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SPICA 11.73% smoothed (spicasm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: SPICA 11.73% smoothed (spicasm-il)
Reynolds number: 1,000,000
Max Cl/Cd: 136.73 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-spicasm-il-1000000.txt
Download as CSV file: xf-spicasm-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.3240   0.13326   0.13151  -0.0287   1.0000   0.0159
 -12.250  -0.3250   0.12914   0.12740  -0.0309   1.0000   0.0160
 -12.000  -0.3227   0.12555   0.12382  -0.0323   1.0000   0.0160
 -11.750  -0.3173   0.12182   0.12010  -0.0323   1.0000   0.0162
 -11.500  -0.3113   0.11904   0.11733  -0.0327   1.0000   0.0163
 -11.250  -0.3035   0.11692   0.11522  -0.0326   1.0000   0.0165
 -11.000  -0.2983   0.11427   0.11259  -0.0332   1.0000   0.0166
 -10.750  -0.2931   0.11176   0.11009  -0.0336   1.0000   0.0168
 -10.500  -0.2885   0.10916   0.10750  -0.0341   1.0000   0.0171
 -10.250  -0.1817   0.09217   0.09062  -0.0500   0.9731   0.0193
 -10.000  -0.1669   0.08581   0.08423  -0.0565   0.9605   0.0194
  -9.750  -0.1419   0.07873   0.07709  -0.0643   0.9456   0.0197
  -9.500  -0.1029   0.07299   0.07123  -0.0736   0.9148   0.0199
  -9.250  -0.0895   0.06990   0.06784  -0.0761   0.8514   0.0202
  -9.000  -0.0879   0.06740   0.06520  -0.0759   0.8167   0.0204
  -8.750  -0.0858   0.06473   0.06243  -0.0761   0.7933   0.0206
  -8.500  -0.0847   0.06185   0.05947  -0.0766   0.7732   0.0209
  -8.250  -0.0846   0.05880   0.05637  -0.0772   0.7564   0.0213
  -8.000  -0.0858   0.05562   0.05314  -0.0779   0.7414   0.0217
  -7.750  -0.1284   0.06355   0.06109  -0.0889   0.7744   0.0212
  -7.500  -0.1322   0.06054   0.05800  -0.0903   0.7540   0.0215
  -7.250  -0.1319   0.05686   0.05424  -0.0925   0.7377   0.0221
  -7.000  -0.1345   0.04871   0.04586  -0.0977   0.7245   0.0233
  -6.750  -0.1414   0.04197   0.03890  -0.0984   0.7136   0.0237
  -6.500  -0.1294   0.03981   0.03661  -0.0979   0.7016   0.0238
  -6.250  -0.1142   0.03810   0.03481  -0.0976   0.6910   0.0240
  -6.000  -0.0978   0.03640   0.03300  -0.0972   0.6814   0.0243
  -5.750  -0.0810   0.03450   0.03097  -0.0967   0.6724   0.0247
  -5.500  -0.0632   0.03245   0.02877  -0.0962   0.6645   0.0252
  -5.250  -0.0451   0.03008   0.02622  -0.0955   0.6570   0.0262
  -5.000  -0.0361   0.02368   0.01914  -0.0930   0.6515   0.0284
  -4.750  -0.0140   0.02258   0.01797  -0.0925   0.6446   0.0287
  -4.500   0.0085   0.02172   0.01700  -0.0919   0.6381   0.0290
  -4.250   0.0323   0.02096   0.01618  -0.0915   0.6326   0.0296
  -4.000   0.0475   0.01590   0.01031  -0.0886   0.6279   0.0285
  -3.750   0.0726   0.01544   0.00982  -0.0882   0.6223   0.0291
  -3.500   0.0956   0.01281   0.00681  -0.0869   0.6179   0.0257
  -3.250   0.1213   0.01191   0.00576  -0.0863   0.6130   0.0255
  -3.000   0.1470   0.01131   0.00505  -0.0858   0.6081   0.0256
  -2.750   0.1734   0.01092   0.00459  -0.0854   0.6035   0.0260
  -2.500   0.2000   0.01053   0.00416  -0.0850   0.5990   0.0265
  -2.250   0.2262   0.01017   0.00374  -0.0845   0.5944   0.0269
  -2.000   0.2522   0.00992   0.00342  -0.0840   0.5895   0.0273
  -1.750   0.2791   0.00965   0.00314  -0.0837   0.5855   0.0276
  -1.500   0.3059   0.00948   0.00294  -0.0833   0.5808   0.0279
  -1.250   0.3308   0.00908   0.00249  -0.0827   0.5762   0.0286
  -1.000   0.3571   0.00889   0.00227  -0.0823   0.5719   0.0293
  -0.750   0.3841   0.00873   0.00212  -0.0820   0.5675   0.0301
  -0.500   0.4109   0.00863   0.00200  -0.0817   0.5626   0.0311
  -0.250   0.4375   0.00858   0.00190  -0.0813   0.5572   0.0324
   0.000   0.4648   0.00845   0.00178  -0.0811   0.5518   0.0341
   0.250   0.4915   0.00837   0.00170  -0.0807   0.5461   0.0371
   0.500   0.5182   0.00833   0.00165  -0.0804   0.5411   0.0425
   0.750   0.5455   0.00821   0.00162  -0.0802   0.5367   0.0630
   1.000   0.5723   0.00815   0.00160  -0.0799   0.5314   0.0828
   1.250   0.5951   0.00769   0.00163  -0.0791   0.5261   0.2971
   1.500   0.6054   0.00639   0.00173  -0.0758   0.5221   0.7920
   1.750   0.6964   0.00623   0.00193  -0.0893   0.5139   0.9931
   2.000   0.7536   0.00630   0.00193  -0.0958   0.5067   1.0000
   2.250   0.7775   0.00635   0.00195  -0.0949   0.5005   1.0000
   2.500   0.8010   0.00644   0.00198  -0.0940   0.4942   1.0000
   2.750   0.8254   0.00649   0.00201  -0.0932   0.4872   1.0000
   3.000   0.8487   0.00659   0.00206  -0.0923   0.4794   1.0000
   3.250   0.8731   0.00666   0.00211  -0.0915   0.4721   1.0000
   3.500   0.8965   0.00678   0.00217  -0.0906   0.4638   1.0000
   3.750   0.9207   0.00687   0.00224  -0.0899   0.4549   1.0000
   4.000   0.9442   0.00699   0.00232  -0.0890   0.4458   1.0000
   4.250   0.9676   0.00713   0.00241  -0.0881   0.4358   1.0000
   4.500   0.9914   0.00726   0.00252  -0.0873   0.4260   1.0000
   4.750   1.0145   0.00742   0.00263  -0.0863   0.4156   1.0000
   5.000   1.0375   0.00760   0.00276  -0.0854   0.4044   1.0000
   5.250   1.0609   0.00776   0.00288  -0.0845   0.3934   1.0000
   5.500   1.0839   0.00794   0.00303  -0.0836   0.3816   1.0000
   5.750   1.1065   0.00815   0.00319  -0.0826   0.3697   1.0000
   6.000   1.1288   0.00838   0.00336  -0.0816   0.3565   1.0000
   6.500   1.1734   0.00884   0.00374  -0.0796   0.3306   1.0000
   6.750   1.1952   0.00909   0.00394  -0.0786   0.3180   1.0000
   7.000   1.2165   0.00936   0.00416  -0.0774   0.3044   1.0000
   7.250   1.2371   0.00967   0.00441  -0.0762   0.2895   1.0000
   7.500   1.2575   0.00999   0.00467  -0.0749   0.2752   1.0000
   7.750   1.2774   0.01033   0.00494  -0.0736   0.2608   1.0000
   8.000   1.2974   0.01066   0.00523  -0.0723   0.2485   1.0000
   8.250   1.3172   0.01099   0.00552  -0.0710   0.2386   1.0000
   8.500   1.3381   0.01126   0.00577  -0.0698   0.2303   1.0000
   8.750   1.3572   0.01160   0.00608  -0.0684   0.2205   1.0000
   9.000   1.3755   0.01196   0.00641  -0.0669   0.2101   1.0000
   9.250   1.3951   0.01225   0.00670  -0.0655   0.2026   1.0000
   9.500   1.4119   0.01264   0.00706  -0.0638   0.1931   1.0000
   9.750   1.4279   0.01299   0.00739  -0.0618   0.1839   1.0000
  10.000   1.4420   0.01337   0.00775  -0.0595   0.1749   1.0000
  10.250   1.4535   0.01386   0.00819  -0.0568   0.1623   1.0000
  10.500   1.4638   0.01443   0.00870  -0.0541   0.1480   1.0000
  10.750   1.4724   0.01512   0.00931  -0.0512   0.1325   1.0000
  11.000   1.4782   0.01598   0.01006  -0.0481   0.1158   1.0000
  11.250   1.4813   0.01702   0.01101  -0.0449   0.0968   1.0000
  11.500   1.4774   0.01855   0.01239  -0.0411   0.0728   1.0000
  11.750   1.4720   0.02036   0.01407  -0.0376   0.0514   1.0000
  12.000   1.4600   0.02289   0.01644  -0.0343   0.0274   1.0000
  12.250   1.4604   0.02478   0.01832  -0.0324   0.0204   1.0000
  12.500   1.4666   0.02635   0.01993  -0.0312   0.0182   1.0000
  12.750   1.4720   0.02805   0.02167  -0.0301   0.0168   1.0000
  13.000   1.4782   0.02974   0.02344  -0.0292   0.0157   1.0000
  13.250   1.4845   0.03148   0.02524  -0.0284   0.0151   1.0000
  13.500   1.4889   0.03343   0.02725  -0.0276   0.0144   1.0000
  13.750   1.4910   0.03565   0.02954  -0.0269   0.0137   1.0000
  14.000   1.4905   0.03817   0.03213  -0.0263   0.0132   1.0000
  14.250   1.4919   0.04054   0.03460  -0.0257   0.0129   1.0000
  14.500   1.4948   0.04283   0.03696  -0.0254   0.0127   1.0000
  14.750   1.4971   0.04521   0.03941  -0.0251   0.0123   1.0000
  15.000   1.4964   0.04795   0.04224  -0.0248   0.0120   1.0000
  15.250   1.4971   0.05060   0.04496  -0.0247   0.0117   1.0000
  15.500   1.4956   0.05356   0.04799  -0.0246   0.0114   1.0000
  15.750   1.4905   0.05699   0.05151  -0.0246   0.0112   1.0000
  16.000   1.4859   0.06044   0.05505  -0.0248   0.0110   1.0000
  16.250   1.4783   0.06435   0.05906  -0.0251   0.0109   1.0000
  16.500   1.4670   0.06879   0.06359  -0.0256   0.0106   1.0000
  16.750   1.4523   0.07382   0.06874  -0.0263   0.0104   1.0000
  17.000   1.4465   0.07774   0.07275  -0.0269   0.0103   1.0000
  17.250   1.4414   0.08160   0.07670  -0.0276   0.0102   1.0000
  17.500   1.4332   0.08596   0.08116  -0.0285   0.0102   1.0000
  17.750   1.4265   0.09020   0.08549  -0.0294   0.0100   1.0000
  18.000   1.4189   0.09461   0.08999  -0.0305   0.0099   1.0000
  18.250   1.4086   0.09945   0.09493  -0.0318   0.0099   1.0000
  18.500   1.3985   0.10437   0.09994  -0.0332   0.0097   1.0000
  18.750   1.3923   0.10875   0.10440  -0.0345   0.0095   1.0000
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