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SPICA 11.73% smoothed (spicasm-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: SPICA 11.73% smoothed (spicasm-il)
Reynolds number: 200,000
Max Cl/Cd: 77.88 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-spicasm-il-200000.txt
Download as CSV file: xf-spicasm-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.750  -0.2057   0.10059   0.09743  -0.0410   1.0000   0.0463
  -9.500  -0.2196   0.09875   0.09568  -0.0416   1.0000   0.0465
  -9.250  -0.2293   0.09631   0.09332  -0.0437   0.9975   0.0467
  -9.000  -0.2030   0.09005   0.08706  -0.0441   0.9939   0.0474
  -8.750  -0.1771   0.08570   0.08269  -0.0458   0.9878   0.0487
  -8.500  -0.1592   0.08126   0.07825  -0.0497   0.9797   0.0502
  -8.250  -0.1435   0.07658   0.07356  -0.0543   0.9709   0.0519
  -8.000  -0.2632   0.08763   0.08452  -0.0428   0.9923   0.0485
  -7.750  -0.2372   0.08344   0.08033  -0.0485   0.9834   0.0499
  -7.500  -0.2150   0.07899   0.07587  -0.0554   0.9684   0.0516
  -7.250  -0.1900   0.07317   0.07000  -0.0687   0.9482   0.0544
  -7.000  -0.1611   0.06458   0.06105  -0.0890   0.9274   0.0561
  -6.750  -0.1356   0.06069   0.05723  -0.0896   0.9144   0.0570
  -6.500  -0.1085   0.05752   0.05399  -0.0922   0.8979   0.0582
  -6.250  -0.0863   0.05441   0.05074  -0.0950   0.8787   0.0601
  -6.000  -0.0699   0.05143   0.04757  -0.0971   0.8588   0.0628
  -5.750  -0.0600   0.04778   0.04325  -0.1001   0.8401   0.0672
  -5.500  -0.0434   0.04468   0.04019  -0.0997   0.8268   0.0683
  -5.250  -0.0262   0.04261   0.03804  -0.0993   0.8146   0.0698
  -5.000  -0.0092   0.04068   0.03598  -0.0988   0.8023   0.0720
  -4.750   0.0128   0.04121   0.03575  -0.0981   0.7906   0.0791
  -4.500   0.0270   0.03609   0.03065  -0.0983   0.7823   0.0811
  -4.250   0.0460   0.03415   0.02872  -0.0977   0.7722   0.0831
  -4.000   0.0671   0.03265   0.02707  -0.0972   0.7642   0.0871
  -3.750   0.0875   0.03098   0.02498  -0.0964   0.7556   0.0958
  -3.500   0.1093   0.02931   0.02328  -0.0960   0.7486   0.0991
  -3.250   0.1309   0.02817   0.02185  -0.0952   0.7405   0.1116
  -3.000   0.1543   0.02688   0.02051  -0.0948   0.7344   0.1184
  -2.750   0.1757   0.02560   0.01912  -0.0942   0.7267   0.1312
  -2.500   0.1988   0.02451   0.01788  -0.0936   0.7204   0.1471
  -2.250   0.2370   0.02074   0.01280  -0.0908   0.7153   0.0651
  -2.000   0.2626   0.01929   0.01119  -0.0901   0.7086   0.0626
  -1.750   0.2900   0.01829   0.00994  -0.0896   0.7031   0.0613
  -1.500   0.3160   0.01771   0.00926  -0.0890   0.6967   0.0630
  -1.250   0.3428   0.01711   0.00854  -0.0884   0.6905   0.0640
  -1.000   0.3703   0.01654   0.00783  -0.0880   0.6854   0.0646
  -0.750   0.3956   0.01609   0.00738  -0.0873   0.6786   0.0658
  -0.500   0.4214   0.01546   0.00672  -0.0866   0.6728   0.0680
  -0.250   0.4465   0.01506   0.00637  -0.0860   0.6673   0.0726
   0.000   0.4713   0.01484   0.00616  -0.0853   0.6606   0.0795
   0.250   0.4967   0.01445   0.00575  -0.0846   0.6552   0.0926
   0.500   0.5168   0.01357   0.00552  -0.0833   0.6490   0.2646
   0.750   0.6137   0.01179   0.00539  -0.0971   0.6411   1.0000
   1.000   0.6375   0.01193   0.00540  -0.0962   0.6351   1.0000
   1.250   0.6602   0.01204   0.00544  -0.0951   0.6277   1.0000
   1.500   0.6856   0.01218   0.00540  -0.0945   0.6218   1.0000
   1.750   0.7073   0.01229   0.00551  -0.0932   0.6138   1.0000
   2.000   0.7322   0.01241   0.00549  -0.0925   0.6074   1.0000
   2.250   0.7549   0.01255   0.00562  -0.0914   0.6000   1.0000
   2.500   0.7792   0.01267   0.00566  -0.0906   0.5932   1.0000
   2.750   0.8033   0.01283   0.00576  -0.0898   0.5867   1.0000
   3.000   0.8265   0.01296   0.00587  -0.0888   0.5792   1.0000
   3.250   0.8522   0.01311   0.00591  -0.0883   0.5732   1.0000
   3.500   0.8740   0.01324   0.00608  -0.0871   0.5649   1.0000
   3.750   0.8995   0.01337   0.00612  -0.0865   0.5586   1.0000
   4.000   0.9215   0.01352   0.00632  -0.0853   0.5502   1.0000
   4.250   0.9465   0.01363   0.00635  -0.0846   0.5431   1.0000
   4.500   0.9686   0.01377   0.00654  -0.0835   0.5345   1.0000
   4.750   0.9934   0.01388   0.00658  -0.0828   0.5271   1.0000
   5.000   1.0152   0.01402   0.00677  -0.0816   0.5176   1.0000
   5.250   1.0396   0.01413   0.00682  -0.0809   0.5097   1.0000
   5.500   1.0613   0.01426   0.00701  -0.0797   0.4995   1.0000
   5.750   1.0839   0.01440   0.00715  -0.0786   0.4900   1.0000
   6.000   1.1071   0.01452   0.00723  -0.0777   0.4802   1.0000
   6.250   1.1280   0.01468   0.00744  -0.0764   0.4686   1.0000
   6.500   1.1496   0.01486   0.00764  -0.0752   0.4573   1.0000
   6.750   1.1710   0.01507   0.00782  -0.0740   0.4457   1.0000
   7.000   1.1923   0.01531   0.00800  -0.0728   0.4338   1.0000
   7.250   1.2120   0.01558   0.00830  -0.0714   0.4206   1.0000
   7.500   1.2315   0.01589   0.00862  -0.0699   0.4073   1.0000
   7.750   1.2506   0.01625   0.00897  -0.0685   0.3942   1.0000
   8.000   1.2694   0.01664   0.00935  -0.0669   0.3813   1.0000
   8.250   1.2878   0.01707   0.00976  -0.0654   0.3692   1.0000
   8.500   1.3061   0.01754   0.01017  -0.0639   0.3576   1.0000
   8.750   1.3228   0.01798   0.01066  -0.0621   0.3456   1.0000
   9.000   1.3397   0.01848   0.01118  -0.0604   0.3346   1.0000
   9.250   1.3561   0.01902   0.01170  -0.0587   0.3243   1.0000
   9.500   1.3705   0.01956   0.01220  -0.0567   0.3132   1.0000
   9.750   1.3823   0.02006   0.01277  -0.0542   0.3017   1.0000
  10.000   1.3922   0.02061   0.01333  -0.0515   0.2912   1.0000
  10.250   1.4010   0.02123   0.01391  -0.0486   0.2810   1.0000
  10.500   1.4096   0.02183   0.01459  -0.0458   0.2714   1.0000
  10.750   1.4184   0.02252   0.01533  -0.0433   0.2622   1.0000
  11.000   1.4264   0.02330   0.01609  -0.0408   0.2535   1.0000
  11.250   1.4337   0.02408   0.01698  -0.0383   0.2443   1.0000
  11.500   1.4397   0.02503   0.01794  -0.0359   0.2356   1.0000
  11.750   1.4454   0.02601   0.01901  -0.0337   0.2265   1.0000
  12.000   1.4507   0.02713   0.02020  -0.0317   0.2176   1.0000
  12.250   1.4532   0.02849   0.02155  -0.0297   0.2088   1.0000
  12.500   1.4575   0.02983   0.02303  -0.0280   0.1987   1.0000
  12.750   1.4609   0.03137   0.02463  -0.0265   0.1897   1.0000
  13.000   1.4607   0.03325   0.02653  -0.0251   0.1800   1.0000
  13.250   1.4627   0.03512   0.02852  -0.0240   0.1685   1.0000
  13.500   1.4616   0.03736   0.03081  -0.0230   0.1554   1.0000
  13.750   1.4553   0.04021   0.03364  -0.0222   0.1395   1.0000
  14.000   1.4464   0.04347   0.03687  -0.0215   0.1185   1.0000
  14.250   1.4291   0.04774   0.04101  -0.0209   0.0944   1.0000
  14.500   1.4093   0.05252   0.04565  -0.0207   0.0735   1.0000
  14.750   1.3898   0.05750   0.05055  -0.0207   0.0597   1.0000
  15.000   1.3723   0.06253   0.05556  -0.0211   0.0506   1.0000
  15.250   1.3602   0.06710   0.06019  -0.0216   0.0459   1.0000
  15.500   1.3473   0.07196   0.06509  -0.0224   0.0430   1.0000
  15.750   1.3359   0.07677   0.07000  -0.0234   0.0404   1.0000
  16.000   1.3263   0.08147   0.07482  -0.0245   0.0387   1.0000
  16.250   1.3154   0.08649   0.07993  -0.0258   0.0372   1.0000
  16.500   1.3045   0.09161   0.08512  -0.0272   0.0362   1.0000
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