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SPICA 11.73% smoothed (spicasm-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: SPICA 11.73% smoothed (spicasm-il)
Reynolds number: 200,000
Max Cl/Cd: 77.63 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-spicasm-il-200000-n5.txt
Download as CSV file: xf-spicasm-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.2859   0.11660   0.11289  -0.0377   1.0000   0.0333
 -10.500  -0.2881   0.11355   0.10988  -0.0396   1.0000   0.0335
 -10.250  -0.2899   0.11035   0.10672  -0.0414   1.0000   0.0336
 -10.000  -0.2842   0.10703   0.10344  -0.0410   1.0000   0.0337
  -9.750  -0.2753   0.10419   0.10063  -0.0400   1.0000   0.0340
  -9.500  -0.2691   0.10164   0.09811  -0.0394   1.0000   0.0344
  -9.250  -0.2658   0.09915   0.09567  -0.0392   1.0000   0.0348
  -9.000  -0.2577   0.09618   0.09274  -0.0404   0.9934   0.0356
  -8.750  -0.2422   0.09242   0.08898  -0.0447   0.9795   0.0374
  -8.500  -0.2322   0.08721   0.08376  -0.0547   0.9537   0.0393
  -8.250  -0.2147   0.08078   0.07729  -0.0678   0.9233   0.0396
  -8.000  -0.1912   0.07483   0.07124  -0.0768   0.8976   0.0398
  -7.750  -0.1622   0.07163   0.06797  -0.0781   0.8777   0.0404
  -7.250  -0.1305   0.06489   0.06097  -0.0854   0.8283   0.0415
  -7.000  -0.1223   0.06170   0.05766  -0.0878   0.8085   0.0421
  -6.750  -0.1145   0.05853   0.05436  -0.0897   0.7917   0.0427
  -6.500  -0.1058   0.05522   0.05088  -0.0918   0.7768   0.0446
  -6.000  -0.0951   0.04231   0.03718  -0.0955   0.7538   0.0333
  -5.750  -0.0800   0.04008   0.03482  -0.0952   0.7428   0.0329
  -5.500  -0.0642   0.03753   0.03205  -0.0948   0.7334   0.0325
  -5.250  -0.0477   0.03475   0.02900  -0.0943   0.7241   0.0321
  -5.000  -0.0300   0.03206   0.02599  -0.0936   0.7156   0.0318
  -4.750  -0.0112   0.02948   0.02305  -0.0927   0.7075   0.0319
  -4.500   0.0087   0.02698   0.02012  -0.0917   0.7001   0.0326
  -4.250   0.0300   0.02497   0.01777  -0.0907   0.6924   0.0325
  -4.000   0.0524   0.02324   0.01570  -0.0899   0.6858   0.0324
  -3.750   0.0757   0.02168   0.01382  -0.0890   0.6788   0.0324
  -3.500   0.1000   0.02033   0.01214  -0.0883   0.6726   0.0325
  -3.250   0.1250   0.01918   0.01072  -0.0876   0.6663   0.0328
  -3.000   0.1505   0.01822   0.00951  -0.0870   0.6601   0.0331
  -2.750   0.1765   0.01745   0.00849  -0.0864   0.6549   0.0335
  -2.500   0.2022   0.01681   0.00782  -0.0860   0.6489   0.0343
  -2.250   0.2282   0.01642   0.00737  -0.0856   0.6432   0.0354
  -2.000   0.2544   0.01601   0.00687  -0.0852   0.6383   0.0365
  -1.750   0.2804   0.01551   0.00633  -0.0847   0.6327   0.0372
  -1.500   0.3062   0.01508   0.00584  -0.0842   0.6274   0.0379
  -1.000   0.3574   0.01440   0.00507  -0.0831   0.6172   0.0399
  -0.750   0.3828   0.01414   0.00482  -0.0825   0.6119   0.0412
  -0.500   0.4087   0.01397   0.00461  -0.0821   0.6072   0.0434
  -0.250   0.4346   0.01383   0.00446  -0.0816   0.6017   0.0471
   0.000   0.4604   0.01369   0.00433  -0.0811   0.5960   0.0515
   0.250   0.4863   0.01355   0.00414  -0.0807   0.5912   0.0586
   0.500   0.5119   0.01340   0.00402  -0.0802   0.5855   0.0721
   1.000   0.6235   0.01105   0.00408  -0.0920   0.5728   1.0000
   1.250   0.6469   0.01113   0.00409  -0.0911   0.5661   1.0000
   1.500   0.6705   0.01124   0.00408  -0.0902   0.5599   1.0000
   1.750   0.6940   0.01134   0.00411  -0.0893   0.5529   1.0000
   2.000   0.7175   0.01144   0.00414  -0.0883   0.5458   1.0000
   2.250   0.7412   0.01156   0.00417  -0.0875   0.5393   1.0000
   2.500   0.7649   0.01167   0.00425  -0.0866   0.5322   1.0000
   3.000   0.8123   0.01191   0.00441  -0.0849   0.5186   1.0000
   3.250   0.8358   0.01205   0.00448  -0.0840   0.5117   1.0000
   3.500   0.8594   0.01217   0.00460  -0.0831   0.5042   1.0000
   3.750   0.8828   0.01231   0.00469  -0.0822   0.4967   1.0000
   4.000   0.9063   0.01245   0.00483  -0.0813   0.4888   1.0000
   4.250   0.9295   0.01261   0.00495  -0.0804   0.4806   1.0000
   4.500   0.9528   0.01276   0.00510  -0.0795   0.4716   1.0000
   4.750   0.9756   0.01294   0.00523  -0.0786   0.4629   1.0000
   5.000   0.9985   0.01311   0.00542  -0.0776   0.4531   1.0000
   5.250   1.0211   0.01331   0.00560  -0.0767   0.4433   1.0000
   5.750   1.0651   0.01375   0.00600  -0.0746   0.4220   1.0000
   6.000   1.0868   0.01400   0.00624  -0.0735   0.4113   1.0000
   6.250   1.1077   0.01428   0.00648  -0.0723   0.4002   1.0000
   6.500   1.1285   0.01457   0.00677  -0.0711   0.3884   1.0000
   6.750   1.1491   0.01488   0.00707  -0.0698   0.3765   1.0000
   7.000   1.1690   0.01521   0.00739  -0.0685   0.3648   1.0000
   7.250   1.1881   0.01557   0.00773  -0.0671   0.3529   1.0000
   7.500   1.2066   0.01596   0.00810  -0.0656   0.3412   1.0000
   7.750   1.2251   0.01635   0.00849  -0.0641   0.3296   1.0000
   8.000   1.2427   0.01677   0.00891  -0.0625   0.3188   1.0000
   8.250   1.2589   0.01723   0.00936  -0.0607   0.3089   1.0000
   8.500   1.2756   0.01768   0.00984  -0.0590   0.2988   1.0000
   8.750   1.2909   0.01816   0.01033  -0.0571   0.2900   1.0000
   9.000   1.3038   0.01867   0.01084  -0.0547   0.2814   1.0000
   9.250   1.3173   0.01916   0.01138  -0.0525   0.2736   1.0000
   9.500   1.3283   0.01976   0.01199  -0.0500   0.2654   1.0000
   9.750   1.3406   0.02034   0.01261  -0.0479   0.2563   1.0000
  10.000   1.3498   0.02106   0.01332  -0.0454   0.2467   1.0000
  10.250   1.3588   0.02182   0.01409  -0.0430   0.2366   1.0000
  10.500   1.3683   0.02261   0.01492  -0.0409   0.2266   1.0000
  10.750   1.3757   0.02355   0.01587  -0.0386   0.2185   1.0000
  11.000   1.3845   0.02449   0.01686  -0.0367   0.2087   1.0000
  11.250   1.3923   0.02554   0.01795  -0.0349   0.2002   1.0000
  11.500   1.3982   0.02676   0.01919  -0.0331   0.1914   1.0000
  11.750   1.4063   0.02794   0.02044  -0.0316   0.1822   1.0000
  12.000   1.4112   0.02938   0.02192  -0.0301   0.1733   1.0000
  12.250   1.4148   0.03101   0.02357  -0.0286   0.1627   1.0000
  12.500   1.4180   0.03276   0.02534  -0.0274   0.1508   1.0000
  12.750   1.4189   0.03479   0.02737  -0.0262   0.1379   1.0000
  13.000   1.4189   0.03699   0.02957  -0.0252   0.1258   1.0000
  13.250   1.4174   0.03940   0.03199  -0.0243   0.1135   1.0000
  13.500   1.4136   0.04213   0.03470  -0.0235   0.1004   1.0000
  13.750   1.4080   0.04513   0.03768  -0.0229   0.0872   1.0000
  14.000   1.3991   0.04858   0.04108  -0.0224   0.0727   1.0000
  14.250   1.3897   0.05222   0.04470  -0.0221   0.0595   1.0000
  14.500   1.3786   0.05620   0.04865  -0.0221   0.0466   1.0000
  14.750   1.3671   0.06041   0.05284  -0.0223   0.0368   1.0000
  15.000   1.3571   0.06460   0.05706  -0.0226   0.0313   1.0000
  15.250   1.3482   0.06881   0.06133  -0.0232   0.0280   1.0000
  15.500   1.3406   0.07299   0.06561  -0.0239   0.0259   1.0000
  15.750   1.3338   0.07719   0.06992  -0.0248   0.0244   1.0000
  16.000   1.3242   0.08190   0.07474  -0.0259   0.0231   1.0000
  16.500   1.3077   0.09136   0.08446  -0.0286   0.0216   1.0000
  16.750   1.3002   0.09611   0.08935  -0.0301   0.0210   1.0000
  17.000   1.2913   0.10120   0.09457  -0.0318   0.0204   1.0000
  17.250   1.2821   0.10644   0.09993  -0.0337   0.0198   1.0000
  17.500   1.2729   0.11176   0.10538  -0.0358   0.0194   1.0000
  17.750   1.2627   0.11732   0.11106  -0.0380   0.0190   1.0000
  18.000   1.2520   0.12307   0.11690  -0.0405   0.0185   1.0000
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