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FX 73-CL2-152 (fx73cl2152-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 73-CL2-152 (fx73cl2152-il)
Reynolds number: 1,000,000
Max Cl/Cd: 135.31 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx73cl2152-il-1000000-n5.txt
Download as CSV file: xf-fx73cl2152-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 73-CL2-152                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.5191   0.08444   0.08189  -0.0910   0.9873   0.0211
 -14.250  -0.5351   0.07692   0.07429  -0.0975   0.9865   0.0213
 -14.000  -0.5462   0.06999   0.06728  -0.1043   0.9857   0.0215
 -13.750  -0.5694   0.06409   0.06131  -0.1072   0.9818   0.0216
 -13.500  -0.5873   0.05743   0.05457  -0.1133   0.9790   0.0218
 -13.250  -0.6039   0.04995   0.04697  -0.1220   0.9763   0.0219
 -13.000  -0.6367   0.04403   0.04095  -0.1253   0.9688   0.0219
 -12.750  -0.6562   0.03644   0.03324  -0.1338   0.9615   0.0220
 -12.500  -0.6496   0.02923   0.02586  -0.1454   0.9549   0.0221
 -12.250  -0.6242   0.02359   0.02004  -0.1570   0.9484   0.0223
 -12.000  -0.5897   0.02081   0.01710  -0.1641   0.9420   0.0227
 -11.750  -0.5590   0.01944   0.01564  -0.1671   0.9368   0.0229
 -11.500  -0.5287   0.01835   0.01447  -0.1694   0.9300   0.0232
 -11.250  -0.4902   0.01732   0.01336  -0.1727   0.9246   0.0236
 -11.000  -0.4487   0.01642   0.01236  -0.1764   0.9145   0.0240
 -10.750  -0.3684   0.01533   0.01107  -0.1877   0.8913   0.0244
 -10.500  -0.2965   0.01456   0.00989  -0.1978   0.8166   0.0251
 -10.250  -0.2780   0.01451   0.00944  -0.1964   0.7326   0.0253
 -10.000  -0.2549   0.01434   0.00902  -0.1960   0.6790   0.0257
  -9.750  -0.2284   0.01415   0.00862  -0.1961   0.6373   0.0260
  -9.500  -0.2001   0.01394   0.00822  -0.1965   0.6045   0.0264
  -9.250  -0.1706   0.01371   0.00784  -0.1971   0.5776   0.0268
  -9.000  -0.1406   0.01347   0.00747  -0.1977   0.5572   0.0272
  -8.750  -0.1103   0.01325   0.00713  -0.1984   0.5406   0.0277
  -8.500  -0.0800   0.01306   0.00682  -0.1990   0.5262   0.0281
  -8.250  -0.0489   0.01279   0.00645  -0.1998   0.5126   0.0286
  -8.000  -0.0178   0.01252   0.00612  -0.2006   0.5017   0.0292
  -7.750   0.0129   0.01233   0.00584  -0.2012   0.4914   0.0297
  -7.500   0.0434   0.01214   0.00559  -0.2017   0.4826   0.0302
  -7.000   0.1042   0.01182   0.00513  -0.2027   0.4670   0.0314
  -6.750   0.1344   0.01169   0.00492  -0.2031   0.4593   0.0319
  -6.500   0.1646   0.01156   0.00473  -0.2034   0.4530   0.0324
  -6.250   0.1955   0.01137   0.00450  -0.2040   0.4481   0.0334
  -6.000   0.2257   0.01124   0.00434  -0.2044   0.4433   0.0342
  -5.750   0.2559   0.01114   0.00418  -0.2047   0.4385   0.0350
  -5.500   0.2860   0.01105   0.00404  -0.2050   0.4344   0.0359
  -5.250   0.3161   0.01094   0.00390  -0.2053   0.4314   0.0366
  -5.000   0.3466   0.01082   0.00375  -0.2057   0.4281   0.0376
  -4.750   0.3769   0.01073   0.00363  -0.2061   0.4247   0.0388
  -4.500   0.4068   0.01067   0.00354  -0.2063   0.4211   0.0402
  -4.000   0.4668   0.01055   0.00335  -0.2068   0.4147   0.0430
  -3.750   0.4969   0.01048   0.00327  -0.2071   0.4125   0.0448
  -3.500   0.5267   0.01043   0.00321  -0.2073   0.4102   0.0466
  -3.250   0.5567   0.01038   0.00314  -0.2075   0.4078   0.0489
  -3.000   0.5865   0.01034   0.00309  -0.2077   0.4053   0.0519
  -2.750   0.6162   0.01032   0.00305  -0.2079   0.4026   0.0554
  -2.500   0.6458   0.01031   0.00302  -0.2081   0.3995   0.0597
  -2.250   0.6756   0.01028   0.00300  -0.2083   0.3972   0.0660
  -2.000   0.7059   0.01022   0.00297  -0.2086   0.3957   0.0761
  -1.750   0.7366   0.01013   0.00294  -0.2091   0.3937   0.0964
  -1.500   0.7673   0.01006   0.00294  -0.2095   0.3910   0.1220
  -1.250   0.7971   0.01004   0.00296  -0.2098   0.3884   0.1411
  -1.000   0.8265   0.01005   0.00299  -0.2099   0.3861   0.1565
  -0.750   0.8555   0.01008   0.00303  -0.2100   0.3836   0.1695
  -0.500   0.8841   0.01014   0.00308  -0.2100   0.3808   0.1804
  -0.250   0.9132   0.01016   0.00313  -0.2100   0.3788   0.1920
   0.000   0.9421   0.01019   0.00318  -0.2100   0.3773   0.2024
   0.250   0.9711   0.01021   0.00323  -0.2101   0.3754   0.2182
   0.500   1.0001   0.01024   0.00330  -0.2101   0.3735   0.2357
   0.750   1.0289   0.01027   0.00337  -0.2102   0.3716   0.2509
   1.000   1.0572   0.01034   0.00344  -0.2101   0.3697   0.2600
   1.250   1.0855   0.01040   0.00351  -0.2100   0.3676   0.2713
   1.500   1.1136   0.01048   0.00360  -0.2099   0.3655   0.2843
   1.750   1.1415   0.01057   0.00370  -0.2097   0.3632   0.2988
   2.000   1.1696   0.01063   0.00380  -0.2096   0.3615   0.3144
   2.250   1.1980   0.01068   0.00389  -0.2096   0.3600   0.3323
   2.500   1.2261   0.01073   0.00400  -0.2095   0.3581   0.3523
   2.750   1.2540   0.01080   0.00410  -0.2093   0.3559   0.3705
   3.000   1.2815   0.01088   0.00421  -0.2091   0.3537   0.3882
   3.250   1.3089   0.01096   0.00433  -0.2089   0.3515   0.4091
   3.500   1.3360   0.01106   0.00447  -0.2086   0.3492   0.4297
   3.750   1.3628   0.01118   0.00460  -0.2083   0.3467   0.4485
   4.000   1.3896   0.01128   0.00475  -0.2080   0.3446   0.4696
   4.250   1.4167   0.01136   0.00489  -0.2077   0.3431   0.4945
   4.500   1.4436   0.01144   0.00503  -0.2074   0.3411   0.5173
   4.750   1.4702   0.01155   0.00518  -0.2071   0.3385   0.5383
   5.000   1.4966   0.01166   0.00534  -0.2067   0.3356   0.5621
   5.250   1.5227   0.01179   0.00551  -0.2063   0.3325   0.5881
   5.500   1.5483   0.01195   0.00570  -0.2058   0.3294   0.6118
   5.750   1.5743   0.01207   0.00588  -0.2053   0.3273   0.6357
   6.000   1.6004   0.01219   0.00606  -0.2049   0.3251   0.6599
   6.250   1.6263   0.01232   0.00625  -0.2045   0.3223   0.6861
   6.500   1.6518   0.01246   0.00646  -0.2040   0.3193   0.7160
   6.750   1.6769   0.01262   0.00669  -0.2034   0.3159   0.7531
   7.000   1.7014   0.01280   0.00693  -0.2028   0.3122   0.7970
   7.250   1.7253   0.01287   0.00715  -0.2019   0.3096   0.8589
   7.500   1.7401   0.01286   0.00728  -0.1991   0.3067   1.0000
   7.750   1.7636   0.01309   0.00750  -0.1983   0.3023   1.0000
   8.000   1.7857   0.01340   0.00777  -0.1972   0.2961   1.0000
   8.250   1.8084   0.01366   0.00802  -0.1962   0.2889   1.0000
   8.500   1.8290   0.01405   0.00835  -0.1950   0.2803   1.0000
   8.750   1.8510   0.01435   0.00864  -0.1939   0.2738   1.0000
   9.000   1.8712   0.01476   0.00901  -0.1926   0.2669   1.0000
   9.250   1.8927   0.01507   0.00933  -0.1915   0.2622   1.0000
   9.500   1.9130   0.01544   0.00969  -0.1901   0.2563   1.0000
   9.750   1.9314   0.01591   0.01013  -0.1885   0.2501   1.0000
  10.000   1.9519   0.01624   0.01048  -0.1873   0.2465   1.0000
  10.250   1.9715   0.01662   0.01088  -0.1859   0.2420   1.0000
  10.500   1.9892   0.01713   0.01137  -0.1843   0.2366   1.0000
  10.750   2.0076   0.01756   0.01182  -0.1827   0.2322   1.0000
  11.000   2.0254   0.01802   0.01230  -0.1811   0.2272   1.0000
  11.250   2.0411   0.01862   0.01289  -0.1792   0.2215   1.0000
  11.500   2.0578   0.01914   0.01343  -0.1775   0.2168   1.0000
  11.750   2.0724   0.01978   0.01408  -0.1755   0.2098   1.0000
  12.000   2.0853   0.02054   0.01482  -0.1734   0.2025   1.0000
  12.250   2.0938   0.02156   0.01580  -0.1706   0.1911   1.0000
  12.500   2.0994   0.02277   0.01696  -0.1675   0.1781   1.0000
  12.750   2.1009   0.02426   0.01839  -0.1641   0.1637   1.0000
  13.000   2.0993   0.02600   0.02009  -0.1605   0.1501   1.0000
  13.250   2.0965   0.02791   0.02197  -0.1569   0.1387   1.0000
  13.500   2.0946   0.02984   0.02390  -0.1538   0.1296   1.0000
  13.750   2.0919   0.03196   0.02603  -0.1509   0.1223   1.0000
  14.000   2.0866   0.03442   0.02852  -0.1481   0.1155   1.0000
  14.250   2.0831   0.03693   0.03107  -0.1459   0.1101   1.0000
  14.500   2.0743   0.04014   0.03432  -0.1437   0.1042   1.0000
  14.750   2.0687   0.04328   0.03753  -0.1422   0.1003   1.0000
  15.000   2.0614   0.04687   0.04120  -0.1411   0.0964   1.0000
  15.250   2.0493   0.05130   0.04570  -0.1404   0.0928   1.0000
  15.500   2.0393   0.05577   0.05027  -0.1401   0.0901   1.0000
  15.750   2.0276   0.06069   0.05529  -0.1402   0.0875   1.0000
  16.000   2.0120   0.06636   0.06106  -0.1407   0.0850   1.0000
  16.250   1.9930   0.07271   0.06752  -0.1415   0.0827   1.0000
  16.500   1.9762   0.07890   0.07383  -0.1425   0.0808   1.0000
  16.750   1.9602   0.08506   0.08011  -0.1437   0.0789   1.0000
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