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SPICA 11.73% smoothed (spicasm-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: SPICA 11.73% smoothed (spicasm-il)
Reynolds number: 500,000
Max Cl/Cd: 104.23 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-spicasm-il-500000-n5.txt
Download as CSV file: xf-spicasm-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.2953   0.11432   0.11192  -0.0356   1.0000   0.0194
 -10.750  -0.2943   0.11080   0.10843  -0.0369   1.0000   0.0195
 -10.250  -0.2898   0.10250   0.10016  -0.0414   0.9905   0.0196
 -10.000  -0.2787   0.09807   0.09572  -0.0452   0.9742   0.0196
  -9.750  -0.2547   0.09299   0.09060  -0.0521   0.9505   0.0195
  -9.500  -0.2131   0.08759   0.08512  -0.0623   0.9301   0.0194
  -9.250  -0.1647   0.08115   0.07851  -0.0761   0.8952   0.0192
  -9.000  -0.1578   0.07416   0.07125  -0.0846   0.8419   0.0196
  -8.750  -0.1334   0.07583   0.07277  -0.0824   0.8095   0.0209
  -8.250  -0.1448   0.06832   0.06510  -0.0850   0.7669   0.0203
  -8.000  -0.1384   0.06702   0.06375  -0.0848   0.7497   0.0211
  -7.750  -0.1461   0.06419   0.06087  -0.0855   0.7343   0.0213
  -7.500  -0.1484   0.06057   0.05718  -0.0879   0.7213   0.0214
  -7.250  -0.1529   0.05514   0.05166  -0.0913   0.7103   0.0207
  -7.000  -0.1544   0.04929   0.04564  -0.0940   0.7012   0.0204
  -6.750  -0.1510   0.04386   0.04000  -0.0954   0.6923   0.0203
  -6.500  -0.1409   0.04015   0.03610  -0.0956   0.6839   0.0204
  -6.250  -0.1276   0.03709   0.03285  -0.0955   0.6752   0.0206
  -6.000  -0.1124   0.03432   0.02987  -0.0951   0.6676   0.0210
  -5.750  -0.0989   0.03051   0.02576  -0.0943   0.6602   0.0212
  -5.500  -0.0854   0.02642   0.02125  -0.0930   0.6537   0.0213
  -5.250  -0.0697   0.02272   0.01713  -0.0915   0.6472   0.0216
  -5.000  -0.0525   0.01945   0.01335  -0.0900   0.6412   0.0218
  -4.750  -0.0310   0.01757   0.01111  -0.0889   0.6355   0.0221
  -4.500  -0.0071   0.01642   0.00970  -0.0882   0.6295   0.0226
  -4.250   0.0173   0.01549   0.00853  -0.0875   0.6239   0.0229
  -4.000   0.0427   0.01471   0.00757  -0.0870   0.6189   0.0231
  -3.750   0.0684   0.01408   0.00679  -0.0865   0.6136   0.0233
  -3.500   0.0941   0.01359   0.00616  -0.0860   0.6086   0.0235
  -3.250   0.1201   0.01311   0.00559  -0.0856   0.6041   0.0236
  -3.000   0.1457   0.01252   0.00494  -0.0851   0.5995   0.0240
  -2.750   0.1716   0.01215   0.00452  -0.0846   0.5949   0.0244
  -2.250   0.2239   0.01159   0.00390  -0.0838   0.5861   0.0251
  -2.000   0.2501   0.01135   0.00363  -0.0834   0.5816   0.0255
  -1.750   0.2763   0.01114   0.00338  -0.0830   0.5771   0.0260
  -1.500   0.3025   0.01097   0.00318  -0.0826   0.5729   0.0266
  -1.250   0.3292   0.01081   0.00300  -0.0823   0.5684   0.0274
  -1.000   0.3557   0.01067   0.00283  -0.0819   0.5635   0.0280
  -0.750   0.3818   0.01053   0.00265  -0.0814   0.5589   0.0286
  -0.500   0.4083   0.01037   0.00250  -0.0811   0.5545   0.0296
  -0.250   0.4350   0.01027   0.00240  -0.0808   0.5494   0.0308
   0.000   0.4616   0.01021   0.00231  -0.0804   0.5444   0.0321
   0.250   0.4883   0.01015   0.00223  -0.0801   0.5394   0.0340
   0.500   0.5150   0.01008   0.00219  -0.0798   0.5332   0.0383
   0.750   0.5410   0.01005   0.00218  -0.0794   0.5265   0.0506
   1.000   0.5678   0.01000   0.00216  -0.0791   0.5196   0.0649
   1.250   0.5940   0.00995   0.00214  -0.0787   0.5130   0.0828
   1.500   0.6100   0.00874   0.00224  -0.0770   0.5077   0.5683
   2.000   0.7333   0.00804   0.00247  -0.0914   0.4914   1.0000
   2.250   0.7571   0.00812   0.00250  -0.0906   0.4837   1.0000
   2.500   0.7807   0.00822   0.00255  -0.0897   0.4768   1.0000
   2.750   0.8046   0.00831   0.00260  -0.0888   0.4688   1.0000
   3.000   0.8281   0.00843   0.00266  -0.0879   0.4606   1.0000
   3.250   0.8516   0.00855   0.00274  -0.0870   0.4513   1.0000
   3.500   0.8752   0.00868   0.00282  -0.0862   0.4427   1.0000
   3.750   0.8983   0.00883   0.00292  -0.0852   0.4336   1.0000
   4.000   0.9218   0.00898   0.00303  -0.0844   0.4238   1.0000
   4.250   0.9447   0.00915   0.00315  -0.0834   0.4138   1.0000
   4.500   0.9675   0.00934   0.00329  -0.0824   0.4034   1.0000
   4.750   0.9907   0.00951   0.00343  -0.0815   0.3936   1.0000
   5.000   1.0131   0.00972   0.00360  -0.0805   0.3824   1.0000
   5.250   1.0351   0.00995   0.00377  -0.0794   0.3709   1.0000
   5.500   1.0577   0.01017   0.00395  -0.0785   0.3592   1.0000
   5.750   1.0796   0.01041   0.00415  -0.0774   0.3469   1.0000
   6.000   1.1012   0.01067   0.00437  -0.0763   0.3348   1.0000
   6.250   1.1225   0.01095   0.00460  -0.0752   0.3231   1.0000
   6.500   1.1436   0.01124   0.00486  -0.0740   0.3112   1.0000
   6.750   1.1647   0.01153   0.00511  -0.0729   0.2997   1.0000
   7.000   1.1856   0.01182   0.00538  -0.0717   0.2900   1.0000
   7.500   1.2263   0.01245   0.00597  -0.0692   0.2703   1.0000
   7.750   1.2459   0.01278   0.00628  -0.0679   0.2616   1.0000
   8.000   1.2649   0.01314   0.00662  -0.0665   0.2516   1.0000
   8.250   1.2834   0.01350   0.00697  -0.0650   0.2412   1.0000
   8.500   1.3001   0.01393   0.00735  -0.0632   0.2296   1.0000
   8.750   1.3150   0.01438   0.00776  -0.0611   0.2184   1.0000
   9.000   1.3302   0.01476   0.00813  -0.0590   0.2097   1.0000
   9.250   1.3441   0.01518   0.00855  -0.0568   0.2021   1.0000
   9.500   1.3571   0.01566   0.00902  -0.0545   0.1920   1.0000
   9.750   1.3714   0.01612   0.00948  -0.0524   0.1840   1.0000
  10.000   1.3836   0.01668   0.01003  -0.0502   0.1755   1.0000
  10.250   1.3970   0.01721   0.01057  -0.0482   0.1667   1.0000
  10.500   1.4073   0.01791   0.01125  -0.0459   0.1552   1.0000
  10.750   1.4166   0.01871   0.01201  -0.0436   0.1440   1.0000
  11.000   1.4230   0.01971   0.01296  -0.0412   0.1295   1.0000
  11.250   1.4277   0.02088   0.01408  -0.0388   0.1148   1.0000
  11.500   1.4298   0.02231   0.01544  -0.0364   0.0992   1.0000
  11.750   1.4300   0.02400   0.01706  -0.0341   0.0833   1.0000
  12.000   1.4300   0.02585   0.01885  -0.0322   0.0691   1.0000
  12.250   1.4262   0.02812   0.02106  -0.0303   0.0536   1.0000
  12.500   1.4196   0.03079   0.02364  -0.0286   0.0365   1.0000
  12.750   1.4132   0.03359   0.02640  -0.0272   0.0249   1.0000
  13.000   1.4128   0.03597   0.02882  -0.0263   0.0203   1.0000
  13.250   1.4136   0.03829   0.03119  -0.0255   0.0177   1.0000
  13.500   1.4159   0.04053   0.03350  -0.0249   0.0163   1.0000
  13.750   1.4167   0.04297   0.03601  -0.0244   0.0152   1.0000
  14.000   1.4178   0.04542   0.03854  -0.0240   0.0145   1.0000
  14.250   1.4197   0.04786   0.04106  -0.0237   0.0139   1.0000
  14.500   1.4204   0.05048   0.04378  -0.0235   0.0134   1.0000
  14.750   1.4204   0.05324   0.04662  -0.0234   0.0130   1.0000
  15.000   1.4187   0.05626   0.04972  -0.0234   0.0126   1.0000
  15.250   1.4156   0.05953   0.05309  -0.0235   0.0121   1.0000
  15.500   1.4109   0.06310   0.05675  -0.0238   0.0118   1.0000
  15.750   1.4079   0.06649   0.06024  -0.0241   0.0116   1.0000
  16.000   1.4052   0.06995   0.06381  -0.0246   0.0112   1.0000
  16.250   1.4013   0.07365   0.06760  -0.0252   0.0111   1.0000
  16.500   1.3965   0.07753   0.07159  -0.0259   0.0108   1.0000
  16.750   1.3919   0.08146   0.07561  -0.0268   0.0106   1.0000
  17.000   1.3854   0.08574   0.08000  -0.0278   0.0104   1.0000
  17.250   1.3786   0.09017   0.08454  -0.0290   0.0102   1.0000
  17.500   1.3717   0.09466   0.08913  -0.0303   0.0100   1.0000
  17.750   1.3635   0.09942   0.09399  -0.0317   0.0099   1.0000
  18.000   1.3540   0.10449   0.09917  -0.0334   0.0097   1.0000
  18.250   1.3442   0.10971   0.10449  -0.0353   0.0095   1.0000
  18.500   1.3342   0.11504   0.10992  -0.0373   0.0094   1.0000
  18.750   1.3235   0.12054   0.11552  -0.0395   0.0093   1.0000
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