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USA 35 A AIRFOIL (usa35a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: USA 35 A AIRFOIL (usa35a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 122.31 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-usa35a-il-1000000.txt
Download as CSV file: xf-usa35a-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: USA 35 A AIRFOIL                                
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.7011   0.03275   0.02939  -0.1380   0.9356   0.0305
 -13.750  -0.7069   0.02984   0.02629  -0.1395   0.9188   0.0305
 -13.500  -0.7033   0.02825   0.02456  -0.1387   0.9046   0.0307
 -13.250  -0.6915   0.02695   0.02313  -0.1382   0.8921   0.0308
 -13.000  -0.6762   0.02589   0.02195  -0.1377   0.8797   0.0310
 -12.750  -0.6583   0.02496   0.02092  -0.1373   0.8688   0.0311
 -12.250  -0.6194   0.02325   0.01898  -0.1365   0.8484   0.0316
 -12.000  -0.5992   0.02241   0.01801  -0.1361   0.8387   0.0318
 -11.750  -0.5780   0.02154   0.01702  -0.1357   0.8305   0.0320
 -11.500  -0.5562   0.02074   0.01610  -0.1353   0.8218   0.0322
 -11.250  -0.5336   0.02001   0.01524  -0.1350   0.8139   0.0324
 -11.000  -0.5100   0.01930   0.01443  -0.1347   0.8063   0.0326
 -10.750  -0.4862   0.01868   0.01368  -0.1343   0.7980   0.0328
 -10.500  -0.4614   0.01809   0.01298  -0.1340   0.7907   0.0330
 -10.250  -0.4362   0.01756   0.01235  -0.1338   0.7826   0.0332
 -10.000  -0.4107   0.01712   0.01179  -0.1334   0.7741   0.0334
  -9.750  -0.3863   0.01631   0.01089  -0.1331   0.7673   0.0337
  -9.500  -0.3619   0.01556   0.01006  -0.1328   0.7591   0.0340
  -9.250  -0.3359   0.01512   0.00955  -0.1325   0.7511   0.0344
  -9.000  -0.3089   0.01475   0.00914  -0.1324   0.7429   0.0347
  -8.750  -0.2820   0.01444   0.00877  -0.1322   0.7336   0.0350
  -8.500  -0.2545   0.01412   0.00840  -0.1320   0.7250   0.0354
  -8.250  -0.2274   0.01383   0.00803  -0.1318   0.7145   0.0358
  -8.000  -0.1999   0.01354   0.00767  -0.1317   0.7045   0.0362
  -7.750  -0.1727   0.01329   0.00732  -0.1314   0.6922   0.0366
  -7.500  -0.1450   0.01305   0.00700  -0.1313   0.6797   0.0370
  -7.250  -0.1175   0.01287   0.00671  -0.1310   0.6657   0.0373
  -7.000  -0.0914   0.01244   0.00620  -0.1307   0.6508   0.0380
  -6.750  -0.0639   0.01222   0.00593  -0.1305   0.6363   0.0386
  -6.500  -0.0363   0.01210   0.00574  -0.1303   0.6217   0.0392
  -6.250  -0.0089   0.01199   0.00555  -0.1301   0.6071   0.0399
  -6.000   0.0191   0.01185   0.00534  -0.1300   0.5949   0.0406
  -5.750   0.0469   0.01175   0.00515  -0.1298   0.5837   0.0412
  -5.500   0.0746   0.01157   0.00489  -0.1296   0.5734   0.0419
  -5.250   0.1021   0.01138   0.00467  -0.1295   0.5643   0.0428
  -5.000   0.1306   0.01127   0.00453  -0.1294   0.5569   0.0437
  -4.750   0.1585   0.01121   0.00441  -0.1293   0.5491   0.0447
  -4.500   0.1872   0.01113   0.00428  -0.1293   0.5435   0.0457
  -4.250   0.2156   0.01094   0.00408  -0.1292   0.5385   0.0470
  -4.000   0.2440   0.01087   0.00399  -0.1292   0.5333   0.0483
  -3.750   0.2723   0.01084   0.00392  -0.1291   0.5280   0.0497
  -3.500   0.3010   0.01075   0.00380  -0.1291   0.5245   0.0513
  -3.250   0.3301   0.01063   0.00372  -0.1292   0.5219   0.0531
  -3.000   0.3591   0.01058   0.00365  -0.1292   0.5187   0.0550
  -2.750   0.3877   0.01049   0.00355  -0.1292   0.5152   0.0569
  -2.500   0.4161   0.01046   0.00351  -0.1292   0.5114   0.0589
  -2.250   0.4443   0.01048   0.00349  -0.1291   0.5070   0.0610
  -2.000   0.4731   0.01039   0.00341  -0.1292   0.5043   0.0634
  -1.750   0.5023   0.01034   0.00338  -0.1293   0.5021   0.0659
  -1.500   0.5313   0.01027   0.00332  -0.1294   0.4996   0.0686
  -1.250   0.5601   0.01024   0.00330  -0.1294   0.4967   0.0715
  -1.000   0.5887   0.01022   0.00326  -0.1294   0.4936   0.0744
  -0.750   0.6168   0.01021   0.00325  -0.1294   0.4900   0.0778
  -0.500   0.6445   0.01026   0.00327  -0.1293   0.4856   0.0815
  -0.250   0.6737   0.01018   0.00324  -0.1294   0.4836   0.0860
   0.000   0.7027   0.01012   0.00322  -0.1295   0.4810   0.0914
   0.250   0.7314   0.01008   0.00320  -0.1296   0.4781   0.0982
   0.500   0.7597   0.01004   0.00320  -0.1296   0.4749   0.1092
   0.750   0.7875   0.00996   0.00322  -0.1296   0.4713   0.1414
   1.000   0.8146   0.00990   0.00330  -0.1295   0.4671   0.2056
   1.500   0.8716   0.00969   0.00339  -0.1298   0.4616   0.3015
   1.750   0.8995   0.00947   0.00348  -0.1300   0.4580   0.4240
   2.000   0.9270   0.00939   0.00356  -0.1300   0.4538   0.4977
   2.250   0.9527   0.00917   0.00370  -0.1297   0.4485   0.6435
   2.500   0.9779   0.00888   0.00383  -0.1291   0.4442   0.8047
   2.750   1.0044   0.00864   0.00394  -0.1284   0.4388   0.9919
   3.000   1.0329   0.00877   0.00400  -0.1285   0.4328   1.0000
   3.250   1.0591   0.00891   0.00409  -0.1282   0.4273   1.0000
   3.500   1.0865   0.00901   0.00416  -0.1281   0.4215   1.0000
   3.750   1.1120   0.00918   0.00426  -0.1277   0.4136   1.0000
   4.000   1.1379   0.00933   0.00437  -0.1273   0.4061   1.0000
   4.250   1.1631   0.00951   0.00449  -0.1269   0.3976   1.0000
   4.500   1.1876   0.00971   0.00464  -0.1263   0.3895   1.0000
   4.750   1.2117   0.00993   0.00480  -0.1257   0.3805   1.0000
   5.000   1.2350   0.01017   0.00498  -0.1249   0.3719   1.0000
   5.250   1.2575   0.01043   0.00517  -0.1240   0.3630   1.0000
   5.500   1.2784   0.01069   0.00539  -0.1228   0.3553   1.0000
   5.750   1.2998   0.01095   0.00560  -0.1217   0.3485   1.0000
   6.000   1.3195   0.01129   0.00588  -0.1203   0.3415   1.0000
   6.250   1.3424   0.01151   0.00610  -0.1196   0.3368   1.0000
   6.500   1.3635   0.01181   0.00637  -0.1185   0.3314   1.0000
   6.750   1.3832   0.01218   0.00669  -0.1173   0.3258   1.0000
   7.000   1.4055   0.01245   0.00696  -0.1165   0.3224   1.0000
   7.250   1.4277   0.01272   0.00723  -0.1157   0.3189   1.0000
   7.500   1.4485   0.01306   0.00755  -0.1148   0.3151   1.0000
   7.750   1.4678   0.01347   0.00794  -0.1136   0.3110   1.0000
   8.000   1.4876   0.01386   0.00832  -0.1125   0.3073   1.0000
   8.250   1.5098   0.01415   0.00863  -0.1119   0.3046   1.0000
   8.500   1.5306   0.01451   0.00899  -0.1110   0.3014   1.0000
   8.750   1.5502   0.01493   0.00941  -0.1101   0.2981   1.0000
   9.000   1.5679   0.01545   0.00992  -0.1088   0.2945   1.0000
   9.250   1.5858   0.01597   0.01043  -0.1077   0.2911   1.0000
   9.500   1.6073   0.01631   0.01081  -0.1071   0.2889   1.0000
   9.750   1.6271   0.01676   0.01127  -0.1063   0.2861   1.0000
  10.000   1.6456   0.01727   0.01180  -0.1053   0.2829   1.0000
  10.250   1.6618   0.01792   0.01244  -0.1041   0.2793   1.0000
  10.500   1.6764   0.01868   0.01319  -0.1028   0.2755   1.0000
  10.750   1.6967   0.01913   0.01368  -0.1022   0.2732   1.0000
  11.000   1.7148   0.01971   0.01429  -0.1013   0.2699   1.0000
  11.250   1.7309   0.02043   0.01502  -0.1003   0.2660   1.0000
  11.500   1.7431   0.02140   0.01598  -0.0989   0.2615   1.0000
  11.750   1.7597   0.02211   0.01672  -0.0981   0.2580   1.0000
  12.000   1.7753   0.02290   0.01754  -0.0972   0.2538   1.0000
  12.250   1.7871   0.02396   0.01859  -0.0959   0.2485   1.0000
  12.500   1.7983   0.02509   0.01973  -0.0947   0.2430   1.0000
  12.750   1.8100   0.02620   0.02084  -0.0936   0.2363   1.0000
  13.000   1.8165   0.02772   0.02235  -0.0921   0.2293   1.0000
  13.250   1.8246   0.02917   0.02380  -0.0909   0.2216   1.0000
  13.500   1.8287   0.03098   0.02559  -0.0894   0.2135   1.0000
  13.750   1.8292   0.03312   0.02770  -0.0878   0.2043   1.0000
  14.000   1.8309   0.03523   0.02982  -0.0864   0.1965   1.0000
  14.250   1.8279   0.03782   0.03240  -0.0848   0.1893   1.0000
  14.500   1.8297   0.04006   0.03466  -0.0837   0.1841   1.0000
  14.750   1.8265   0.04279   0.03740  -0.0824   0.1792   1.0000
  15.000   1.8270   0.04525   0.03990  -0.0814   0.1754   1.0000
  15.250   1.8268   0.04784   0.04253  -0.0806   0.1722   1.0000
  15.500   1.8233   0.05080   0.04552  -0.0796   0.1690   1.0000
  15.750   1.8167   0.05412   0.04887  -0.0787   0.1656   1.0000
  16.000   1.8200   0.05645   0.05126  -0.0782   0.1638   1.0000
  16.250   1.8204   0.05913   0.05400  -0.0777   0.1620   1.0000
  16.500   1.8202   0.06188   0.05681  -0.0772   0.1602   1.0000
  16.750   1.8161   0.06508   0.06006  -0.0767   0.1583   1.0000
  17.000   1.8095   0.06858   0.06360  -0.0762   0.1563   1.0000
  17.250   1.8017   0.07223   0.06730  -0.0758   0.1540   1.0000
  17.500   1.8036   0.07485   0.06998  -0.0756   0.1529   1.0000
  17.750   1.8071   0.07724   0.07244  -0.0754   0.1517   1.0000
  18.000   1.8058   0.08021   0.07548  -0.0753   0.1503   1.0000
  18.250   1.8055   0.08304   0.07836  -0.0751   0.1487   1.0000
  18.500   1.8013   0.08639   0.08176  -0.0751   0.1472   1.0000
  18.750   1.7972   0.08973   0.08514  -0.0751   0.1455   1.0000
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