   0.04232   0.03591  -0.0323   0.1228   0.9114
  13.500   1.3373   0.04413   0.03772  -0.0310   0.1172   0.9140
  13.750   1.3464   0.04569   0.03946  -0.0303   0.1111   0.9166
  14.000   1.3523   0.04766   0.04148  -0.0298   0.1055   0.9191
  14.250   1.3584   0.04977   0.04366  -0.0296   0.1000   0.9216
  14.500   1.3643   0.05193   0.04592  -0.0295   0.0942   0.9239
  14.750   1.3628   0.05444   0.04842  -0.0286   0.0896   0.9264
  15.000   1.3686   0.05647   0.05063  -0.0283   0.0846   0.9293
  15.250   1.3697   0.05916   0.05338  -0.0283   0.0801   0.9324
  15.500   1.3701   0.06209   0.05637  -0.0284   0.0764   0.9353
  15.750   1.3741   0.06456   0.05901  -0.0285   0.0725   0.9383
  16.000   1.3731   0.06744   0.06201  -0.0285   0.0693   0.9416
  16.250   1.3692   0.07093   0.06554  -0.0289   0.0666   0.9446
  16.500   1.3697   0.07409   0.06884  -0.0295   0.0641   0.9477
  16.750   1.3697   0.07734   0.07225  -0.0303   0.0610   0.9509
  17.000   1.3644   0.08097   0.07597  -0.0308   0.0585   0.9549
  17.250   1.3574   0.08512   0.08020  -0.0318   0.0565   0.9589
  17.500   1.3512   0.08923   0.08439  -0.0329   0.0547   0.9630
  17.750   1.3480   0.09268   0.08803  -0.0337   0.0530   0.9685
  18.000   1.3436   0.09661   0.09214  -0.0350   0.0509   0.9744
  18.250   1.3359   0.10106   0.09672  -0.0368   0.0486   0.9831
  18.500   1.3254   0.10631   0.10207  -0.0394   0.0464   0.9999
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