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WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il)
Reynolds number: 500,000
Max Cl/Cd: 59.92 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fxlv152-il-500000.txt
Download as CSV file: xf-fxlv152-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -1.1638   0.11361   0.10988   0.0201   1.0005   0.0087
 -18.000  -1.1770   0.10712   0.10327   0.0169   1.0005   0.0087
 -17.750  -1.1899   0.10079   0.09682   0.0138   1.0005   0.0087
 -17.500  -1.2021   0.09471   0.09062   0.0109   1.0005   0.0087
 -17.250  -1.2136   0.08889   0.08467   0.0083   1.0005   0.0088
 -17.000  -1.2241   0.08335   0.07901   0.0059   1.0005   0.0088
 -16.750  -1.2332   0.07819   0.07373   0.0037   1.0005   0.0088
 -16.500  -1.2412   0.07336   0.06878   0.0018   1.0005   0.0089
 -16.250  -1.2480   0.06880   0.06411   0.0001   1.0005   0.0089
 -16.000  -1.2536   0.06457   0.05977  -0.0014   1.0005   0.0090
 -15.750  -1.2582   0.06059   0.05568  -0.0027   1.0005   0.0091
 -15.500  -1.2615   0.05694   0.05192  -0.0037   1.0005   0.0091
 -15.250  -1.2641   0.05354   0.04841  -0.0045   1.0005   0.0092
 -15.000  -1.2660   0.05036   0.04514  -0.0051   1.0005   0.0093
 -14.750  -1.2665   0.04741   0.04209  -0.0055   1.0005   0.0094
 -14.500  -1.2655   0.04466   0.03924  -0.0058   1.0005   0.0095
 -14.250  -1.2633   0.04210   0.03658  -0.0061   1.0005   0.0096
 -14.000  -1.2596   0.03972   0.03411  -0.0062   1.0005   0.0097
 -13.750  -1.2547   0.03749   0.03180  -0.0063   1.0005   0.0099
 -13.500  -1.2479   0.03549   0.02974  -0.0063   1.0005   0.0101
 -13.250  -1.2388   0.03372   0.02793  -0.0063   1.0005   0.0104
 -13.000  -1.2281   0.03214   0.02629  -0.0063   1.0005   0.0109
 -12.750  -1.2168   0.03060   0.02469  -0.0062   1.0005   0.0114
 -12.500  -1.2054   0.02910   0.02312  -0.0061   1.0005   0.0120
 -12.250  -1.1920   0.02780   0.02179  -0.0060   1.0005   0.0127
 -12.000  -1.1784   0.02652   0.02045  -0.0059   1.0005   0.0136
 -11.750  -1.1642   0.02533   0.01918  -0.0057   1.0005   0.0146
 -11.500  -1.1502   0.02417   0.01797  -0.0054   1.0005   0.0157
 -11.250  -1.1334   0.02328   0.01698  -0.0051   1.0005   0.0169
 -11.000  -1.1215   0.02205   0.01571  -0.0044   1.0005   0.0179
 -10.750  -1.1061   0.02116   0.01476  -0.0037   1.0005   0.0191
 -10.500  -1.0890   0.02036   0.01390  -0.0030   1.0005   0.0201
 -10.250  -1.0712   0.01950   0.01300  -0.0024   1.0005   0.0213
 -10.000  -1.0505   0.01884   0.01229  -0.0020   1.0005   0.0224
  -9.750  -1.0300   0.01811   0.01156  -0.0017   1.0005   0.0237
  -9.500  -1.0078   0.01750   0.01094  -0.0015   1.0005   0.0252
  -9.250  -0.9764   0.01698   0.01035  -0.0030   0.9199   0.0271
  -9.000  -0.9563   0.01665   0.00988  -0.0019   0.8700   0.0290
  -8.750  -0.9345   0.01631   0.00942  -0.0012   0.8432   0.0319
  -8.500  -0.9112   0.01595   0.00896  -0.0007   0.8215   0.0353
  -8.250  -0.8875   0.01557   0.00849  -0.0004   0.8038   0.0391
  -8.000  -0.8636   0.01515   0.00801  -0.0001   0.7887   0.0438
  -7.750  -0.8398   0.01468   0.00755   0.0002   0.7762   0.0527
  -7.500  -0.8149   0.01429   0.00715   0.0003   0.7660   0.0644
  -7.250  -0.7901   0.01392   0.00674   0.0005   0.7574   0.0739
  -7.000  -0.7649   0.01348   0.00635   0.0005   0.7494   0.0865
  -6.750  -0.7397   0.01308   0.00598   0.0006   0.7424   0.1035
  -6.500  -0.7140   0.01268   0.00564   0.0006   0.7361   0.1225
  -6.250  -0.6880   0.01228   0.00531   0.0005   0.7298   0.1420
  -6.000  -0.6619   0.01192   0.00498   0.0005   0.7241   0.1610
  -5.750  -0.6364   0.01144   0.00461   0.0005   0.7187   0.1885
  -5.500  -0.6117   0.01077   0.00420   0.0005   0.7131   0.2418
  -5.250  -0.5866   0.01021   0.00385   0.0006   0.7079   0.2992
  -5.000  -0.5617   0.00965   0.00348   0.0007   0.7034   0.3514
  -4.750  -0.5365   0.00911   0.00326   0.0007   0.6991   0.4218
  -4.500  -0.5091   0.00890   0.00312   0.0007   0.6948   0.4558
  -4.250  -0.4812   0.00876   0.00301   0.0006   0.6908   0.4777
  -4.000  -0.4531   0.00868   0.00295   0.0005   0.6870   0.4965
  -3.750  -0.4247   0.00868   0.00294   0.0004   0.6833   0.5140
  -3.500  -0.3958   0.00867   0.00294   0.0003   0.6795   0.5295
  -3.250  -0.3668   0.00870   0.00292   0.0001   0.6757   0.5413
  -3.000  -0.3381   0.00874   0.00293  -0.0001   0.6723   0.5536
  -2.750  -0.3094   0.00877   0.00294  -0.0001   0.6688   0.5636
  -2.500  -0.2806   0.00885   0.00297  -0.0003   0.6650   0.5724
  -2.250  -0.2517   0.00884   0.00295  -0.0005   0.6612   0.5797
  -2.000  -0.2229   0.00885   0.00299  -0.0006   0.6572   0.5870
  -1.750  -0.1939   0.00892   0.00300  -0.0008   0.6536   0.5944
  -1.500  -0.1652   0.00894   0.00303  -0.0009   0.6505   0.6008
  -1.250  -0.1363   0.00904   0.00311  -0.0010   0.6472   0.6065
  -1.000  -0.1070   0.00906   0.00312  -0.0013   0.6441   0.6121
  -0.750  -0.0779   0.00904   0.00310  -0.0015   0.6403   0.6164
  -0.500  -0.0489   0.00902   0.00311  -0.0017   0.6365   0.6203
  -0.250  -0.0199   0.00904   0.00311  -0.0018   0.6325   0.6246
   0.000   0.0090   0.00911   0.00313  -0.0020   0.6281   0.6291
   0.250   0.0383   0.00910   0.00312  -0.0022   0.6237   0.6325
   0.500   0.0672   0.00902   0.00309  -0.0024   0.6193   0.6363
   0.750   0.0962   0.00899   0.00308  -0.0026   0.6149   0.6401
   1.000   0.1251   0.00902   0.00307  -0.0027   0.6102   0.6436
   1.250   0.1542   0.00899   0.00308  -0.0030   0.6054   0.6471
   1.500   0.1834   0.00898   0.00306  -0.0032   0.5999   0.6504
   1.750   0.2120   0.00891   0.00299  -0.0033   0.5933   0.6541
   2.000   0.2407   0.00886   0.00298  -0.0034   0.5857   0.6579
   2.250   0.2694   0.00881   0.00297  -0.0035   0.5780   0.6616
   2.500   0.2980   0.00884   0.00296  -0.0036   0.5705   0.6653
   2.750   0.3270   0.00879   0.00295  -0.0037   0.5605   0.6688
   3.000   0.3554   0.00876   0.00292  -0.0038   0.5509   0.6724
   3.250   0.3841   0.00869   0.00294  -0.0039   0.5393   0.6759
   3.500   0.4128   0.00867   0.00295  -0.0040   0.5272   0.6795
   3.750   0.4414   0.00868   0.00296  -0.0041   0.5128   0.6832
   4.000   0.4696   0.00872   0.00298  -0.0042   0.4926   0.6871
   4.250   0.4973   0.00881   0.00304  -0.0042   0.4739   0.6910
   4.500   0.5249   0.00893   0.00316  -0.0042   0.4517   0.6950
   4.750   0.5513   0.00920   0.00331  -0.0041   0.4081   0.6993
   5.000   0.5753   0.00982   0.00359  -0.0038   0.3351   0.7037
   5.250   0.6000   0.01036   0.00393  -0.0036   0.2893   0.7080
   5.500   0.6245   0.01089   0.00428  -0.0035   0.2342   0.7126
   5.750   0.6484   0.01154   0.00469  -0.0033   0.1822   0.7179
   6.000   0.6735   0.01206   0.00507  -0.0032   0.1554   0.7234
   6.250   0.6991   0.01239   0.00539  -0.0031   0.1364   0.7292
   6.500   0.7244   0.01278   0.00572  -0.0030   0.1168   0.7360
   6.750   0.7495   0.01322   0.00607  -0.0029   0.0969   0.7432
   7.000   0.7738   0.01363   0.00645  -0.0026   0.0802   0.7504
   7.250   0.7985   0.01404   0.00684  -0.0024   0.0695   0.7583
   7.500   0.8232   0.01438   0.00723  -0.0022   0.0605   0.7665
   7.750   0.8475   0.01478   0.00762  -0.0019   0.0497   0.7763
   8.000   0.8708   0.01523   0.00809  -0.0016   0.0423   0.7880
   8.250   0.8943   0.01564   0.00856  -0.0012   0.0379   0.8020
   8.500   0.9177   0.01602   0.00901  -0.0008   0.0341   0.8188
   8.750   0.9402   0.01637   0.00947  -0.0002   0.0306   0.8394
   9.000   0.9612   0.01673   0.00994   0.0007   0.0280   0.8658
   9.250   0.9794   0.01707   0.01041   0.0022   0.0261   0.9135
   9.500   1.0092   0.01756   0.01100   0.0011   0.0246   0.9995
   9.750   1.0304   0.01820   0.01164   0.0014   0.0233   0.9995
  10.000   1.0511   0.01884   0.01231   0.0019   0.0220   0.9995
  10.250   1.0699   0.01959   0.01310   0.0024   0.0208   0.9995
  10.500   1.0871   0.02040   0.01395   0.0032   0.0198   0.9995
  10.750   1.1036   0.02114   0.01476   0.0041   0.0187   0.9995
  11.000   1.1169   0.02218   0.01584   0.0049   0.0177   0.9995
  11.250   1.1318   0.02316   0.01689   0.0054   0.0167   0.9995
  11.500   1.1468   0.02418   0.01798   0.0058   0.0155   0.9995
  11.750   1.1597   0.02541   0.01926   0.0061   0.0147   0.9995
  12.000   1.1742   0.02654   0.02048   0.0064   0.0136   0.9995
  12.250   1.1874   0.02781   0.02181   0.0066   0.0128   0.9995
  12.500   1.1996   0.02917   0.02321   0.0068   0.0122   0.9995
  12.750   1.2105   0.03068   0.02479   0.0070   0.0116   0.9995
  13.000   1.2212   0.03221   0.02639   0.0071   0.0111   0.9995
  13.250   1.2312   0.03381   0.02804   0.0073   0.0107   0.9995
  13.500   1.2403   0.03551   0.02978   0.0074   0.0103   0.9995
  13.750   1.2473   0.03742   0.03174   0.0074   0.0101   0.9995
  14.000   1.2519   0.03958   0.03399   0.0075   0.0099   0.9995
  14.250   1.2551   0.04191   0.03641   0.0075   0.0098   0.9995
  14.500   1.2571   0.04440   0.03898   0.0074   0.0097   0.9995
  14.750   1.2576   0.04708   0.04175   0.0072   0.0096   0.9995
  15.000   1.2568   0.04993   0.04470   0.0069   0.0095   0.9995
  15.250   1.2550   0.05296   0.04783   0.0066   0.0094   0.9995
  15.500   1.2524   0.05621   0.05119   0.0060   0.0093   0.9995
  15.750   1.2489   0.05973   0.05481   0.0051   0.0093   0.9995
  16.000   1.2443   0.06354   0.05873   0.0041   0.0092   0.9995
  16.250   1.2385   0.06761   0.06291   0.0028   0.0091   0.9995
  16.500   1.2316   0.07196   0.06737   0.0014   0.0091   0.9995
  16.750   1.2235   0.07661   0.07213  -0.0003   0.0091   0.9995
  17.000   1.2142   0.08156   0.07720  -0.0022   0.0090   0.9995
  17.250   1.2038   0.08682   0.08258  -0.0043   0.0090   0.9995
  17.500   1.1923   0.09237   0.08824  -0.0067   0.0090   0.9995
  17.750   1.1800   0.09817   0.09417  -0.0092   0.0090   0.9995
  18.000   1.1669   0.10425   0.10037  -0.0120   0.0090   0.9995
  18.250   1.1535   0.11046   0.10669  -0.0149   0.0090   0.9995
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