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WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il)
Reynolds number: 100,000
Max Cl/Cd: 38.24 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxlv152-il-100000-n5.txt
Download as CSV file: xf-fxlv152-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.8423   0.15607   0.15128   0.0368   1.0005   0.0246
 -16.500  -0.9297   0.12703   0.12183   0.0206   1.0005   0.0232
 -16.250  -0.9487   0.11809   0.11273   0.0154   1.0005   0.0233
 -16.000  -0.9649   0.11016   0.10464   0.0109   1.0005   0.0235
 -15.750  -0.9793   0.10291   0.09722   0.0068   1.0005   0.0238
 -15.500  -0.9926   0.09620   0.09035   0.0032   1.0005   0.0242
 -15.250  -1.0049   0.08992   0.08388   0.0001   1.0005   0.0249
 -15.000  -1.0156   0.08421   0.07799  -0.0026   1.0005   0.0256
 -14.750  -1.0231   0.07930   0.07298  -0.0050   1.0005   0.0262
 -14.500  -1.0300   0.07466   0.06822  -0.0071   1.0005   0.0271
 -14.250  -1.0360   0.07032   0.06368  -0.0087   1.0005   0.0284
 -14.000  -1.0403   0.06650   0.05974  -0.0101   1.0005   0.0295
 -13.750  -1.0430   0.06295   0.05604  -0.0112   1.0005   0.0309
 -13.500  -1.0439   0.05966   0.05258  -0.0120   1.0005   0.0327
 -13.250  -1.0437   0.05665   0.04944  -0.0128   1.0005   0.0345
 -13.000  -1.0415   0.05386   0.04648  -0.0133   1.0005   0.0366
 -12.750  -1.0386   0.05128   0.04379  -0.0137   1.0005   0.0384
 -12.500  -1.0333   0.04894   0.04128  -0.0137   1.0005   0.0403
 -12.250  -1.0283   0.04667   0.03895  -0.0139   1.0005   0.0419
 -12.000  -1.0210   0.04461   0.03674  -0.0138   1.0005   0.0440
 -11.750  -1.0139   0.04261   0.03470  -0.0138   1.0005   0.0459
 -11.500  -1.0049   0.04079   0.03277  -0.0137   1.0005   0.0485
 -11.250  -0.9959   0.03903   0.03096  -0.0136   1.0005   0.0508
 -11.000  -0.9852   0.03740   0.02922  -0.0133   1.0005   0.0535
 -10.750  -0.9748   0.03580   0.02756  -0.0131   1.0005   0.0561
 -10.500  -0.9627   0.03435   0.02600  -0.0127   1.0005   0.0597
 -10.250  -0.9515   0.03289   0.02450  -0.0124   1.0005   0.0636
 -10.000  -0.9397   0.03151   0.02307  -0.0120   1.0005   0.0685
  -9.750  -0.9277   0.03019   0.02173  -0.0115   1.0005   0.0741
  -9.500  -0.9154   0.02898   0.02051  -0.0108   1.0005   0.0806
  -9.250  -0.9022   0.02788   0.01942  -0.0100   1.0005   0.0879
  -9.000  -0.8866   0.02683   0.01837  -0.0095   1.0005   0.0960
  -8.750  -0.8698   0.02585   0.01738  -0.0090   1.0005   0.1049
  -8.500  -0.8524   0.02489   0.01645  -0.0085   1.0005   0.1153
  -8.250  -0.8341   0.02397   0.01556  -0.0082   1.0005   0.1270
  -8.000  -0.8152   0.02308   0.01471  -0.0079   1.0005   0.1404
  -7.500  -0.7633   0.02130   0.01296  -0.0100   0.9213   0.1783
  -7.250  -0.7421   0.02041   0.01219  -0.0100   0.8949   0.2066
  -7.000  -0.7237   0.01952   0.01147  -0.0093   0.8745   0.2461
  -6.750  -0.7053   0.01872   0.01082  -0.0085   0.8587   0.3003
  -6.500  -0.6869   0.01803   0.01039  -0.0073   0.8458   0.3522
  -6.250  -0.6658   0.01769   0.01026  -0.0063   0.8339   0.4064
  -6.000  -0.6418   0.01756   0.01012  -0.0057   0.8239   0.4457
  -5.750  -0.6168   0.01756   0.01009  -0.0050   0.8152   0.4721
  -5.500  -0.5908   0.01764   0.01014  -0.0044   0.8063   0.4938
  -5.250  -0.5650   0.01775   0.01013  -0.0039   0.7975   0.5148
  -5.000  -0.5389   0.01785   0.01009  -0.0034   0.7889   0.5337
  -4.750  -0.5126   0.01797   0.01009  -0.0029   0.7807   0.5490
  -4.500  -0.4863   0.01802   0.00998  -0.0025   0.7742   0.5619
  -4.250  -0.4594   0.01808   0.00993  -0.0023   0.7675   0.5736
  -4.000  -0.4324   0.01820   0.00997  -0.0018   0.7620   0.5829
  -3.750  -0.4060   0.01824   0.00985  -0.0015   0.7574   0.5940
  -3.500  -0.3782   0.01839   0.01000  -0.0013   0.7516   0.6021
  -3.250  -0.3511   0.01840   0.00988  -0.0012   0.7462   0.6120
  -3.000  -0.3239   0.01844   0.00985  -0.0009   0.7415   0.6185
  -2.750  -0.2962   0.01842   0.00976  -0.0009   0.7363   0.6242
  -2.500  -0.2687   0.01830   0.00952  -0.0012   0.7306   0.6307
  -2.250  -0.2412   0.01824   0.00940  -0.0012   0.7259   0.6355
  -2.000  -0.2137   0.01824   0.00935  -0.0010   0.7221   0.6405
  -1.750  -0.1862   0.01822   0.00927  -0.0012   0.7170   0.6482
  -1.500  -0.1589   0.01823   0.00929  -0.0012   0.7117   0.6549
  -1.250  -0.1317   0.01826   0.00930  -0.0009   0.7070   0.6610
  -1.000  -0.1043   0.01821   0.00916  -0.0009   0.7033   0.6674
  -0.750  -0.0765   0.01819   0.00916  -0.0012   0.6985   0.6720
  -0.500  -0.0488   0.01821   0.00920  -0.0012   0.6936   0.6760
  -0.250  -0.0213   0.01818   0.00916  -0.0012   0.6891   0.6806
   0.000   0.0064   0.01814   0.00905  -0.0013   0.6854   0.6855
   0.250   0.0343   0.01815   0.00908  -0.0016   0.6807   0.6895
   0.500   0.0619   0.01820   0.00919  -0.0017   0.6760   0.6932
   0.750   0.0895   0.01824   0.00925  -0.0017   0.6718   0.6979
   1.000   0.1172   0.01822   0.00919  -0.0017   0.6675   0.7031
   1.250   0.1445   0.01824   0.00926  -0.0018   0.6607   0.7077
   1.500   0.1716   0.01824   0.00930  -0.0016   0.6536   0.7115
   1.750   0.1990   0.01820   0.00925  -0.0014   0.6482   0.7162
   2.000   0.2263   0.01827   0.00940  -0.0016   0.6410   0.7218
   2.250   0.2537   0.01832   0.00952  -0.0017   0.6353   0.7265
   2.500   0.2811   0.01833   0.00958  -0.0015   0.6306   0.7308
   2.750   0.3084   0.01841   0.00976  -0.0016   0.6247   0.7357
   3.000   0.3359   0.01846   0.00988  -0.0017   0.6172   0.7412
   3.250   0.3632   0.01836   0.00984  -0.0013   0.6109   0.7457
   3.500   0.3896   0.01838   0.01000  -0.0011   0.6008   0.7509
   3.750   0.4171   0.01822   0.00987  -0.0007   0.5923   0.7570
   4.000   0.4435   0.01822   0.01002  -0.0005   0.5819   0.7626
   4.250   0.4704   0.01810   0.00998   0.0000   0.5735   0.7677
   4.500   0.4965   0.01808   0.01010   0.0003   0.5610   0.7738
   4.750   0.5230   0.01794   0.01006   0.0008   0.5477   0.7805
   5.000   0.5490   0.01780   0.01002   0.0015   0.5327   0.7878
   5.250   0.5747   0.01773   0.01009   0.0019   0.5134   0.7971
   5.500   0.5996   0.01764   0.01014   0.0026   0.4918   0.8056
   5.750   0.6251   0.01758   0.01012   0.0032   0.4692   0.8153
   6.000   0.6492   0.01760   0.01019   0.0041   0.4411   0.8237
   6.250   0.6725   0.01774   0.01029   0.0049   0.4012   0.8339
   6.500   0.6925   0.01811   0.01045   0.0061   0.3472   0.8447
   6.750   0.7101   0.01881   0.01090   0.0073   0.2959   0.8570
   7.000   0.7272   0.01961   0.01154   0.0085   0.2432   0.8721
   7.250   0.7445   0.02046   0.01225   0.0094   0.2052   0.8924
   7.500   0.7647   0.02130   0.01300   0.0097   0.1786   0.9192
   7.750   0.7918   0.02225   0.01391   0.0085   0.1577   0.9539
   8.000   0.8154   0.02312   0.01476   0.0078   0.1407   0.9995
   8.250   0.8339   0.02398   0.01559   0.0082   0.1269   0.9995
   8.500   0.8517   0.02487   0.01646   0.0087   0.1151   0.9995
   8.750   0.8685   0.02581   0.01737   0.0092   0.1046   0.9995
   9.000   0.8842   0.02680   0.01835   0.0099   0.0959   0.9995
   9.250   0.8985   0.02785   0.01939   0.0106   0.0880   0.9995
   9.500   0.9103   0.02897   0.02049   0.0116   0.0813   0.9995
   9.750   0.9223   0.03019   0.02172   0.0122   0.0749   0.9995
  10.000   0.9343   0.03148   0.02305   0.0128   0.0691   0.9995
  10.250   0.9460   0.03284   0.02446   0.0133   0.0640   0.9995
  10.500   0.9572   0.03427   0.02594   0.0137   0.0599   0.9995
  10.750   0.9682   0.03575   0.02751   0.0141   0.0566   0.9995
  11.000   0.9786   0.03732   0.02916   0.0145   0.0540   0.9995
  11.250   0.9884   0.03895   0.03088   0.0148   0.0515   0.9995
  11.500   0.9974   0.04067   0.03266   0.0150   0.0490   0.9995
  11.750   1.0057   0.04247   0.03455   0.0152   0.0465   0.9995
  12.000   1.0129   0.04440   0.03656   0.0153   0.0442   0.9995
  12.250   1.0193   0.04645   0.03872   0.0153   0.0422   0.9995
  12.500   1.0240   0.04867   0.04098   0.0153   0.0409   0.9995
  12.750   1.0295   0.05092   0.04342   0.0155   0.0391   0.9995
  13.000   1.0322   0.05342   0.04601   0.0153   0.0375   0.9995
  13.250   1.0340   0.05612   0.04887   0.0150   0.0355   0.9995
  13.500   1.0340   0.05904   0.05193   0.0143   0.0336   0.9995
  13.750   1.0329   0.06221   0.05527   0.0136   0.0318   0.9995
  14.000   1.0302   0.06563   0.05884   0.0127   0.0303   0.9995
  14.250   1.0259   0.06930   0.06260   0.0114   0.0292   0.9995
  14.500   1.0201   0.07346   0.06698   0.0101   0.0279   0.9995
  14.750   1.0132   0.07791   0.07157   0.0083   0.0269   0.9995
  15.000   1.0057   0.08266   0.07641   0.0061   0.0262   0.9995
  15.250   0.9955   0.08804   0.08196   0.0036   0.0255   0.9995
  15.500   0.9832   0.09404   0.08815   0.0008   0.0249   0.9995
  15.750   0.9697   0.10053   0.09480  -0.0025   0.0244   0.9995
  16.000   0.9549   0.10752   0.10195  -0.0063   0.0241   0.9995
  16.250   0.9385   0.11519   0.10977  -0.0105   0.0239   0.9995
  16.500   0.9188   0.12388   0.11863  -0.0153   0.0237   0.9995
  16.750   0.8726   0.14001   0.13507  -0.0244   0.0243   0.9995
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