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SPICA 11.73% smoothed (spicasm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: SPICA 11.73% smoothed (spicasm-il)
Reynolds number: 1,000,000
Max Cl/Cd: 123.17 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-spicasm-il-1000000-n5.txt
Download as CSV file: xf-spicasm-il-1000000-n5.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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.1677   0.08464   0.08201  -0.0800   0.7872   0.0138
  -9.750  -0.1655   0.08179   0.07907  -0.0808   0.7654   0.0138
  -9.500  -0.1627   0.07906   0.07628  -0.0817   0.7474   0.0139
  -9.250  -0.1608   0.07621   0.07338  -0.0826   0.7318   0.0141
  -9.000  -0.1601   0.07323   0.07036  -0.0836   0.7175   0.0142
  -8.750  -0.1603   0.07024   0.06733  -0.0846   0.7049   0.0146
  -8.500  -0.1657   0.06667   0.06375  -0.0859   0.6927   0.0148
  -8.250  -0.1784   0.06307   0.06015  -0.0871   0.6827   0.0149
  -8.000  -0.1957   0.05730   0.05433  -0.0909   0.6731   0.0155
  -7.750  -0.2115   0.04920   0.04611  -0.0952   0.6663   0.0158
  -7.500  -0.2487   0.03402   0.03042  -0.0974   0.6618   0.0164
  -7.250  -0.2354   0.03135   0.02757  -0.0968   0.6539   0.0166
  -7.000  -0.2193   0.02910   0.02514  -0.0961   0.6460   0.0168
  -6.750  -0.2292   0.01944   0.01459  -0.0928   0.6406   0.0175
  -6.500  -0.2099   0.01765   0.01249  -0.0918   0.6336   0.0178
  -6.250  -0.1885   0.01631   0.01089  -0.0909   0.6265   0.0180
  -6.000  -0.1656   0.01528   0.00965  -0.0901   0.6203   0.0181
  -5.750  -0.1415   0.01444   0.00864  -0.0895   0.6144   0.0183
  -5.500  -0.1169   0.01376   0.00781  -0.0889   0.6087   0.0185
  -5.250  -0.0917   0.01318   0.00710  -0.0884   0.6037   0.0186
  -5.000  -0.0660   0.01267   0.00648  -0.0879   0.5990   0.0188
  -4.750  -0.0400   0.01230   0.00602  -0.0875   0.5941   0.0190
  -4.500  -0.0140   0.01194   0.00557  -0.0871   0.5895   0.0192
  -4.250   0.0124   0.01158   0.00514  -0.0867   0.5854   0.0194
  -4.000   0.0388   0.01127   0.00476  -0.0863   0.5813   0.0195
  -3.750   0.0652   0.01098   0.00441  -0.0859   0.5772   0.0196
  -3.500   0.0905   0.01050   0.00386  -0.0854   0.5732   0.0199
  -3.250   0.1168   0.01017   0.00350  -0.0850   0.5694   0.0202
  -3.000   0.1433   0.00994   0.00324  -0.0847   0.5654   0.0205
  -2.750   0.1698   0.00976   0.00303  -0.0843   0.5611   0.0207
  -2.500   0.1964   0.00959   0.00283  -0.0840   0.5573   0.0210
  -2.250   0.2234   0.00942   0.00265  -0.0837   0.5536   0.0212
  -2.000   0.2503   0.00927   0.00248  -0.0834   0.5491   0.0216
  -1.750   0.2770   0.00914   0.00232  -0.0831   0.5446   0.0218
  -1.500   0.3038   0.00903   0.00218  -0.0828   0.5405   0.0222
  -1.250   0.3310   0.00891   0.00206  -0.0825   0.5361   0.0225
  -1.000   0.3580   0.00882   0.00194  -0.0822   0.5312   0.0229
  -0.750   0.3848   0.00876   0.00185  -0.0819   0.5263   0.0233
  -0.500   0.4120   0.00867   0.00176  -0.0817   0.5214   0.0239
  -0.250   0.4388   0.00859   0.00166  -0.0814   0.5145   0.0249
   0.000   0.4656   0.00855   0.00160  -0.0811   0.5074   0.0256
   0.250   0.4927   0.00852   0.00155  -0.0809   0.4997   0.0266
   0.500   0.5195   0.00851   0.00152  -0.0806   0.4934   0.0277
   0.750   0.5467   0.00848   0.00149  -0.0804   0.4869   0.0295
   1.000   0.5734   0.00847   0.00148  -0.0801   0.4803   0.0348
   1.250   0.6002   0.00844   0.00150  -0.0799   0.4737   0.0531
   1.500   0.6268   0.00846   0.00152  -0.0796   0.4653   0.0633
   2.000   0.6689   0.00730   0.00167  -0.0774   0.4505   0.6035
   2.250   0.6817   0.00661   0.00179  -0.0740   0.4432   0.8863
   2.500   0.7604   0.00674   0.00196  -0.0852   0.4287   0.9852
   2.750   0.8031   0.00690   0.00204  -0.0886   0.4186   0.9964
   3.000   0.8431   0.00703   0.00211  -0.0913   0.4083   1.0000
   3.250   0.8662   0.00717   0.00219  -0.0904   0.3984   1.0000
   3.500   0.8893   0.00731   0.00228  -0.0894   0.3884   1.0000
   3.750   0.9129   0.00744   0.00237  -0.0885   0.3796   1.0000
   4.000   0.9358   0.00761   0.00249  -0.0876   0.3690   1.0000
   4.250   0.9586   0.00780   0.00261  -0.0866   0.3566   1.0000
   4.500   0.9817   0.00797   0.00273  -0.0856   0.3451   1.0000
   4.750   1.0045   0.00816   0.00287  -0.0847   0.3339   1.0000
   5.000   1.0269   0.00838   0.00302  -0.0837   0.3219   1.0000
   5.250   1.0492   0.00861   0.00319  -0.0826   0.3095   1.0000
   5.500   1.0719   0.00881   0.00336  -0.0817   0.2986   1.0000
   5.750   1.0942   0.00904   0.00354  -0.0807   0.2873   1.0000
   6.000   1.1163   0.00928   0.00373  -0.0796   0.2773   1.0000
   6.250   1.1387   0.00950   0.00392  -0.0787   0.2678   1.0000
   6.500   1.1608   0.00973   0.00412  -0.0777   0.2588   1.0000
   7.000   1.2045   0.01022   0.00454  -0.0756   0.2415   1.0000
   7.250   1.2255   0.01050   0.00479  -0.0744   0.2320   1.0000
   7.500   1.2459   0.01082   0.00505  -0.0732   0.2211   1.0000
   7.750   1.2661   0.01112   0.00532  -0.0719   0.2098   1.0000
   8.000   1.2862   0.01143   0.00559  -0.0706   0.2004   1.0000
   8.250   1.3051   0.01179   0.00590  -0.0692   0.1900   1.0000
   8.500   1.3253   0.01207   0.00618  -0.0679   0.1819   1.0000
   8.750   1.3440   0.01241   0.00649  -0.0665   0.1742   1.0000
   9.000   1.3615   0.01279   0.00682  -0.0648   0.1640   1.0000
   9.250   1.3776   0.01317   0.00718  -0.0629   0.1539   1.0000
   9.500   1.3905   0.01359   0.00756  -0.0604   0.1438   1.0000
   9.750   1.4004   0.01414   0.00804  -0.0574   0.1297   1.0000
  10.000   1.4089   0.01479   0.00861  -0.0544   0.1144   1.0000
  10.250   1.4178   0.01547   0.00923  -0.0515   0.1012   1.0000
  10.500   1.4225   0.01639   0.01005  -0.0483   0.0843   1.0000
  10.750   1.4271   0.01738   0.01096  -0.0452   0.0688   1.0000
  11.000   1.4288   0.01862   0.01212  -0.0421   0.0528   1.0000
  11.250   1.4210   0.02058   0.01393  -0.0384   0.0283   1.0000
  11.500   1.4235   0.02210   0.01541  -0.0362   0.0189   1.0000
  11.750   1.4311   0.02338   0.01672  -0.0347   0.0156   1.0000
  12.000   1.4407   0.02458   0.01796  -0.0335   0.0141   1.0000
  12.250   1.4497   0.02590   0.01932  -0.0324   0.0130   1.0000
  12.500   1.4582   0.02731   0.02077  -0.0314   0.0121   1.0000
  12.750   1.4666   0.02878   0.02230  -0.0306   0.0115   1.0000
  13.000   1.4754   0.03027   0.02385  -0.0299   0.0111   1.0000
  13.250   1.4828   0.03190   0.02554  -0.0292   0.0106   1.0000
  13.500   1.4892   0.03367   0.02736  -0.0285   0.0102   1.0000
  13.750   1.4944   0.03559   0.02934  -0.0279   0.0098   1.0000
  14.000   1.4974   0.03775   0.03155  -0.0273   0.0093   1.0000
  14.250   1.5006   0.03993   0.03380  -0.0268   0.0091   1.0000
  14.500   1.5054   0.04198   0.03593  -0.0264   0.0088   1.0000
  14.750   1.5094   0.04415   0.03816  -0.0261   0.0086   1.0000
  15.000   1.5118   0.04652   0.04060  -0.0258   0.0084   1.0000
  15.250   1.5129   0.04907   0.04323  -0.0256   0.0082   1.0000
  15.500   1.5138   0.05172   0.04595  -0.0255   0.0079   1.0000
  15.750   1.5135   0.05451   0.04881  -0.0254   0.0078   1.0000
  16.000   1.5116   0.05756   0.05193  -0.0255   0.0075   1.0000
  16.250   1.5097   0.06067   0.05512  -0.0256   0.0074   1.0000
  16.500   1.5062   0.06402   0.05855  -0.0258   0.0073   1.0000
  16.750   1.5027   0.06740   0.06201  -0.0261   0.0072   1.0000
  17.000   1.4958   0.07130   0.06600  -0.0265   0.0070   1.0000
  17.250   1.4892   0.07524   0.07003  -0.0271   0.0069   1.0000
  17.500   1.4856   0.07883   0.07370  -0.0277   0.0068   1.0000
  17.750   1.4788   0.08288   0.07785  -0.0284   0.0068   1.0000
  18.000   1.4740   0.08672   0.08177  -0.0291   0.0066   1.0000
  18.250   1.4670   0.09094   0.08608  -0.0301   0.0065   1.0000
  18.500   1.4571   0.09565   0.09089  -0.0312   0.0065   1.0000
  18.750   1.4511   0.09981   0.09514  -0.0323   0.0063   1.0000
  19.000   1.4431   0.10435   0.09976  -0.0337   0.0062   1.0000
  19.250   1.4327   0.10935   0.10487  -0.0352   0.0062   1.0000
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