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FX 60-177 AIRFOIL (fx60177-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: FX 60-177 AIRFOIL (fx60177-il)
Reynolds number: 100,000
Max Cl/Cd: 37.32 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx60177-il-100000-n5.txt
Download as CSV file: xf-fx60177-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.5769   0.10180   0.09624  -0.0666   1.0001   0.0157
 -14.000  -0.6026   0.09440   0.08874  -0.0695   1.0001   0.0155
 -13.750  -0.6279   0.08795   0.08217  -0.0717   1.0001   0.0154
 -13.500  -0.6524   0.08234   0.07643  -0.0729   1.0001   0.0153
 -13.250  -0.6760   0.07748   0.07141  -0.0733   1.0001   0.0153
 -13.000  -0.6984   0.07322   0.06699  -0.0730   1.0001   0.0152
 -12.750  -0.7195   0.06944   0.06304  -0.0720   1.0001   0.0152
 -12.500  -0.7391   0.06605   0.05947  -0.0704   1.0001   0.0152
 -12.250  -0.7568   0.06301   0.05625  -0.0684   1.0001   0.0153
 -12.000  -0.7728   0.06024   0.05329  -0.0661   1.0001   0.0153
 -11.750  -0.7804   0.05716   0.04995  -0.0651   0.9988   0.0155
 -11.500  -0.7782   0.05396   0.04640  -0.0654   0.9960   0.0158
 -11.250  -0.7704   0.05156   0.04384  -0.0658   0.9934   0.0161
 -11.000  -0.7617   0.04955   0.04170  -0.0658   0.9899   0.0165
 -10.750  -0.7510   0.04772   0.03973  -0.0659   0.9867   0.0170
 -10.500  -0.7378   0.04601   0.03785  -0.0661   0.9842   0.0179
 -10.250  -0.7259   0.04436   0.03596  -0.0653   0.9806   0.0190
 -10.000  -0.7131   0.04286   0.03435  -0.0647   0.9768   0.0202
  -9.750  -0.6988   0.04165   0.03308  -0.0647   0.9735   0.0216
  -9.500  -0.6814   0.04038   0.03164  -0.0645   0.9707   0.0236
  -9.250  -0.6736   0.03922   0.03043  -0.0626   0.9655   0.0251
  -9.000  -0.6597   0.03815   0.02931  -0.0620   0.9616   0.0273
  -8.750  -0.6411   0.03712   0.02817  -0.0619   0.9587   0.0307
  -8.500  -0.6368   0.03638   0.02741  -0.0594   0.9524   0.0338
  -8.250  -0.6212   0.03547   0.02643  -0.0588   0.9484   0.0384
  -8.000  -0.6004   0.03456   0.02546  -0.0591   0.9454   0.0437
  -7.750  -0.5913   0.03359   0.02449  -0.0572   0.9401   0.0478
  -7.500  -0.5774   0.03267   0.02351  -0.0561   0.9352   0.0527
  -7.250  -0.5584   0.03157   0.02238  -0.0561   0.9319   0.0582
  -7.000  -0.5342   0.03061   0.02137  -0.0569   0.9293   0.0678
  -6.750  -0.5279   0.02980   0.02060  -0.0543   0.9224   0.0768
  -6.500  -0.5063   0.02884   0.01974  -0.0545   0.9186   0.0957
  -6.250  -0.4807   0.02774   0.01890  -0.0557   0.9159   0.1374
  -6.000  -0.4669   0.02660   0.01815  -0.0549   0.9103   0.2006
  -5.750  -0.4462   0.02498   0.01732  -0.0562   0.9061   0.3274
  -5.500  -0.4189   0.02420   0.01720  -0.0571   0.9032   0.4474
  -5.250  -0.3905   0.02444   0.01771  -0.0564   0.9009   0.5129
  -5.000  -0.3746   0.02480   0.01813  -0.0538   0.8948   0.5503
  -4.750  -0.3508   0.02539   0.01870  -0.0523   0.8905   0.5854
  -4.500  -0.3200   0.02593   0.01914  -0.0524   0.8876   0.6153
  -4.250  -0.2875   0.02648   0.01957  -0.0526   0.8854   0.6324
  -4.000  -0.2722   0.02681   0.01979  -0.0505   0.8779   0.6461
  -3.750  -0.2472   0.02753   0.02044  -0.0486   0.8737   0.6551
  -3.500  -0.2143   0.02793   0.02071  -0.0489   0.8709   0.6657
  -3.250  -0.1953   0.02803   0.02069  -0.0479   0.8635   0.6773
  -3.000  -0.1705   0.02841   0.02100  -0.0465   0.8592   0.6813
  -2.750  -0.1374   0.02843   0.02089  -0.0475   0.8564   0.6879
  -2.500  -0.1165   0.02845   0.02081  -0.0468   0.8494   0.6949
  -2.250  -0.0909   0.02861   0.02090  -0.0459   0.8442   0.6993
  -2.000  -0.0516   0.02824   0.02040  -0.0490   0.8413   0.7085
  -1.750  -0.0356   0.02851   0.02063  -0.0465   0.8339   0.7115
  -1.500  -0.0097   0.02856   0.02062  -0.0460   0.8289   0.7155
  -1.250   0.0266   0.02830   0.02028  -0.0481   0.8260   0.7220
  -1.000   0.0467   0.02841   0.02035  -0.0470   0.8186   0.7268
  -0.750   0.0731   0.02837   0.02027  -0.0463   0.8130   0.7308
  -0.500   0.1105   0.02800   0.01983  -0.0481   0.8099   0.7362
  -0.250   0.1319   0.02801   0.01980  -0.0478   0.8006   0.7414
   0.000   0.1616   0.02779   0.01956  -0.0478   0.7963   0.7442
   0.250   0.1971   0.02737   0.01911  -0.0488   0.7935   0.7476
   0.500   0.2178   0.02741   0.01913  -0.0483   0.7826   0.7533
   0.750   0.2551   0.02686   0.01855  -0.0499   0.7791   0.7574
   1.000   0.2709   0.02700   0.01871  -0.0477   0.7689   0.7607
   1.250   0.3035   0.02659   0.01829  -0.0483   0.7646   0.7641
   1.500   0.3303   0.02644   0.01813  -0.0486   0.7556   0.7683
   1.750   0.3692   0.02589   0.01757  -0.0510   0.7495   0.7723
   2.000   0.3907   0.02575   0.01746  -0.0496   0.7399   0.7747
   2.250   0.4220   0.02528   0.01700  -0.0498   0.7329   0.7773
   2.500   0.4457   0.02515   0.01689  -0.0492   0.7213   0.7805
   2.750   0.4833   0.02457   0.01631  -0.0508   0.7137   0.7839
   3.250   0.5374   0.02426   0.01604  -0.0510   0.6891   0.7904
   3.500   0.5651   0.02399   0.01581  -0.0508   0.6774   0.7930
   3.750   0.5968   0.02363   0.01545  -0.0513   0.6643   0.7956
   4.000   0.6282   0.02338   0.01520  -0.0520   0.6485   0.7987
   4.250   0.6614   0.02319   0.01499  -0.0534   0.6307   0.8021
   4.500   0.6933   0.02298   0.01476  -0.0542   0.6125   0.8046
   4.750   0.7214   0.02283   0.01458  -0.0540   0.5934   0.8066
   5.000   0.7491   0.02277   0.01447  -0.0540   0.5732   0.8087
   5.250   0.7753   0.02282   0.01449  -0.0539   0.5515   0.8113
   5.500   0.8025   0.02294   0.01453  -0.0541   0.5290   0.8143
   5.750   0.8301   0.02316   0.01466  -0.0546   0.5053   0.8174
   6.000   0.8535   0.02347   0.01490  -0.0543   0.4817   0.8199
   6.250   0.8726   0.02378   0.01515  -0.0530   0.4607   0.8220
   6.500   0.8912   0.02416   0.01549  -0.0518   0.4405   0.8245
   6.750   0.9104   0.02457   0.01589  -0.0509   0.4211   0.8273
   7.000   0.9315   0.02503   0.01631  -0.0503   0.4034   0.8303
   7.250   0.9538   0.02556   0.01682  -0.0503   0.3854   0.8333
   7.500   0.9723   0.02610   0.01733  -0.0494   0.3678   0.8357
   7.750   0.9871   0.02663   0.01785  -0.0477   0.3517   0.8382
   8.000   1.0030   0.02721   0.01842  -0.0464   0.3361   0.8409
   8.250   1.0206   0.02784   0.01906  -0.0455   0.3215   0.8437
   8.500   1.0395   0.02851   0.01974  -0.0449   0.3077   0.8463
   8.750   1.0592   0.02924   0.02049  -0.0447   0.2946   0.8490
   9.000   1.0742   0.02996   0.02120  -0.0434   0.2830   0.8514
   9.250   1.0881   0.03065   0.02196  -0.0420   0.2708   0.8540
   9.500   1.1031   0.03141   0.02278  -0.0408   0.2596   0.8566
   9.750   1.1182   0.03226   0.02365  -0.0399   0.2490   0.8591
  10.000   1.1337   0.03318   0.02461  -0.0392   0.2382   0.8616
  10.250   1.1506   0.03413   0.02564  -0.0388   0.2280   0.8640
  10.500   1.1630   0.03512   0.02662  -0.0376   0.2197   0.8662
  10.750   1.1759   0.03599   0.02766  -0.0363   0.2106   0.8687
  11.000   1.1870   0.03704   0.02877  -0.0350   0.2023   0.8715
  11.250   1.1987   0.03816   0.02999  -0.0340   0.1932   0.8744
  11.500   1.2106   0.03939   0.03129  -0.0332   0.1850   0.8771
  11.750   1.2219   0.04077   0.03272  -0.0326   0.1771   0.8796
  12.000   1.2306   0.04204   0.03410  -0.0313   0.1698   0.8819
  12.250   1.2382   0.04343   0.03559  -0.0301   0.1624   0.8842
  12.500   1.2462   0.04491   0.03719  -0.0290   0.1555   0.8868
  12.750   1.2538   0.04650   0.03892  -0.0282   0.1485   0.8896
  13.000   1.2610   0.04827   0.04075  -0.0275   0.1427   0.8924
  13.250   1.2683   0.05007   0.04272  -0.0270   0.1364   0.8952
  13.500   1.2702   0.05200   0.04468  -0.0258   0.1316   0.8980
  13.750   1.2748   0.05395   0.04681  -0.0250   0.1257   0.9008
  14.000   1.2774   0.05622   0.04920  -0.0244   0.1201   0.9036
  14.250   1.2790   0.05872   0.05175  -0.0241   0.1152   0.9063
  14.750   1.2804   0.06395   0.05732  -0.0236   0.1051   0.9121
  15.000   1.2790   0.06678   0.06025  -0.0234   0.1011   0.9153
  15.250   1.2783   0.06981   0.06348  -0.0236   0.0965   0.9185
  15.500   1.2750   0.07330   0.06706  -0.0242   0.0927   0.9216
  15.750   1.2706   0.07685   0.07066  -0.0247   0.0895   0.9245
  16.000   1.2673   0.08033   0.07437  -0.0252   0.0859   0.9276
  16.250   1.2622   0.08421   0.07842  -0.0261   0.0827   0.9309
  16.500   1.2561   0.08838   0.08271  -0.0273   0.0800   0.9344
  16.750   1.2494   0.09260   0.08698  -0.0287   0.0775   0.9379
  17.000   1.2419   0.09695   0.09156  -0.0299   0.0749   0.9420
  17.250   1.2338   0.10163   0.09644  -0.0317   0.0725   0.9463
  17.750   1.2161   0.11138   0.10648  -0.0358   0.0684   0.9559
  18.000   1.2084   0.11615   0.11133  -0.0382   0.0664   0.9621
  18.250   1.1985   0.12138   0.11672  -0.0409   0.0646   0.9703
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