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SPICA 11.73% smoothed (spicasm-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: SPICA 11.73% smoothed (spicasm-il)
Reynolds number: 50,000
Max Cl/Cd: 30.89 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-spicasm-il-50000-n5.txt
Download as CSV file: xf-spicasm-il-50000-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 =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.250  -0.2671   0.11105   0.10422  -0.0373   1.0000   0.1169
  -9.000  -0.2818   0.11039   0.10371  -0.0387   1.0000   0.1196
  -8.750  -0.3017   0.11001   0.10354  -0.0397   1.0000   0.1204
  -8.500  -0.2910   0.10549   0.09911  -0.0382   1.0000   0.1219
  -8.250  -0.2769   0.10178   0.09543  -0.0360   1.0000   0.1249
  -8.000  -0.2796   0.09983   0.09361  -0.0343   1.0000   0.1277
  -7.750  -0.2927   0.09877   0.09272  -0.0318   1.0000   0.1300
  -7.500  -0.3058   0.09770   0.09180  -0.0312   0.9953   0.1329
  -7.250  -0.3006   0.09389   0.08801  -0.0447   0.9703   0.1380
  -7.000  -0.2716   0.08945   0.08354  -0.0426   0.9643   0.1426
  -6.500  -0.2343   0.08177   0.07583  -0.0523   0.9363   0.1602
  -6.250  -0.2200   0.07808   0.07208  -0.0592   0.9216   0.1729
  -6.000  -0.2031   0.07490   0.06881  -0.0650   0.9086   0.1880
  -5.750  -0.1747   0.07092   0.06483  -0.0649   0.9017   0.1942
  -5.500  -0.1430   0.06072   0.05370  -0.0810   0.8863   0.0884
  -5.000  -0.0956   0.05263   0.04494  -0.0860   0.8671   0.0751
  -4.750  -0.0757   0.04990   0.04204  -0.0865   0.8561   0.0736
  -4.500  -0.0527   0.04716   0.03900  -0.0875   0.8468   0.0730
  -4.250  -0.0283   0.04466   0.03613  -0.0884   0.8381   0.0734
  -4.000  -0.0063   0.04251   0.03363  -0.0884   0.8285   0.0734
  -3.750   0.0203   0.04029   0.03103  -0.0889   0.8208   0.0729
  -3.500   0.0423   0.03851   0.02891  -0.0884   0.8116   0.0722
  -3.250   0.0701   0.03666   0.02666  -0.0886   0.8044   0.0717
  -3.000   0.0936   0.03525   0.02490  -0.0880   0.7955   0.0716
  -2.750   0.1221   0.03379   0.02307  -0.0879   0.7885   0.0718
  -2.500   0.1475   0.03273   0.02169  -0.0874   0.7805   0.0732
  -2.250   0.1755   0.03180   0.02036  -0.0871   0.7730   0.0756
  -2.000   0.2032   0.03077   0.01915  -0.0869   0.7662   0.0777
  -1.750   0.2288   0.02998   0.01825  -0.0864   0.7582   0.0794
  -1.500   0.2624   0.02905   0.01715  -0.0869   0.7530   0.0816
  -1.250   0.2855   0.02869   0.01667  -0.0860   0.7440   0.0841
  -1.000   0.3177   0.02814   0.01588  -0.0861   0.7382   0.0896
  -0.750   0.3400   0.02779   0.01556  -0.0853   0.7302   0.0959
  -0.500   0.3671   0.02743   0.01504  -0.0848   0.7237   0.1034
  -0.250   0.3919   0.02709   0.01470  -0.0843   0.7169   0.1158
   0.000   0.4146   0.02687   0.01450  -0.0834   0.7093   0.1363
   0.250   0.4862   0.02363   0.01377  -0.0909   0.7050   1.0000
   0.500   0.5033   0.02415   0.01402  -0.0891   0.6963   1.0000
   0.750   0.5292   0.02437   0.01394  -0.0885   0.6899   1.0000
   1.000   0.5482   0.02486   0.01424  -0.0870   0.6817   1.0000
   1.250   0.5721   0.02515   0.01433  -0.0862   0.6746   1.0000
   1.500   0.5935   0.02556   0.01458  -0.0851   0.6671   1.0000
   1.750   0.6153   0.02594   0.01483  -0.0840   0.6593   1.0000
   2.000   0.6393   0.02626   0.01500  -0.0832   0.6523   1.0000
   2.250   0.6588   0.02675   0.01540  -0.0818   0.6437   1.0000
   2.500   0.6850   0.02697   0.01550  -0.0812   0.6371   1.0000
   2.750   0.7024   0.02755   0.01603  -0.0797   0.6278   1.0000
   3.000   0.7294   0.02772   0.01610  -0.0792   0.6211   1.0000
   3.250   0.7462   0.02832   0.01668  -0.0775   0.6114   1.0000
   3.500   0.7715   0.02855   0.01684  -0.0768   0.6040   1.0000
   3.750   0.7902   0.02906   0.01732  -0.0754   0.5946   1.0000
   4.000   0.8118   0.02944   0.01768  -0.0742   0.5860   1.0000
   4.500   0.8519   0.03031   0.01854  -0.0716   0.5676   1.0000
   4.750   0.8792   0.03037   0.01858  -0.0711   0.5599   1.0000
   5.000   0.8925   0.03114   0.01939  -0.0691   0.5492   1.0000
   5.250   0.9242   0.03095   0.01916  -0.0690   0.5423   1.0000
   5.500   0.9337   0.03190   0.02020  -0.0666   0.5308   1.0000
   5.750   0.9538   0.03231   0.02064  -0.0653   0.5217   1.0000
   6.000   0.9762   0.03255   0.02091  -0.0643   0.5125   1.0000
   6.250   0.9878   0.03338   0.02181  -0.0621   0.5016   1.0000
   6.500   1.0204   0.03307   0.02152  -0.0621   0.4946   1.0000
   6.750   1.0269   0.03414   0.02269  -0.0595   0.4826   1.0000
   7.000   1.0401   0.03486   0.02348  -0.0575   0.4721   1.0000
   7.250   1.0702   0.03464   0.02329  -0.0572   0.4642   1.0000
   7.500   1.0755   0.03580   0.02456  -0.0545   0.4526   1.0000
   7.750   1.0900   0.03644   0.02526  -0.0528   0.4426   1.0000
   8.000   1.1171   0.03636   0.02522  -0.0521   0.4340   1.0000
   8.250   1.1192   0.03770   0.02666  -0.0492   0.4231   1.0000
   8.500   1.1384   0.03808   0.02711  -0.0478   0.4139   1.0000
   8.750   1.1543   0.03864   0.02773  -0.0462   0.4044   1.0000
   9.000   1.1565   0.04008   0.02927  -0.0436   0.3944   1.0000
   9.250   1.1914   0.03961   0.02880  -0.0436   0.3864   1.0000
   9.500   1.1814   0.04186   0.03121  -0.0403   0.3759   1.0000
   9.750   1.1952   0.04274   0.03217  -0.0388   0.3672   1.0000
  10.000   1.2072   0.04377   0.03328  -0.0373   0.3585   1.0000
  10.250   1.2057   0.04584   0.03547  -0.0354   0.3494   1.0000
  10.500   1.2322   0.04583   0.03551  -0.0346   0.3417   1.0000
  10.750   1.2167   0.04923   0.03906  -0.0326   0.3327   1.0000
  11.000   1.2530   0.04837   0.03827  -0.0320   0.3256   1.0000
  11.250   1.2235   0.05325   0.04332  -0.0302   0.3166   1.0000
  11.500   1.2663   0.05169   0.04181  -0.0294   0.3101   1.0000
  11.750   1.2215   0.05855   0.04887  -0.0284   0.3013   1.0000
  12.000   1.2698   0.05609   0.04648  -0.0272   0.2950   1.0000
  12.250   1.2068   0.06575   0.05630  -0.0276   0.2858   1.0000
  12.500   1.2573   0.06253   0.05320  -0.0258   0.2803   1.0000
  12.750   1.1722   0.07640   0.06716  -0.0285   0.2698   1.0000
  13.000   1.2299   0.07144   0.06236  -0.0258   0.2656   1.0000
  13.250   1.1347   0.08865   0.07957  -0.0310   0.2533   1.0000
  13.500   1.1885   0.08338   0.07452  -0.0277   0.2504   1.0000
  14.000   1.1323   0.09923   0.09048  -0.0322   0.2335   1.0000
  14.250   1.0805   0.11252   0.10374  -0.0376   0.2219   1.0000
  14.500   1.1183   0.10881   0.10024  -0.0346   0.2195   1.0000
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