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UA(2)-180 smoothed (ua2-180sm-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: UA(2)-180 smoothed (ua2-180sm-il)
Reynolds number: 500,000
Max Cl/Cd: 106.82 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ua2-180sm-il-500000-n5.txt
Download as CSV file: xf-ua2-180sm-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: UA(2)-180 smoothed                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000   0.0717   0.08944   0.08460  -0.0974   0.5118   0.0132
  -9.750   0.0746   0.08636   0.08153  -0.0985   0.5113   0.0131
  -9.500   0.0752   0.08293   0.07812  -0.0998   0.5107   0.0133
  -9.250   0.0752   0.07949   0.07470  -0.1011   0.5102   0.0135
  -9.000   0.0615   0.07357   0.06882  -0.1037   0.5099   0.0142
  -8.750   0.0779   0.07359   0.06884  -0.1034   0.5090   0.0148
  -8.500   0.0721   0.06949   0.06477  -0.1051   0.5085   0.0146
  -8.250   0.0621   0.06491   0.06023  -0.1072   0.5080   0.0145
  -8.000  -0.0065   0.05216   0.04752  -0.1138   0.5081   0.0141
  -7.750  -0.0192   0.04762   0.04287  -0.1140   0.5076   0.0142
  -7.500  -0.0307   0.04275   0.03783  -0.1132   0.5071   0.0142
  -7.250  -0.0252   0.04064   0.03560  -0.1122   0.5063   0.0143
  -7.000  -0.0162   0.03884   0.03367  -0.1112   0.5055   0.0145
  -6.750  -0.0125   0.03555   0.03017  -0.1096   0.5051   0.0146
  -6.500  -0.0007   0.03356   0.02802  -0.1084   0.5047   0.0148
  -6.250   0.0110   0.03126   0.02552  -0.1069   0.5042   0.0151
  -6.000   0.0245   0.02909   0.02311  -0.1054   0.5037   0.0154
  -5.750   0.0374   0.02653   0.02023  -0.1034   0.5031   0.0161
  -5.500   0.0520   0.02411   0.01742  -0.1015   0.5026   0.0163
  -5.250   0.0705   0.02236   0.01534  -0.1000   0.5020   0.0166
  -5.000   0.0914   0.02102   0.01369  -0.0987   0.5013   0.0169
  -4.750   0.1140   0.02000   0.01242  -0.0978   0.5005   0.0172
  -4.500   0.1378   0.01915   0.01149  -0.0972   0.4996   0.0174
  -4.250   0.1627   0.01857   0.01085  -0.0968   0.4988   0.0177
  -4.000   0.1881   0.01817   0.01040  -0.0965   0.4979   0.0181
  -3.750   0.2137   0.01771   0.00988  -0.0961   0.4972   0.0185
  -3.500   0.2394   0.01715   0.00921  -0.0957   0.4965   0.0188
  -3.250   0.2652   0.01663   0.00860  -0.0953   0.4958   0.0192
  -3.000   0.2913   0.01618   0.00806  -0.0949   0.4951   0.0195
  -2.750   0.3174   0.01578   0.00759  -0.0945   0.4944   0.0197
  -2.500   0.3436   0.01546   0.00720  -0.0942   0.4937   0.0201
  -2.250   0.3699   0.01520   0.00688  -0.0939   0.4931   0.0204
  -2.000   0.3955   0.01484   0.00650  -0.0935   0.4924   0.0207
  -1.750   0.4209   0.01453   0.00620  -0.0931   0.4917   0.0212
  -1.500   0.4468   0.01435   0.00601  -0.0928   0.4911   0.0218
  -1.250   0.4729   0.01419   0.00583  -0.0925   0.4903   0.0224
  -1.000   0.4990   0.01406   0.00568  -0.0922   0.4894   0.0230
  -0.750   0.5251   0.01394   0.00554  -0.0919   0.4886   0.0234
  -0.500   0.5511   0.01380   0.00541  -0.0916   0.4880   0.0239
  -0.250   0.5772   0.01370   0.00531  -0.0913   0.4874   0.0244
   0.000   0.6030   0.01355   0.00518  -0.0910   0.4868   0.0251
   0.250   0.6292   0.01348   0.00512  -0.0908   0.4862   0.0258
   0.500   0.6557   0.01343   0.00509  -0.0906   0.4855   0.0271
   0.750   0.6822   0.01341   0.00506  -0.0904   0.4846   0.0284
   1.000   0.7085   0.01338   0.00503  -0.0902   0.4836   0.0297
   1.250   0.7350   0.01337   0.00503  -0.0901   0.4827   0.0316
   1.500   0.7615   0.01336   0.00503  -0.0899   0.4817   0.0354
   1.750   0.7774   0.01239   0.00508  -0.0882   0.4805   0.4101
   2.000   0.7862   0.01147   0.00516  -0.0846   0.4793   0.7384
   2.500   0.9296   0.01145   0.00554  -0.1029   0.4764   0.9849
   2.750   0.9776   0.01157   0.00560  -0.1074   0.4752   0.9936
   3.000   1.0286   0.01168   0.00562  -0.1125   0.4738   0.9992
   3.250   1.0560   0.01178   0.00570  -0.1128   0.4725   1.0000
   3.500   1.0771   0.01184   0.00579  -0.1117   0.4711   1.0000
   3.750   1.0985   0.01192   0.00587  -0.1106   0.4695   1.0000
   4.000   1.1199   0.01198   0.00594  -0.1096   0.4677   1.0000
   4.250   1.1416   0.01204   0.00601  -0.1086   0.4658   1.0000
   4.500   1.1633   0.01210   0.00606  -0.1076   0.4640   1.0000
   4.750   1.1851   0.01216   0.00610  -0.1067   0.4623   1.0000
   5.000   1.2071   0.01223   0.00615  -0.1058   0.4607   1.0000
   5.250   1.2291   0.01231   0.00621  -0.1049   0.4591   1.0000
   5.500   1.2509   0.01242   0.00632  -0.1040   0.4576   1.0000
   5.750   1.2719   0.01254   0.00648  -0.1029   0.4558   1.0000
   6.000   1.2928   0.01265   0.00663  -0.1019   0.4537   1.0000
   6.250   1.3136   0.01274   0.00676  -0.1008   0.4514   1.0000
   6.500   1.3343   0.01284   0.00687  -0.0997   0.4492   1.0000
   6.750   1.3549   0.01293   0.00697  -0.0987   0.4472   1.0000
   7.000   1.3751   0.01303   0.00707  -0.0975   0.4453   1.0000
   7.250   1.3949   0.01315   0.00720  -0.0963   0.4432   1.0000
   7.500   1.4141   0.01330   0.00741  -0.0950   0.4402   1.0000
   7.750   1.4327   0.01344   0.00760  -0.0937   0.4371   1.0000
   8.000   1.4485   0.01356   0.00774  -0.0917   0.4337   1.0000
   8.250   1.4620   0.01369   0.00787  -0.0893   0.4308   1.0000
   8.500   1.4772   0.01388   0.00810  -0.0874   0.4276   1.0000
   8.750   1.4923   0.01408   0.00836  -0.0855   0.4234   1.0000
   9.000   1.5060   0.01430   0.00860  -0.0834   0.4189   1.0000
   9.250   1.5197   0.01458   0.00889  -0.0815   0.4141   1.0000
   9.500   1.5334   0.01491   0.00926  -0.0796   0.4077   1.0000
   9.750   1.5438   0.01535   0.00970  -0.0774   0.4006   1.0000
  10.000   1.5540   0.01588   0.01025  -0.0753   0.3923   1.0000
  10.250   1.5617   0.01659   0.01095  -0.0731   0.3839   1.0000
  10.500   1.5648   0.01758   0.01192  -0.0705   0.3749   1.0000
  10.750   1.5694   0.01867   0.01302  -0.0684   0.3657   1.0000
  11.000   1.5698   0.02011   0.01446  -0.0661   0.3574   1.0000
  11.250   1.5676   0.02189   0.01624  -0.0639   0.3486   1.0000
  11.500   1.5649   0.02385   0.01822  -0.0620   0.3402   1.0000
  11.750   1.5535   0.02661   0.02098  -0.0598   0.3313   1.0000
  12.000   1.5504   0.02894   0.02336  -0.0584   0.3240   1.0000
  12.250   1.5361   0.03232   0.02675  -0.0567   0.3165   1.0000
  12.500   1.5322   0.03493   0.02942  -0.0556   0.3099   1.0000
  12.750   1.5189   0.03842   0.03292  -0.0542   0.3029   1.0000
  13.000   1.5152   0.04108   0.03563  -0.0533   0.2973   1.0000
  13.250   1.5085   0.04404   0.03861  -0.0523   0.2911   1.0000
  13.500   1.5018   0.04700   0.04158  -0.0514   0.2855   1.0000
  13.750   1.5019   0.04936   0.04399  -0.0507   0.2800   1.0000
  14.000   1.4960   0.05231   0.04694  -0.0499   0.2741   1.0000
  14.250   1.4988   0.05445   0.04910  -0.0494   0.2699   1.0000
  14.500   1.5011   0.05668   0.05138  -0.0489   0.2656   1.0000
  14.750   1.5025   0.05897   0.05369  -0.0485   0.2613   1.0000
  15.000   1.5051   0.06114   0.05586  -0.0480   0.2573   1.0000
  15.250   1.5104   0.06312   0.05791  -0.0478   0.2536   1.0000
  15.500   1.5136   0.06532   0.06015  -0.0475   0.2492   1.0000
  15.750   1.5179   0.06736   0.06220  -0.0472   0.2457   1.0000
  16.000   1.5234   0.06927   0.06414  -0.0470   0.2425   1.0000
  16.250   1.5297   0.07119   0.06612  -0.0468   0.2395   1.0000
  16.500   1.5347   0.07322   0.06821  -0.0467   0.2360   1.0000
  16.750   1.5359   0.07567   0.07065  -0.0465   0.2308   1.0000
  17.000   1.5383   0.07802   0.07304  -0.0464   0.2258   1.0000
  17.250   1.5413   0.08032   0.07540  -0.0463   0.2217   1.0000
  17.500   1.5399   0.08309   0.07815  -0.0462   0.2159   1.0000
  17.750   1.5470   0.08491   0.08003  -0.0462   0.2135   1.0000
  18.000   1.5513   0.08711   0.08230  -0.0462   0.2099   1.0000
  18.250   1.5480   0.09021   0.08540  -0.0462   0.2033   1.0000
  18.500   1.5500   0.09265   0.08788  -0.0463   0.1988   1.0000
  18.750   1.5520   0.09512   0.09042  -0.0465   0.1945   1.0000
  19.000   1.5475   0.09838   0.09367  -0.0466   0.1882   1.0000
  19.250   1.5462   0.10131   0.09665  -0.0468   0.1810   1.0000
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