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S1014 (s1014-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: S1014 (s1014-il)
Reynolds number: 200,000
Max Cl/Cd: 33.7 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1014-il-200000.txt
Download as CSV file: xf-s1014-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1014                                           
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.8173   0.11507   0.11119  -0.0414   1.0000   0.0470
 -17.500  -0.8765   0.09942   0.09532  -0.0510   1.0000   0.0462
 -17.250  -0.9219   0.08804   0.08368  -0.0577   1.0000   0.0459
 -17.000  -0.9563   0.07956   0.07495  -0.0621   1.0000   0.0458
 -16.750  -0.9864   0.07255   0.06766  -0.0651   1.0000   0.0459
 -16.500  -1.0102   0.06695   0.06180  -0.0667   1.0000   0.0461
 -16.250  -1.0294   0.06236   0.05695  -0.0675   1.0000   0.0464
 -16.000  -1.0472   0.05839   0.05270  -0.0677   1.0000   0.0468
 -15.750  -1.0553   0.05464   0.04875  -0.0676   1.0000   0.0475
 -15.500  -1.0439   0.05262   0.04676  -0.0679   1.0000   0.0487
 -15.250  -1.0383   0.05061   0.04469  -0.0679   1.0000   0.0498
 -15.000  -1.0360   0.04855   0.04251  -0.0677   1.0000   0.0510
 -14.750  -1.0340   0.04641   0.04021  -0.0672   1.0000   0.0522
 -14.500  -1.0352   0.04444   0.03802  -0.0664   1.0000   0.0538
 -14.250  -1.0374   0.04262   0.03593  -0.0651   1.0000   0.0548
 -14.000  -1.0145   0.04059   0.03390  -0.0662   0.9856   0.0570
 -13.750  -0.9951   0.03925   0.03252  -0.0674   0.9772   0.0591
 -13.500  -0.9789   0.03774   0.03083  -0.0682   0.9712   0.0616
 -13.250  -0.9647   0.03626   0.02908  -0.0686   0.9659   0.0637
 -13.000  -0.9390   0.03470   0.02753  -0.0696   0.9625   0.0668
 -12.750  -0.9202   0.03372   0.02650  -0.0701   0.9585   0.0698
 -12.500  -0.9028   0.03263   0.02522  -0.0701   0.9548   0.0728
 -12.250  -0.8818   0.03143   0.02392  -0.0702   0.9513   0.0761
 -12.000  -0.8624   0.03062   0.02314  -0.0701   0.9478   0.0794
 -11.750  -0.8452   0.02984   0.02225  -0.0697   0.9446   0.0830
 -11.500  -0.8252   0.02895   0.02121  -0.0695   0.9422   0.0869
 -11.250  -0.8027   0.02817   0.02049  -0.0696   0.9402   0.0912
 -11.000  -0.7843   0.02752   0.01977  -0.0692   0.9380   0.0956
 -10.750  -0.7615   0.02674   0.01892  -0.0692   0.9362   0.1004
 -10.500  -0.7417   0.02611   0.01833  -0.0689   0.9342   0.1054
 -10.250  -0.7228   0.02559   0.01769  -0.0684   0.9322   0.1107
 -10.000  -0.6994   0.02487   0.01704  -0.0684   0.9308   0.1166
  -9.750  -0.6801   0.02437   0.01650  -0.0679   0.9291   0.1231
  -9.500  -0.6586   0.02377   0.01592  -0.0676   0.9277   0.1300
  -9.250  -0.6392   0.02331   0.01544  -0.0671   0.9263   0.1374
  -9.000  -0.6194   0.02278   0.01494  -0.0665   0.9249   0.1457
  -8.750  -0.6002   0.02236   0.01449  -0.0659   0.9232   0.1550
  -8.500  -0.5816   0.02181   0.01405  -0.0653   0.9219   0.1651
  -8.250  -0.5633   0.02135   0.01362  -0.0646   0.9206   0.1767
  -8.000  -0.5457   0.02092   0.01323  -0.0638   0.9193   0.1902
  -7.750  -0.5298   0.02048   0.01288  -0.0628   0.9180   0.2057
  -7.500  -0.5164   0.02001   0.01253  -0.0613   0.9167   0.2240
  -7.250  -0.5052   0.01955   0.01221  -0.0596   0.9153   0.2460
  -7.000  -0.4965   0.01909   0.01190  -0.0573   0.9135   0.2733
  -6.750  -0.4926   0.01861   0.01162  -0.0541   0.9116   0.3073
  -6.500  -0.4942   0.01818   0.01141  -0.0501   0.9101   0.3476
  -6.250  -0.5055   0.01798   0.01144  -0.0441   0.9085   0.3885
  -6.000  -0.5384   0.01838   0.01195  -0.0337   0.9052   0.4079
  -5.750  -0.5790   0.01893   0.01254  -0.0214   0.9024   0.4181
  -5.500  -0.6157   0.01915   0.01286  -0.0096   0.9001   0.4378
  -5.250  -0.6334   0.01880   0.01286  -0.0015   0.8981   0.4961
  -5.000  -0.6288   0.01888   0.01369   0.0035   0.8971   0.6043
  -4.750  -0.5837   0.02072   0.01579   0.0024   0.8966   0.6790
  -4.500  -0.5725   0.02116   0.01613   0.0055   0.8949   0.7060
  -4.250  -0.5456   0.02192   0.01679   0.0059   0.8936   0.7253
  -4.000  -0.5583   0.02252   0.01737   0.0136   0.8917   0.7352
  -3.750  -0.5635   0.02290   0.01769   0.0197   0.8896   0.7473
  -3.500  -0.5431   0.02389   0.01867   0.0218   0.8876   0.7555
  -3.250  -0.5267   0.02454   0.01927   0.0243   0.8852   0.7654
  -3.000  -0.4968   0.02553   0.02022   0.0247   0.8832   0.7727
  -2.750  -0.4673   0.02613   0.02075   0.0248   0.8807   0.7814
  -2.500  -0.4111   0.02742   0.02201   0.0209   0.8790   0.7857
  -2.250  -0.4150   0.02748   0.02202   0.0263   0.8750   0.7968
  -2.000  -0.3919   0.02830   0.02284   0.0280   0.8712   0.8008
  -1.750  -0.3882   0.02819   0.02268   0.0319   0.8668   0.8122
  -1.500  -0.3266   0.02946   0.02394   0.0272   0.8648   0.8151
  -1.250  -0.2380   0.03114   0.02560   0.0177   0.8641   0.8195
  -1.000  -0.1857   0.03185   0.02627   0.0138   0.8623   0.8301
  -0.750  -0.0855   0.03257   0.02697   0.0008   0.8625   0.8313
  -0.500  -0.1571   0.03243   0.02685   0.0189   0.8505   0.8461
  -0.250  -0.0743   0.03281   0.02722   0.0087   0.8494   0.8469
   0.000   0.0001   0.03291   0.02732   0.0000   0.8481   0.8481
   0.250   0.0745   0.03281   0.02722  -0.0087   0.8469   0.8494
   0.500   0.1575   0.03242   0.02684  -0.0190   0.8461   0.8505
   0.750   0.0853   0.03257   0.02698  -0.0008   0.8314   0.8626
   1.000   0.1863   0.03183   0.02626  -0.0139   0.8301   0.8623
   1.250   0.2405   0.03107   0.02553  -0.0181   0.8194   0.8640
   1.500   0.3260   0.02950   0.02397  -0.0271   0.8152   0.8648
   1.750   0.3880   0.02821   0.02270  -0.0319   0.8122   0.8669
   2.000   0.3918   0.02829   0.02284  -0.0280   0.8008   0.8713
   2.250   0.4145   0.02749   0.02204  -0.0263   0.7968   0.8750
   2.500   0.4104   0.02745   0.02204  -0.0208   0.7858   0.8790
   2.750   0.4669   0.02615   0.02077  -0.0248   0.7815   0.8807
   3.000   0.4966   0.02552   0.02021  -0.0247   0.7727   0.8832
   3.250   0.5265   0.02453   0.01926  -0.0243   0.7654   0.8852
   3.500   0.5429   0.02390   0.01868  -0.0218   0.7557   0.8875
   3.750   0.5631   0.02291   0.01771  -0.0196   0.7474   0.8896
   4.000   0.5579   0.02251   0.01736  -0.0136   0.7351   0.8917
   4.250   0.5456   0.02192   0.01679  -0.0060   0.7253   0.8936
   4.500   0.5726   0.02114   0.01611  -0.0055   0.7054   0.8950
   4.750   0.5832   0.02071   0.01578  -0.0023   0.6790   0.8965
   5.000   0.6285   0.01888   0.01369  -0.0035   0.6048   0.8971
   5.250   0.6333   0.01879   0.01285   0.0015   0.4965   0.8981
   5.500   0.6157   0.01914   0.01285   0.0096   0.4382   0.9001
   5.750   0.5792   0.01892   0.01254   0.0214   0.4185   0.9024
   6.000   0.5386   0.01838   0.01195   0.0337   0.4080   0.9052
   6.250   0.5054   0.01798   0.01144   0.0441   0.3882   0.9085
   6.500   0.4945   0.01817   0.01141   0.0500   0.3478   0.9101
   6.750   0.4926   0.01861   0.01161   0.0541   0.3070   0.9117
   7.000   0.4966   0.01909   0.01190   0.0572   0.2731   0.9136
   7.250   0.5053   0.01955   0.01221   0.0595   0.2458   0.9153
   7.500   0.5165   0.02001   0.01253   0.0613   0.2238   0.9167
   7.750   0.5300   0.02048   0.01287   0.0627   0.2056   0.9180
   8.000   0.5460   0.02092   0.01323   0.0638   0.1903   0.9193
   8.250   0.5636   0.02134   0.01362   0.0646   0.1767   0.9206
   8.500   0.5819   0.02181   0.01404   0.0653   0.1650   0.9219
   8.750   0.6005   0.02235   0.01448   0.0659   0.1550   0.9233
   9.000   0.6198   0.02277   0.01494   0.0664   0.1457   0.9250
   9.250   0.6396   0.02330   0.01543   0.0670   0.1374   0.9264
   9.500   0.6590   0.02377   0.01591   0.0675   0.1299   0.9277
   9.750   0.6805   0.02437   0.01649   0.0678   0.1229   0.9291
  10.000   0.7000   0.02486   0.01703   0.0683   0.1167   0.9308
  10.250   0.7229   0.02557   0.01768   0.0684   0.1106   0.9323
  10.500   0.7419   0.02610   0.01832   0.0689   0.1053   0.9343
  10.750   0.7622   0.02674   0.01892   0.0691   0.1003   0.9362
  11.000   0.7844   0.02751   0.01976   0.0692   0.0954   0.9381
  11.250   0.8030   0.02815   0.02047   0.0696   0.0911   0.9403
  11.500   0.8265   0.02896   0.02121   0.0693   0.0868   0.9422
  11.750   0.8456   0.02983   0.02224   0.0696   0.0830   0.9447
  12.000   0.8630   0.03062   0.02314   0.0700   0.0793   0.9479
  12.250   0.8824   0.03142   0.02390   0.0701   0.0760   0.9515
  12.500   0.9033   0.03262   0.02522   0.0700   0.0727   0.9549
  12.750   0.9206   0.03371   0.02649   0.0700   0.0696   0.9587
  13.000   0.9401   0.03470   0.02753   0.0695   0.0668   0.9626
  13.250   0.9656   0.03624   0.02906   0.0685   0.0637   0.9661
  13.500   0.9792   0.03771   0.03081   0.0681   0.0614   0.9715
  13.750   0.9964   0.03925   0.03252   0.0672   0.0591   0.9775
  14.000   1.0160   0.04057   0.03388   0.0660   0.0570   0.9861
  14.250   1.0380   0.04262   0.03593   0.0650   0.0548   1.0000
  14.500   1.0358   0.04444   0.03802   0.0663   0.0537   1.0000
  14.750   1.0357   0.04647   0.04026   0.0670   0.0524   1.0000
  15.000   1.0373   0.04852   0.04248   0.0675   0.0510   1.0000
  15.250   1.0395   0.05062   0.04470   0.0677   0.0498   1.0000
  15.500   1.0459   0.05253   0.04666   0.0677   0.0487   1.0000
  15.750   1.0570   0.05463   0.04874   0.0674   0.0475   1.0000
  16.000   1.0490   0.05833   0.05264   0.0675   0.0468   1.0000
  16.250   1.0306   0.06238   0.05697   0.0674   0.0464   1.0000
  16.500   1.0106   0.06706   0.06192   0.0665   0.0461   1.0000
  16.750   0.9873   0.07256   0.06768   0.0649   0.0458   1.0000
  17.000   0.9590   0.07935   0.07473   0.0620   0.0457   1.0000
  17.250   0.9220   0.08821   0.08386   0.0574   0.0458   1.0000
  17.500   0.8790   0.09921   0.09511   0.0509   0.0462   1.0000
  17.750   0.8136   0.11615   0.11229   0.0404   0.0470   1.0000
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