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WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il)
Reynolds number: 1,000,000
Max Cl/Cd: 62.59 at α=8.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxlv152-il-1000000-n5.txt
Download as CSV file: xf-fxlv152-il-1000000-n5.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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -1.1498   0.12171   0.11852   0.0266   1.0005   0.0034
 -18.250  -1.1687   0.11391   0.11060   0.0226   1.0005   0.0034
 -18.000  -1.1860   0.10659   0.10316   0.0190   1.0005   0.0034
 -17.750  -1.2030   0.09944   0.09589   0.0155   1.0005   0.0034
 -17.500  -1.2184   0.09275   0.08908   0.0123   1.0005   0.0034
 -17.250  -1.2312   0.08663   0.08285   0.0095   1.0005   0.0034
 -17.000  -1.2426   0.08094   0.07704   0.0070   1.0005   0.0034
 -16.750  -1.2515   0.07581   0.07180   0.0049   1.0005   0.0034
 -16.500  -1.2594   0.07094   0.06683   0.0029   1.0005   0.0034
 -16.250  -1.2654   0.06650   0.06229   0.0013   1.0005   0.0034
 -16.000  -1.2693   0.06249   0.05818  -0.0002   1.0005   0.0034
 -15.750  -1.2721   0.05874   0.05434  -0.0014   1.0005   0.0035
 -15.500  -1.2790   0.05466   0.05015  -0.0026   1.0005   0.0035
 -15.250  -1.2858   0.05080   0.04618  -0.0034   1.0005   0.0035
 -15.000  -1.2913   0.04726   0.04254  -0.0041   1.0005   0.0036
 -14.750  -1.2946   0.04401   0.03919  -0.0046   1.0005   0.0036
 -14.500  -1.2960   0.04106   0.03615  -0.0049   1.0005   0.0037
 -14.250  -1.2946   0.03845   0.03345  -0.0051   1.0005   0.0037
 -14.000  -1.2914   0.03606   0.03098  -0.0052   1.0005   0.0038
 -13.750  -1.2865   0.03386   0.02871  -0.0053   1.0005   0.0038
 -13.500  -1.2800   0.03184   0.02661  -0.0053   1.0005   0.0039
 -13.250  -1.2720   0.03000   0.02470  -0.0052   1.0005   0.0039
 -13.000  -1.2626   0.02831   0.02295  -0.0051   1.0005   0.0040
 -12.750  -1.2521   0.02673   0.02131  -0.0050   1.0005   0.0040
 -12.500  -1.2407   0.02529   0.01980  -0.0048   1.0005   0.0041
 -12.250  -1.2298   0.02424   0.01847  -0.0040   0.8623   0.0042
 -12.000  -1.2174   0.02315   0.01721  -0.0035   0.8299   0.0042
 -11.750  -1.2037   0.02213   0.01605  -0.0029   0.8026   0.0043
 -11.500  -1.1890   0.02122   0.01500  -0.0023   0.7750   0.0044
 -11.250  -1.1734   0.02044   0.01410  -0.0015   0.7615   0.0044
 -11.000  -1.1557   0.01975   0.01332  -0.0007   0.7521   0.0045
 -10.750  -1.1359   0.01911   0.01259  -0.0002   0.7437   0.0045
 -10.500  -1.1149   0.01850   0.01192   0.0002   0.7367   0.0046
 -10.250  -1.0932   0.01794   0.01130   0.0005   0.7279   0.0047
 -10.000  -1.0707   0.01742   0.01070   0.0008   0.7189   0.0047
  -9.750  -1.0476   0.01693   0.01015   0.0011   0.7075   0.0048
  -9.500  -1.0240   0.01647   0.00962   0.0013   0.6968   0.0049
  -9.000  -0.9756   0.01560   0.00862   0.0017   0.6810   0.0052
  -8.750  -0.9509   0.01518   0.00814   0.0018   0.6754   0.0054
  -8.500  -0.9258   0.01479   0.00769   0.0019   0.6696   0.0056
  -8.250  -0.9005   0.01441   0.00727   0.0020   0.6646   0.0059
  -8.000  -0.8747   0.01404   0.00687   0.0020   0.6605   0.0062
  -7.750  -0.8489   0.01368   0.00649   0.0021   0.6564   0.0073
  -7.500  -0.8228   0.01334   0.00617   0.0021   0.6526   0.0133
  -7.250  -0.7958   0.01312   0.00592   0.0020   0.6490   0.0144
  -7.000  -0.7689   0.01286   0.00565   0.0019   0.6460   0.0153
  -6.750  -0.7417   0.01262   0.00540   0.0018   0.6429   0.0161
  -6.500  -0.7143   0.01240   0.00516   0.0017   0.6393   0.0167
  -6.250  -0.6869   0.01218   0.00492   0.0016   0.6353   0.0173
  -6.000  -0.6596   0.01193   0.00465   0.0015   0.6314   0.0181
  -5.750  -0.6322   0.01171   0.00441   0.0014   0.6279   0.0191
  -5.500  -0.6044   0.01150   0.00419   0.0012   0.6250   0.0199
  -5.250  -0.5767   0.01128   0.00396   0.0011   0.6215   0.0212
  -5.000  -0.5491   0.01103   0.00372   0.0010   0.6182   0.0240
  -4.750  -0.5220   0.01070   0.00346   0.0009   0.6148   0.0410
  -4.500  -0.4950   0.01035   0.00320   0.0008   0.6113   0.0619
  -4.250  -0.4671   0.01015   0.00302   0.0006   0.6079   0.0717
  -4.000  -0.4402   0.00974   0.00276   0.0005   0.6043   0.1034
  -3.750  -0.4133   0.00935   0.00253   0.0004   0.6008   0.1395
  -3.500  -0.3855   0.00909   0.00235   0.0003   0.5972   0.1611
  -3.250  -0.3587   0.00868   0.00211   0.0002   0.5939   0.2066
  -2.750  -0.3040   0.00801   0.00176  -0.0001   0.5884   0.2907
  -2.500  -0.2761   0.00775   0.00161  -0.0003   0.5859   0.3209
  -2.250  -0.2495   0.00730   0.00142  -0.0003   0.5830   0.3872
  -2.000  -0.2219   0.00702   0.00132  -0.0005   0.5798   0.4348
  -1.750  -0.1936   0.00689   0.00126  -0.0006   0.5760   0.4638
  -1.500  -0.1653   0.00678   0.00121  -0.0007   0.5718   0.4851
  -1.000  -0.1073   0.00665   0.00120  -0.0012   0.5667   0.5188
  -0.750  -0.0782   0.00662   0.00121  -0.0014   0.5637   0.5346
  -0.500  -0.0490   0.00661   0.00122  -0.0016   0.5602   0.5438
  -0.250  -0.0198   0.00661   0.00122  -0.0019   0.5570   0.5504
   0.000   0.0095   0.00664   0.00122  -0.0021   0.5534   0.5546
   0.250   0.0390   0.00664   0.00122  -0.0024   0.5489   0.5575
   0.500   0.0683   0.00662   0.00121  -0.0026   0.5409   0.5608
   0.750   0.0972   0.00663   0.00121  -0.0028   0.5314   0.5643
   1.000   0.1264   0.00664   0.00121  -0.0031   0.5188   0.5686
   1.500   0.1835   0.00684   0.00123  -0.0034   0.4739   0.5754
   1.750   0.2120   0.00696   0.00128  -0.0035   0.4534   0.5773
   2.000   0.2399   0.00713   0.00135  -0.0036   0.4203   0.5800
   2.250   0.2665   0.00748   0.00148  -0.0036   0.3590   0.5826
   2.500   0.2935   0.00780   0.00165  -0.0036   0.3165   0.5854
   2.750   0.3210   0.00806   0.00180  -0.0037   0.2864   0.5885
   3.250   0.3745   0.00881   0.00218  -0.0038   0.1906   0.5937
   3.750   0.4284   0.00946   0.00259  -0.0038   0.1304   0.5999
   4.000   0.4545   0.00988   0.00284  -0.0038   0.0893   0.6039
   4.250   0.4814   0.01021   0.00307  -0.0038   0.0684   0.6079
   4.500   0.5084   0.01052   0.00330  -0.0039   0.0481   0.6115
   5.000   0.5622   0.01111   0.00379  -0.0039   0.0225   0.6182
   5.250   0.5895   0.01134   0.00402  -0.0040   0.0206   0.6217
   5.500   0.6170   0.01154   0.00424  -0.0040   0.0196   0.6251
   5.750   0.6442   0.01177   0.00448  -0.0041   0.0185   0.6287
   6.000   0.6713   0.01202   0.00474  -0.0041   0.0176   0.6318
   6.250   0.6985   0.01223   0.00496  -0.0041   0.0171   0.6348
   6.500   0.7255   0.01243   0.00519  -0.0042   0.0164   0.6383
   6.750   0.7524   0.01266   0.00544  -0.0042   0.0156   0.6423
   7.000   0.7790   0.01292   0.00571  -0.0042   0.0147   0.6463
   7.250   0.8058   0.01315   0.00595  -0.0042   0.0140   0.6499
   7.500   0.8320   0.01343   0.00623  -0.0041   0.0079   0.6534
   7.750   0.8572   0.01380   0.00660  -0.0040   0.0063   0.6575
   8.000   0.8825   0.01415   0.00699  -0.0038   0.0059   0.6618
   8.250   0.9076   0.01451   0.00739  -0.0037   0.0056   0.6658
   8.500   0.9325   0.01490   0.00781  -0.0035   0.0053   0.6695
   8.750   0.9570   0.01529   0.00826  -0.0032   0.0051   0.6744
   9.000   0.9813   0.01568   0.00870  -0.0030   0.0050   0.6799
   9.250   1.0053   0.01609   0.00918  -0.0028   0.0049   0.6858
   9.500   1.0288   0.01652   0.00967  -0.0024   0.0048   0.6938
   9.750   1.0518   0.01698   0.01020  -0.0021   0.0047   0.7040
  10.000   1.0741   0.01747   0.01077  -0.0017   0.0047   0.7151
  10.250   1.0959   0.01800   0.01136  -0.0012   0.0046   0.7249
  10.500   1.1168   0.01856   0.01199  -0.0007   0.0045   0.7349
  10.750   1.1369   0.01916   0.01266  -0.0002   0.0045   0.7436
  11.000   1.1556   0.01980   0.01339   0.0005   0.0044   0.7527
  11.250   1.1712   0.02048   0.01416   0.0016   0.0044   0.7627
  11.500   1.1872   0.02129   0.01509   0.0023   0.0043   0.7777
  11.750   1.2016   0.02221   0.01615   0.0030   0.0042   0.8062
  12.000   1.2148   0.02324   0.01732   0.0036   0.0042   0.8337
  12.250   1.2264   0.02434   0.01860   0.0043   0.0041   0.8682
  12.500   1.2357   0.02541   0.01994   0.0053   0.0040   0.9995
  12.750   1.2466   0.02688   0.02146   0.0055   0.0040   0.9995
  13.000   1.2566   0.02845   0.02310   0.0057   0.0040   0.9995
  13.250   1.2653   0.03014   0.02486   0.0059   0.0039   0.9995
  13.500   1.2728   0.03197   0.02676   0.0061   0.0039   0.9995
  13.750   1.2790   0.03395   0.02881   0.0062   0.0039   0.9995
  14.000   1.2837   0.03609   0.03102   0.0062   0.0038   0.9995
  14.250   1.2869   0.03839   0.03340   0.0063   0.0038   0.9995
  14.500   1.2888   0.04085   0.03594   0.0062   0.0038   0.9995
  14.750   1.2888   0.04354   0.03872   0.0061   0.0038   0.9995
  15.000   1.2875   0.04642   0.04169   0.0058   0.0038   0.9995
  15.250   1.2846   0.04951   0.04487   0.0055   0.0037   0.9995
  15.500   1.2802   0.05287   0.04832   0.0049   0.0037   0.9995
  15.750   1.2751   0.05651   0.05206   0.0041   0.0037   0.9995
  16.000   1.2693   0.06040   0.05605   0.0031   0.0037   0.9995
  16.250   1.2616   0.06471   0.06047   0.0017   0.0037   0.9995
  16.500   1.2531   0.06927   0.06513   0.0002   0.0037   0.9995
  16.750   1.2429   0.07421   0.07018  -0.0016   0.0036   0.9995
  17.000   1.2314   0.07951   0.07559  -0.0036   0.0036   0.9995
  17.250   1.2184   0.08521   0.08140  -0.0060   0.0036   0.9995
  17.500   1.2042   0.09126   0.08756  -0.0085   0.0036   0.9995
  17.750   1.1889   0.09765   0.09407  -0.0114   0.0036   0.9995
  18.000   1.1730   0.10427   0.10081  -0.0144   0.0036   0.9995
  18.250   1.1559   0.11126   0.10791  -0.0176   0.0036   0.9995
  18.500   1.1393   0.11824   0.11501  -0.0210   0.0036   0.9995
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