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SPICA 11.73% smoothed (spicasm-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: SPICA 11.73% smoothed (spicasm-il)
Reynolds number: 500,000
Max Cl/Cd: 112.06 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-spicasm-il-500000.txt
Download as CSV file: xf-spicasm-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.500  -0.2711   0.09958   0.09735  -0.0371   1.0000   0.0247
  -9.250  -0.2691   0.09704   0.09484  -0.0372   1.0000   0.0252
  -9.000  -0.2687   0.09448   0.09232  -0.0373   1.0000   0.0257
  -8.750  -0.2552   0.09034   0.08819  -0.0418   0.9972   0.0267
  -8.500  -0.2490   0.08311   0.08096  -0.0549   0.9768   0.0278
  -8.250  -0.2323   0.07653   0.07438  -0.0643   0.9575   0.0280
  -8.000  -0.1996   0.07266   0.07046  -0.0688   0.9435   0.0284
  -7.750  -0.1551   0.06794   0.06565  -0.0792   0.9195   0.0289
  -7.500  -0.1232   0.06352   0.06102  -0.0884   0.8751   0.0296
  -7.250  -0.1167   0.06043   0.05771  -0.0911   0.8357   0.0303
  -7.000  -0.1135   0.05725   0.05437  -0.0929   0.8093   0.0311
  -6.750  -0.1160   0.04994   0.04660  -0.0987   0.7875   0.0331
  -6.500  -0.1124   0.04570   0.04223  -0.0984   0.7719   0.0335
  -6.250  -0.0997   0.04380   0.04026  -0.0978   0.7575   0.0338
  -6.000  -0.0853   0.04206   0.03842  -0.0973   0.7447   0.0342
  -5.750  -0.0700   0.04023   0.03645  -0.0969   0.7332   0.0347
  -5.500  -0.0537   0.03818   0.03427  -0.0966   0.7224   0.0355
  -5.250  -0.0335   0.03553   0.03105  -0.0957   0.7134   0.0392
  -5.000  -0.0223   0.03127   0.02656  -0.0950   0.7051   0.0399
  -4.750  -0.0024   0.02975   0.02501  -0.0947   0.6969   0.0405
  -4.500   0.0185   0.02853   0.02371  -0.0942   0.6891   0.0413
  -4.250   0.0400   0.02722   0.02227  -0.0936   0.6823   0.0426
  -4.000   0.0666   0.02740   0.02192  -0.0920   0.6752   0.0466
  -3.750   0.0827   0.02340   0.01774  -0.0913   0.6695   0.0480
  -3.500   0.1060   0.02216   0.01647  -0.0909   0.6633   0.0489
  -3.250   0.1299   0.02116   0.01536  -0.0904   0.6574   0.0504
  -3.000   0.1525   0.01720   0.01053  -0.0879   0.6528   0.0403
  -2.750   0.1784   0.01599   0.00924  -0.0873   0.6472   0.0379
  -2.500   0.2041   0.01479   0.00785  -0.0867   0.6419   0.0371
  -2.250   0.2301   0.01365   0.00649  -0.0860   0.6371   0.0362
  -2.000   0.2565   0.01289   0.00564  -0.0855   0.6319   0.0362
  -1.750   0.2828   0.01234   0.00503  -0.0850   0.6267   0.0365
  -1.500   0.3090   0.01196   0.00455  -0.0845   0.6219   0.0371
  -1.250   0.3351   0.01158   0.00416  -0.0840   0.6168   0.0378
  -1.000   0.3612   0.01129   0.00383  -0.0835   0.6117   0.0386
  -0.750   0.3871   0.01104   0.00352  -0.0830   0.6068   0.0399
  -0.500   0.4129   0.01077   0.00328  -0.0825   0.6019   0.0419
  -0.250   0.4391   0.01060   0.00312  -0.0821   0.5966   0.0439
   0.000   0.4656   0.01050   0.00296  -0.0816   0.5916   0.0463
   0.250   0.4916   0.01032   0.00280  -0.0812   0.5864   0.0512
   0.500   0.5177   0.01014   0.00265  -0.0807   0.5805   0.0624
   0.750   0.5431   0.00993   0.00253  -0.0802   0.5748   0.1108
   1.000   0.5482   0.00804   0.00265  -0.0760   0.5700   0.7849
   1.250   0.6678   0.00786   0.00271  -0.0954   0.5609   1.0000
   1.500   0.6915   0.00795   0.00272  -0.0945   0.5558   1.0000
   1.750   0.7153   0.00799   0.00274  -0.0936   0.5500   1.0000
   2.000   0.7389   0.00807   0.00275  -0.0927   0.5443   1.0000
   2.250   0.7629   0.00815   0.00279  -0.0918   0.5388   1.0000
   2.500   0.7869   0.00821   0.00283  -0.0910   0.5325   1.0000
   2.750   0.8106   0.00832   0.00286  -0.0901   0.5265   1.0000
   3.000   0.8347   0.00837   0.00293  -0.0893   0.5199   1.0000
   3.250   0.8586   0.00847   0.00298  -0.0885   0.5134   1.0000
   3.500   0.8826   0.00856   0.00305  -0.0877   0.5066   1.0000
   3.750   0.9064   0.00865   0.00312  -0.0868   0.4988   1.0000
   4.000   0.9302   0.00875   0.00320  -0.0860   0.4913   1.0000
   4.250   0.9540   0.00886   0.00329  -0.0851   0.4833   1.0000
   4.500   0.9776   0.00897   0.00339  -0.0843   0.4749   1.0000
   4.750   1.0008   0.00911   0.00349  -0.0833   0.4657   1.0000
   5.000   1.0244   0.00924   0.00361  -0.0825   0.4560   1.0000
   5.250   1.0472   0.00940   0.00374  -0.0815   0.4464   1.0000
   5.500   1.0698   0.00958   0.00389  -0.0805   0.4354   1.0000
   5.750   1.0926   0.00975   0.00405  -0.0796   0.4241   1.0000
   6.000   1.1148   0.00996   0.00423  -0.0785   0.4127   1.0000
   6.250   1.1365   0.01020   0.00443  -0.0774   0.4007   1.0000
   6.750   1.1793   0.01071   0.00487  -0.0751   0.3751   1.0000
   7.000   1.2005   0.01098   0.00511  -0.0740   0.3616   1.0000
   7.250   1.2212   0.01127   0.00538  -0.0727   0.3484   1.0000
   7.500   1.2413   0.01159   0.00567  -0.0714   0.3356   1.0000
   7.750   1.2607   0.01194   0.00598  -0.0700   0.3223   1.0000
   8.000   1.2792   0.01232   0.00631  -0.0685   0.3083   1.0000
   8.250   1.2971   0.01273   0.00667  -0.0669   0.2949   1.0000
   8.500   1.3141   0.01315   0.00705  -0.0651   0.2807   1.0000
   9.000   1.3484   0.01395   0.00780  -0.0617   0.2578   1.0000
   9.250   1.3632   0.01436   0.00821  -0.0596   0.2492   1.0000
   9.500   1.3763   0.01480   0.00864  -0.0571   0.2399   1.0000
   9.750   1.3909   0.01520   0.00906  -0.0550   0.2313   1.0000
  10.000   1.4024   0.01574   0.00956  -0.0525   0.2220   1.0000
  10.250   1.4163   0.01621   0.01006  -0.0505   0.2126   1.0000
  10.500   1.4294   0.01674   0.01060  -0.0484   0.2051   1.0000
  10.750   1.4401   0.01740   0.01124  -0.0461   0.1953   1.0000
  11.000   1.4532   0.01798   0.01185  -0.0442   0.1861   1.0000
  11.250   1.4627   0.01876   0.01262  -0.0420   0.1744   1.0000
  11.500   1.4709   0.01966   0.01350  -0.0398   0.1624   1.0000
  11.750   1.4772   0.02074   0.01454  -0.0376   0.1482   1.0000
  12.000   1.4804   0.02211   0.01584  -0.0354   0.1315   1.0000
  12.250   1.4792   0.02388   0.01752  -0.0330   0.1133   1.0000
  12.500   1.4731   0.02619   0.01969  -0.0307   0.0905   1.0000
  12.750   1.4625   0.02905   0.02242  -0.0285   0.0670   1.0000
  13.250   1.4343   0.03603   0.02919  -0.0252   0.0301   1.0000
  13.500   1.4301   0.03885   0.03204  -0.0243   0.0260   1.0000
  13.750   1.4264   0.04170   0.03496  -0.0236   0.0237   1.0000
  14.000   1.4264   0.04427   0.03762  -0.0231   0.0225   1.0000
  14.250   1.4235   0.04719   0.04061  -0.0227   0.0214   1.0000
  14.500   1.4186   0.05044   0.04395  -0.0225   0.0206   1.0000
  14.750   1.4108   0.05411   0.04771  -0.0224   0.0198   1.0000
  15.000   1.4094   0.05715   0.05086  -0.0224   0.0191   1.0000
  15.250   1.4059   0.06051   0.05433  -0.0226   0.0187   1.0000
  15.500   1.4012   0.06411   0.05803  -0.0229   0.0183   1.0000
  15.750   1.3947   0.06801   0.06203  -0.0234   0.0178   1.0000
  16.000   1.3878   0.07207   0.06619  -0.0240   0.0175   1.0000
  16.250   1.3792   0.07649   0.07071  -0.0249   0.0172   1.0000
  16.500   1.3697   0.08111   0.07542  -0.0259   0.0169   1.0000
  16.750   1.3571   0.08628   0.08070  -0.0271   0.0166   1.0000
  17.000   1.3452   0.09145   0.08596  -0.0285   0.0164   1.0000
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