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WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il)
Reynolds number: 200,000
Max Cl/Cd: 52.25 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fxlv152-il-200000.txt
Download as CSV file: xf-fxlv152-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX L V-152 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.9356   0.14530   0.14177   0.0309   1.0005   0.0222
 -17.250  -0.9693   0.13173   0.12802   0.0220   1.0005   0.0217
 -17.000  -1.0068   0.11834   0.11435   0.0131   1.0005   0.0211
 -16.750  -1.0416   0.10663   0.10231   0.0056   1.0005   0.0207
 -16.500  -1.0668   0.09772   0.09312   0.0003   1.0005   0.0206
 -16.250  -1.0828   0.09105   0.08623  -0.0032   1.0005   0.0206
 -16.000  -1.0952   0.08529   0.08027  -0.0059   1.0005   0.0207
 -15.750  -1.1050   0.08017   0.07497  -0.0081   1.0005   0.0209
 -15.500  -1.1133   0.07547   0.07007  -0.0098   1.0005   0.0210
 -15.250  -1.1198   0.07118   0.06560  -0.0110   1.0005   0.0212
 -15.000  -1.1245   0.06727   0.06149  -0.0119   1.0005   0.0215
 -14.750  -1.1274   0.06367   0.05769  -0.0124   1.0005   0.0218
 -14.500  -1.1290   0.06028   0.05409  -0.0127   1.0005   0.0222
 -14.250  -1.1277   0.05730   0.05094  -0.0127   1.0005   0.0226
 -14.000  -1.1210   0.05512   0.04881  -0.0122   1.0005   0.0232
 -13.750  -1.1170   0.05265   0.04629  -0.0121   1.0005   0.0239
 -13.500  -1.1137   0.05008   0.04360  -0.0120   1.0005   0.0248
 -13.250  -1.1104   0.04757   0.04102  -0.0117   1.0005   0.0258
 -13.000  -1.1063   0.04524   0.03868  -0.0117   1.0005   0.0270
 -12.750  -1.1021   0.04288   0.03619  -0.0114   1.0005   0.0288
 -12.500  -1.0966   0.04071   0.03402  -0.0114   1.0005   0.0307
 -12.250  -1.0901   0.03863   0.03185  -0.0113   1.0005   0.0333
 -12.000  -1.0812   0.03678   0.02985  -0.0112   1.0005   0.0361
 -11.750  -1.0730   0.03498   0.02804  -0.0110   1.0005   0.0385
 -11.500  -1.0630   0.03332   0.02629  -0.0107   1.0005   0.0410
 -11.250  -1.0521   0.03179   0.02471  -0.0105   1.0005   0.0433
 -11.000  -1.0408   0.03031   0.02319  -0.0102   1.0005   0.0456
 -10.750  -1.0279   0.02900   0.02182  -0.0099   1.0005   0.0481
 -10.500  -1.0152   0.02769   0.02049  -0.0095   1.0005   0.0504
 -10.250  -1.0004   0.02661   0.01935  -0.0091   1.0005   0.0535
 -10.000  -0.9861   0.02553   0.01827  -0.0087   1.0005   0.0567
  -9.750  -0.9712   0.02454   0.01723  -0.0080   1.0005   0.0605
  -9.500  -0.9554   0.02362   0.01627  -0.0072   1.0005   0.0651
  -9.250  -0.9395   0.02257   0.01525  -0.0066   1.0005   0.0705
  -9.000  -0.9230   0.02151   0.01423  -0.0061   1.0005   0.0772
  -8.750  -0.9048   0.02053   0.01329  -0.0056   1.0005   0.0854
  -8.500  -0.8846   0.01965   0.01247  -0.0055   1.0005   0.0956
  -8.250  -0.8632   0.01880   0.01171  -0.0057   1.0005   0.1074
  -8.000  -0.8373   0.01804   0.01103  -0.0068   0.9804   0.1220
  -7.750  -0.8003   0.01726   0.01027  -0.0098   0.9369   0.1429
  -7.500  -0.7774   0.01666   0.00965  -0.0096   0.9074   0.1651
  -7.250  -0.7593   0.01586   0.00900  -0.0086   0.8866   0.1933
  -7.000  -0.7411   0.01503   0.00836  -0.0077   0.8705   0.2375
  -6.750  -0.7219   0.01427   0.00779  -0.0069   0.8569   0.2974
  -6.500  -0.7023   0.01358   0.00732  -0.0059   0.8452   0.3497
  -6.250  -0.6805   0.01315   0.00709  -0.0051   0.8341   0.4088
  -6.000  -0.6562   0.01298   0.00701  -0.0046   0.8247   0.4535
  -5.750  -0.6308   0.01296   0.00700  -0.0041   0.8164   0.4852
  -5.500  -0.6042   0.01310   0.00714  -0.0036   0.8092   0.5087
  -5.250  -0.5767   0.01324   0.00721  -0.0034   0.8019   0.5278
  -5.000  -0.5497   0.01340   0.00724  -0.0031   0.7959   0.5435
  -4.750  -0.5221   0.01356   0.00727  -0.0031   0.7898   0.5585
  -4.500  -0.4944   0.01376   0.00748  -0.0027   0.7835   0.5706
  -4.250  -0.4671   0.01395   0.00760  -0.0023   0.7781   0.5820
  -4.000  -0.4395   0.01417   0.00773  -0.0021   0.7727   0.5940
  -3.750  -0.4114   0.01442   0.00802  -0.0018   0.7673   0.6033
  -3.500  -0.3840   0.01461   0.00808  -0.0016   0.7626   0.6148
  -3.250  -0.3562   0.01481   0.00829  -0.0011   0.7586   0.6217
  -3.000  -0.3280   0.01489   0.00831  -0.0013   0.7536   0.6301
  -2.750  -0.3000   0.01490   0.00830  -0.0013   0.7483   0.6363
  -2.500  -0.2722   0.01498   0.00834  -0.0011   0.7437   0.6426
  -2.250  -0.2447   0.01506   0.00827  -0.0011   0.7400   0.6510
  -2.000  -0.2164   0.01507   0.00837  -0.0011   0.7353   0.6562
  -1.750  -0.1882   0.01509   0.00839  -0.0012   0.7305   0.6616
  -1.500  -0.1602   0.01505   0.00826  -0.0014   0.7260   0.6676
  -1.250  -0.1324   0.01502   0.00818  -0.0014   0.7221   0.6722
  -1.000  -0.1042   0.01507   0.00829  -0.0015   0.7175   0.6767
  -0.750  -0.0759   0.01509   0.00831  -0.0017   0.7124   0.6822
  -0.500  -0.0478   0.01506   0.00822  -0.0019   0.7077   0.6884
  -0.250  -0.0203   0.01508   0.00825  -0.0015   0.7038   0.6926
   0.000   0.0076   0.01514   0.00836  -0.0016   0.6984   0.6978
   0.250   0.0358   0.01514   0.00834  -0.0018   0.6925   0.7041
   0.500   0.0634   0.01507   0.00826  -0.0017   0.6876   0.7088
   0.750   0.0911   0.01510   0.00829  -0.0015   0.6832   0.7130
   1.000   0.1193   0.01511   0.00836  -0.0018   0.6771   0.7174
   1.250   0.1477   0.01508   0.00830  -0.0020   0.6717   0.7223
   1.500   0.1759   0.01503   0.00822  -0.0020   0.6674   0.7262
   1.750   0.2035   0.01506   0.00835  -0.0021   0.6614   0.7300
   2.000   0.2313   0.01505   0.00838  -0.0021   0.6548   0.7347
   2.250   0.2595   0.01500   0.00828  -0.0020   0.6492   0.7400
   2.500   0.2872   0.01498   0.00832  -0.0021   0.6421   0.7443
   2.750   0.3148   0.01491   0.00833  -0.0020   0.6349   0.7482
   3.000   0.3429   0.01483   0.00823  -0.0018   0.6292   0.7529
   3.250   0.3706   0.01480   0.00830  -0.0019   0.6205   0.7583
   3.500   0.3985   0.01460   0.00812  -0.0016   0.6128   0.7630
   3.750   0.4256   0.01444   0.00805  -0.0013   0.6029   0.7675
   4.000   0.4536   0.01416   0.00776  -0.0009   0.5927   0.7726
   4.250   0.4812   0.01397   0.00763  -0.0008   0.5803   0.7782
   4.500   0.5086   0.01374   0.00742  -0.0003   0.5697   0.7828
   4.750   0.5356   0.01356   0.00734   0.0001   0.5560   0.7886
   5.000   0.5630   0.01342   0.00728   0.0002   0.5412   0.7956
   5.250   0.5896   0.01324   0.00722   0.0007   0.5246   0.8016
   5.500   0.6162   0.01308   0.00713   0.0011   0.5037   0.8090
   5.750   0.6424   0.01298   0.00699   0.0016   0.4788   0.8165
   6.000   0.6671   0.01302   0.00706   0.0022   0.4471   0.8243
   6.250   0.6908   0.01322   0.00716   0.0029   0.4025   0.8342
   6.500   0.7109   0.01369   0.00740   0.0040   0.3430   0.8446
   6.750   0.7294   0.01442   0.00790   0.0051   0.2891   0.8559
   7.000   0.7472   0.01521   0.00846   0.0062   0.2297   0.8694
   7.250   0.7643   0.01599   0.00909   0.0074   0.1888   0.8856
   7.500   0.7814   0.01669   0.00971   0.0087   0.1635   0.9060
   7.750   0.8015   0.01736   0.01035   0.0094   0.1429   0.9340
   8.000   0.8366   0.01806   0.01106   0.0069   0.1222   0.9732
   8.250   0.8642   0.01887   0.01177   0.0054   0.1075   0.9995
   8.500   0.8859   0.01964   0.01249   0.0052   0.0954   0.9995
   8.750   0.9055   0.02051   0.01330   0.0055   0.0853   0.9995
   9.000   0.9228   0.02149   0.01423   0.0061   0.0772   0.9995
   9.250   0.9387   0.02252   0.01524   0.0068   0.0706   0.9995
   9.500   0.9540   0.02353   0.01623   0.0075   0.0649   0.9995
   9.750   0.9680   0.02448   0.01718   0.0085   0.0603   0.9995
  10.000   0.9830   0.02544   0.01817   0.0091   0.0563   0.9995
  10.250   0.9975   0.02650   0.01928   0.0096   0.0530   0.9995
  10.500   1.0103   0.02770   0.02047   0.0100   0.0504   0.9995
  10.750   1.0237   0.02893   0.02179   0.0105   0.0480   0.9995
  11.000   1.0351   0.03032   0.02319   0.0109   0.0460   0.9995
  11.250   1.0468   0.03174   0.02469   0.0113   0.0435   0.9995
  11.500   1.0564   0.03332   0.02626   0.0116   0.0413   0.9995
  11.750   1.0668   0.03490   0.02796   0.0120   0.0388   0.9995
  12.000   1.0743   0.03669   0.02976   0.0123   0.0366   0.9995
  12.250   1.0829   0.03848   0.03169   0.0125   0.0339   0.9995
  12.500   1.0892   0.04049   0.03380   0.0128   0.0314   0.9995
  12.750   1.0943   0.04261   0.03593   0.0128   0.0295   0.9995
  13.000   1.0985   0.04491   0.03836   0.0132   0.0276   0.9995
  13.250   1.1023   0.04719   0.04065   0.0133   0.0264   0.9995
  13.500   1.1050   0.04965   0.04319   0.0137   0.0253   0.9995
  13.750   1.1078   0.05214   0.04579   0.0139   0.0244   0.9995
  14.000   1.1112   0.05455   0.04823   0.0141   0.0237   0.9995
  14.250   1.1170   0.05668   0.05031   0.0147   0.0231   0.9995
  14.500   1.1177   0.05961   0.05342   0.0148   0.0226   0.9995
  14.750   1.1163   0.06280   0.05681   0.0147   0.0222   0.9995
  15.000   1.1140   0.06617   0.06036   0.0144   0.0219   0.9995
  15.250   1.1102   0.06980   0.06416   0.0138   0.0216   0.9995
  15.500   1.1049   0.07374   0.06827   0.0129   0.0214   0.9995
  15.750   1.0978   0.07808   0.07279   0.0116   0.0212   0.9995
  16.000   1.0880   0.08295   0.07785   0.0099   0.0211   0.9995
  16.250   1.0750   0.08855   0.08367   0.0075   0.0211   0.9995
  16.500   1.0572   0.09524   0.09060   0.0041   0.0211   0.9995
  16.750   1.0328   0.10358   0.09921  -0.0006   0.0212   0.9995
  17.000   1.0019   0.11389   0.10981  -0.0069   0.0215   0.9995
  17.250   0.9657   0.12623   0.12243  -0.0148   0.0220   0.9995
  17.500   0.9260   0.14058   0.13699  -0.0241   0.0225   0.9995
  17.750   0.8931   0.15421   0.15074  -0.0324   0.0230   0.9995
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