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SPICA 11.73% smoothed (spicasm-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: SPICA 11.73% smoothed (spicasm-il)
Reynolds number: 100,000
Max Cl/Cd: 50.89 at α=8.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-spicasm-il-100000.txt
Download as CSV file: xf-spicasm-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SPICA  11.73% smoothed                          
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.500  -0.2803   0.11123   0.10637  -0.0404   1.0000   0.0785
  -9.250  -0.2955   0.11051   0.10577  -0.0427   1.0000   0.0790
  -9.000  -0.3115   0.10950   0.10490  -0.0437   1.0000   0.0791
  -8.750  -0.2741   0.10143   0.09678  -0.0395   1.0000   0.0812
  -8.500  -0.2671   0.09860   0.09401  -0.0378   1.0000   0.0829
  -8.250  -0.2686   0.09654   0.09205  -0.0365   1.0000   0.0846
  -8.000  -0.2792   0.09527   0.09092  -0.0342   1.0000   0.0859
  -7.750  -0.3116   0.09626   0.09212  -0.0281   1.0000   0.0855
  -7.500  -0.3116   0.09425   0.09018  -0.0303   0.9943   0.0876
  -7.250  -0.2920   0.08948   0.08533  -0.0513   0.9735   0.0928
  -7.000  -0.2701   0.08340   0.07922  -0.0584   0.9626   0.0945
  -6.750  -0.2385   0.07961   0.07547  -0.0561   0.9591   0.0985
  -6.500  -0.2124   0.07543   0.07121  -0.0637   0.9471   0.1049
  -6.250  -0.1899   0.06993   0.06553  -0.0757   0.9336   0.1105
  -6.000  -0.1558   0.06609   0.06172  -0.0774   0.9292   0.1152
  -5.750  -0.1325   0.06211   0.05736  -0.0878   0.9153   0.1258
  -5.500  -0.1017   0.05813   0.05350  -0.0883   0.9102   0.1300
  -5.250  -0.0788   0.05498   0.05004  -0.0937   0.8982   0.1427
  -5.000  -0.0562   0.05215   0.04730  -0.0933   0.8888   0.1483
  -4.750  -0.0287   0.04901   0.04398  -0.0965   0.8811   0.1625
  -4.500  -0.0122   0.04696   0.04182  -0.0968   0.8694   0.1781
  -4.250   0.0106   0.04476   0.03957  -0.0971   0.8613   0.1971
  -4.000   0.0279   0.04322   0.03785  -0.0972   0.8512   0.2261
  -3.750   0.0453   0.04125   0.03594  -0.0959   0.8423   0.2459
  -3.500   0.0640   0.03958   0.03426  -0.0947   0.8343   0.2794
  -3.000   0.0935   0.03683   0.03160  -0.0899   0.8179   0.3609
  -2.750   0.1058   0.03562   0.03049  -0.0864   0.8094   0.3996
  -2.500   0.1925   0.02957   0.02127  -0.0972   0.8028   0.1096
  -2.250   0.2188   0.02814   0.01967  -0.0966   0.7959   0.1070
  -2.000   0.2430   0.02680   0.01815  -0.0958   0.7880   0.1037
  -1.750   0.2752   0.02543   0.01644  -0.0956   0.7829   0.0994
  -1.500   0.2959   0.02490   0.01571  -0.0941   0.7737   0.0976
  -1.250   0.3267   0.02399   0.01462  -0.0939   0.7681   0.0976
  -1.000   0.3488   0.02361   0.01422  -0.0928   0.7598   0.1000
  -0.750   0.3768   0.02309   0.01362  -0.0923   0.7534   0.1054
  -0.500   0.4012   0.02272   0.01321  -0.0913   0.7463   0.1095
  -0.250   0.4243   0.02216   0.01279  -0.0902   0.7389   0.1163
   0.000   0.4518   0.02164   0.01225  -0.0895   0.7335   0.1307
   0.250   0.4707   0.02151   0.01225  -0.0880   0.7246   0.1608
   0.500   0.5653   0.01868   0.01133  -0.0997   0.7194   1.0000
   0.750   0.5826   0.01917   0.01170  -0.0979   0.7105   1.0000
   1.000   0.6085   0.01930   0.01164  -0.0972   0.7039   1.0000
   1.250   0.6268   0.01978   0.01202  -0.0955   0.6953   1.0000
   1.500   0.6524   0.01991   0.01201  -0.0947   0.6883   1.0000
   1.750   0.6716   0.02035   0.01238  -0.0932   0.6798   1.0000
   2.000   0.6974   0.02047   0.01237  -0.0924   0.6724   1.0000
   2.250   0.7171   0.02089   0.01274  -0.0909   0.6637   1.0000
   2.500   0.7438   0.02095   0.01269  -0.0902   0.6562   1.0000
   2.750   0.7633   0.02137   0.01308  -0.0887   0.6470   1.0000
   3.000   0.7911   0.02139   0.01299  -0.0882   0.6397   1.0000
   3.250   0.8101   0.02183   0.01344  -0.0866   0.6301   1.0000
   3.500   0.8392   0.02180   0.01329  -0.0863   0.6231   1.0000
   3.750   0.8573   0.02228   0.01380  -0.0846   0.6131   1.0000
   4.000   0.8881   0.02218   0.01360  -0.0845   0.6064   1.0000
   4.250   0.9051   0.02270   0.01417  -0.0827   0.5958   1.0000
   4.500   0.9359   0.02261   0.01397  -0.0826   0.5890   1.0000
   4.750   0.9539   0.02303   0.01445  -0.0810   0.5781   1.0000
   5.000   0.9777   0.02323   0.01466  -0.0800   0.5691   1.0000
   5.250   1.0044   0.02324   0.01463  -0.0794   0.5600   1.0000
   5.500   1.0237   0.02361   0.01506  -0.0779   0.5493   1.0000
   5.750   1.0559   0.02340   0.01475  -0.0780   0.5415   1.0000
   6.000   1.0738   0.02374   0.01518  -0.0762   0.5296   1.0000
   6.250   1.0947   0.02399   0.01547  -0.0749   0.5186   1.0000
   6.500   1.1250   0.02381   0.01522  -0.0748   0.5096   1.0000
   6.750   1.1450   0.02404   0.01552  -0.0733   0.4977   1.0000
   7.000   1.1650   0.02430   0.01583  -0.0718   0.4857   1.0000
   7.250   1.1884   0.02441   0.01594  -0.0708   0.4745   1.0000
   7.500   1.2178   0.02429   0.01574  -0.0706   0.4642   1.0000
   7.750   1.2355   0.02464   0.01617  -0.0689   0.4515   1.0000
   8.000   1.2546   0.02500   0.01659  -0.0674   0.4391   1.0000
   8.250   1.2758   0.02534   0.01694  -0.0662   0.4275   1.0000
   8.500   1.3002   0.02560   0.01717  -0.0655   0.4163   1.0000
   8.750   1.3221   0.02598   0.01755  -0.0645   0.4048   1.0000
   9.000   1.3376   0.02664   0.01832  -0.0626   0.3931   1.0000
   9.250   1.3570   0.02723   0.01894  -0.0613   0.3824   1.0000
   9.500   1.3830   0.02766   0.01931  -0.0610   0.3721   1.0000
   9.750   1.3959   0.02843   0.02023  -0.0589   0.3614   1.0000
  10.000   1.4122   0.02921   0.02109  -0.0573   0.3515   1.0000
  10.250   1.4371   0.02973   0.02156  -0.0569   0.3415   1.0000
  10.500   1.4474   0.03058   0.02258  -0.0544   0.3315   1.0000
  10.750   1.4610   0.03136   0.02345  -0.0525   0.3214   1.0000
  11.000   1.4797   0.03184   0.02388  -0.0513   0.3104   1.0000
  11.250   1.4905   0.03235   0.02443  -0.0489   0.2989   1.0000
  11.500   1.4906   0.03319   0.02543  -0.0451   0.2885   1.0000
  11.750   1.4948   0.03380   0.02605  -0.0419   0.2778   1.0000
  12.000   1.5038   0.03430   0.02647  -0.0394   0.2669   1.0000
  12.250   1.4932   0.03545   0.02783  -0.0348   0.2584   1.0000
  12.500   1.4928   0.03640   0.02881  -0.0317   0.2488   1.0000
  12.750   1.4923   0.03743   0.02987  -0.0290   0.2392   1.0000
  13.000   1.4836   0.03912   0.03175  -0.0260   0.2310   1.0000
  13.250   1.4843   0.04040   0.03302  -0.0240   0.2219   1.0000
  13.500   1.4737   0.04257   0.03542  -0.0218   0.2137   1.0000
  13.750   1.4682   0.04458   0.03751  -0.0201   0.2052   1.0000
  14.000   1.4597   0.04697   0.04001  -0.0188   0.1963   1.0000
  14.250   1.4477   0.04997   0.04319  -0.0178   0.1873   1.0000
  14.500   1.4365   0.05304   0.04633  -0.0172   0.1776   1.0000
  14.750   1.4216   0.05675   0.05014  -0.0170   0.1672   1.0000
  15.000   1.4028   0.06133   0.05486  -0.0174   0.1553   1.0000
  15.250   1.3832   0.06637   0.05997  -0.0182   0.1423   1.0000
  15.500   1.3620   0.07198   0.06558  -0.0194   0.1287   1.0000
  15.750   1.3384   0.07824   0.07178  -0.0210   0.1149   1.0000
  16.000   1.3157   0.08473   0.07818  -0.0228   0.1023   1.0000
  16.250   1.2951   0.09117   0.08455  -0.0247   0.0912   1.0000
  16.500   1.2800   0.09694   0.09030  -0.0264   0.0824   1.0000
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