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SPICA 11.73% smoothed (spicasm-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: SPICA 11.73% smoothed (spicasm-il)
Reynolds number: 100,000
Max Cl/Cd: 55.9 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-spicasm-il-100000-n5.txt
Download as CSV file: xf-spicasm-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.000  -0.2600   0.10156   0.09674  -0.0389   1.0000   0.0592
  -8.750  -0.2611   0.09918   0.09444  -0.0388   1.0000   0.0603
  -8.500  -0.2651   0.09704   0.09241  -0.0385   1.0000   0.0613
  -8.250  -0.2626   0.09408   0.08953  -0.0416   0.9921   0.0627
  -8.000  -0.2570   0.08982   0.08529  -0.0533   0.9641   0.0642
  -7.750  -0.2435   0.08413   0.07951  -0.0677   0.9381   0.0646
  -7.500  -0.2179   0.08059   0.07604  -0.0606   0.9349   0.0664
  -7.250  -0.1947   0.07687   0.07229  -0.0639   0.9200   0.0684
  -7.000  -0.1731   0.07266   0.06800  -0.0700   0.9029   0.0705
  -6.750  -0.1528   0.06823   0.06345  -0.0769   0.8852   0.0725
  -6.500  -0.1409   0.06384   0.05852  -0.0884   0.8621   0.0761
  -6.250  -0.1239   0.05937   0.05396  -0.0902   0.8485   0.0768
  -6.000  -0.1054   0.05588   0.05044  -0.0907   0.8359   0.0776
  -5.750  -0.0879   0.04977   0.04397  -0.0922   0.8230   0.0538
  -5.500  -0.0707   0.04693   0.04098  -0.0927   0.8110   0.0527
  -5.250  -0.0521   0.04392   0.03768  -0.0934   0.8004   0.0524
  -4.750  -0.0159   0.03647   0.02908  -0.0931   0.7798   0.0466
  -4.500   0.0057   0.03438   0.02679  -0.0928   0.7709   0.0462
  -4.250   0.0268   0.03243   0.02457  -0.0922   0.7616   0.0459
  -4.000   0.0498   0.03054   0.02233  -0.0917   0.7538   0.0456
  -3.750   0.0723   0.02886   0.02033  -0.0910   0.7451   0.0455
  -3.500   0.0968   0.02728   0.01836  -0.0903   0.7379   0.0456
  -3.250   0.1212   0.02604   0.01666  -0.0895   0.7299   0.0466
  -3.000   0.1460   0.02496   0.01550  -0.0892   0.7229   0.0479
  -2.750   0.1713   0.02400   0.01435  -0.0887   0.7159   0.0487
  -2.500   0.1971   0.02304   0.01316  -0.0881   0.7087   0.0490
  -2.250   0.2241   0.02218   0.01208  -0.0877   0.7030   0.0496
  -2.000   0.2496   0.02144   0.01122  -0.0871   0.6957   0.0504
  -1.750   0.2765   0.02076   0.01039  -0.0866   0.6898   0.0515
  -1.500   0.3025   0.02020   0.00972  -0.0860   0.6835   0.0529
  -1.250   0.3282   0.01973   0.00918  -0.0854   0.6771   0.0555
  -1.000   0.3543   0.01927   0.00873  -0.0850   0.6719   0.0588
  -0.750   0.3783   0.01892   0.00837  -0.0842   0.6652   0.0616
  -0.500   0.4034   0.01859   0.00797  -0.0835   0.6592   0.0648
  -0.250   0.4287   0.01824   0.00759  -0.0828   0.6540   0.0698
   0.000   0.4528   0.01803   0.00739  -0.0821   0.6473   0.0789
   0.250   0.4790   0.01776   0.00712  -0.0816   0.6416   0.0987
   0.500   0.4981   0.01604   0.00710  -0.0806   0.6362   0.5812
   0.750   0.5846   0.01533   0.00694  -0.0915   0.6282   1.0000
   1.000   0.6095   0.01547   0.00686  -0.0908   0.6230   1.0000
   1.250   0.6311   0.01568   0.00699  -0.0896   0.6155   1.0000
   1.500   0.6552   0.01583   0.00700  -0.0887   0.6093   1.0000
   1.750   0.6784   0.01602   0.00708  -0.0878   0.6028   1.0000
   2.000   0.7013   0.01620   0.00719  -0.0868   0.5955   1.0000
   2.250   0.7261   0.01635   0.00720  -0.0860   0.5894   1.0000
   2.500   0.7478   0.01656   0.00739  -0.0849   0.5812   1.0000
   2.750   0.7729   0.01669   0.00740  -0.0842   0.5747   1.0000
   3.000   0.7943   0.01691   0.00763  -0.0830   0.5661   1.0000
   3.250   0.8189   0.01705   0.00767  -0.0822   0.5591   1.0000
   3.500   0.8407   0.01728   0.00791  -0.0811   0.5507   1.0000
   3.750   0.8649   0.01743   0.00799  -0.0803   0.5435   1.0000
   4.000   0.8868   0.01766   0.00825  -0.0792   0.5351   1.0000
   4.250   0.9107   0.01782   0.00838  -0.0784   0.5277   1.0000
   4.500   0.9324   0.01806   0.00865  -0.0773   0.5189   1.0000
   4.750   0.9562   0.01822   0.00876  -0.0764   0.5112   1.0000
   5.000   0.9773   0.01848   0.00909  -0.0753   0.5016   1.0000
   5.250   1.0007   0.01865   0.00922  -0.0744   0.4936   1.0000
   5.500   1.0215   0.01891   0.00954  -0.0732   0.4834   1.0000
   5.750   1.0433   0.01914   0.00979  -0.0721   0.4740   1.0000
   6.000   1.0653   0.01935   0.01000  -0.0710   0.4646   1.0000
   6.250   1.0856   0.01964   0.01035  -0.0697   0.4536   1.0000
   6.500   1.1065   0.01992   0.01063  -0.0685   0.4433   1.0000
   6.750   1.1275   0.02017   0.01088  -0.0673   0.4331   1.0000
   7.000   1.1465   0.02053   0.01129  -0.0659   0.4214   1.0000
   7.250   1.1657   0.02089   0.01168  -0.0645   0.4102   1.0000
   7.500   1.1848   0.02126   0.01204  -0.0631   0.3993   1.0000
   7.750   1.2029   0.02168   0.01248  -0.0615   0.3880   1.0000
   8.000   1.2199   0.02215   0.01300  -0.0599   0.3763   1.0000
   8.250   1.2367   0.02264   0.01351  -0.0582   0.3654   1.0000
   8.500   1.2531   0.02314   0.01399  -0.0565   0.3551   1.0000
   8.750   1.2679   0.02371   0.01464  -0.0547   0.3442   1.0000
   9.000   1.2825   0.02430   0.01528  -0.0528   0.3343   1.0000
   9.500   1.3074   0.02557   0.01661  -0.0484   0.3156   1.0000
   9.750   1.3195   0.02625   0.01732  -0.0463   0.3074   1.0000
  10.000   1.3302   0.02700   0.01815  -0.0440   0.2988   1.0000
  10.250   1.3414   0.02779   0.01897  -0.0420   0.2910   1.0000
  10.500   1.3515   0.02864   0.01990  -0.0399   0.2831   1.0000
  10.750   1.3618   0.02954   0.02085  -0.0380   0.2757   1.0000
  11.000   1.3703   0.03052   0.02193  -0.0360   0.2680   1.0000
  11.250   1.3790   0.03155   0.02303  -0.0341   0.2607   1.0000
  11.500   1.3849   0.03272   0.02427  -0.0321   0.2527   1.0000
  11.750   1.3894   0.03401   0.02565  -0.0303   0.2443   1.0000
  12.000   1.3924   0.03542   0.02709  -0.0284   0.2358   1.0000
  12.250   1.3930   0.03711   0.02893  -0.0268   0.2267   1.0000
  12.500   1.3937   0.03885   0.03068  -0.0253   0.2181   1.0000
  12.750   1.3917   0.04094   0.03290  -0.0240   0.2086   1.0000
  13.000   1.3899   0.04315   0.03520  -0.0229   0.1995   1.0000
  13.250   1.3869   0.04553   0.03761  -0.0220   0.1907   1.0000
  13.500   1.3836   0.04818   0.04041  -0.0214   0.1813   1.0000
  13.750   1.3784   0.05108   0.04339  -0.0210   0.1718   1.0000
  14.250   1.3660   0.05756   0.05007  -0.0208   0.1528   1.0000
  14.500   1.3596   0.06105   0.05364  -0.0210   0.1440   1.0000
  14.750   1.3518   0.06483   0.05749  -0.0214   0.1358   1.0000
  15.000   1.3440   0.06883   0.06160  -0.0220   0.1264   1.0000
  15.250   1.3341   0.07322   0.06608  -0.0228   0.1175   1.0000
  15.500   1.3215   0.07815   0.07105  -0.0240   0.1086   1.0000
  15.750   1.3086   0.08334   0.07632  -0.0254   0.0990   1.0000
  16.000   1.2939   0.08903   0.08206  -0.0272   0.0891   1.0000
  16.250   1.2790   0.09489   0.08798  -0.0291   0.0805   1.0000
  16.500   1.2623   0.10122   0.09434  -0.0314   0.0724   1.0000
  16.750   1.2468   0.10752   0.10069  -0.0339   0.0658   1.0000
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