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SM701 (sm701-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: SM701 (sm701-il)
Reynolds number: 1,000,000
Max Cl/Cd: 110.87 at α=2.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sm701-il-1000000.txt
Download as CSV file: xf-sm701-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SM701                                           
  
 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  -0.6237   0.07051   0.06829  -0.0809   0.9974   0.0133
 -13.750  -0.6528   0.06018   0.05772  -0.0904   0.9959   0.0133
 -13.500  -0.6685   0.05311   0.05044  -0.0972   0.9945   0.0133
 -13.250  -0.6813   0.04720   0.04431  -0.1025   0.9926   0.0133
 -13.000  -0.6844   0.04316   0.04008  -0.1061   0.9896   0.0135
 -12.750  -0.6802   0.03982   0.03654  -0.1097   0.9872   0.0136
 -12.500  -0.6692   0.03721   0.03375  -0.1135   0.9853   0.0137
 -12.250  -0.6563   0.03456   0.03090  -0.1172   0.9837   0.0138
 -12.000  -0.6610   0.03105   0.02712  -0.1180   0.9783   0.0139
 -11.750  -0.6513   0.02771   0.02360  -0.1196   0.9752   0.0143
 -11.500  -0.6270   0.02632   0.02214  -0.1218   0.9734   0.0145
 -11.250  -0.6006   0.02492   0.02065  -0.1242   0.9721   0.0148
 -11.000  -0.5709   0.02370   0.01936  -0.1268   0.9712   0.0150
 -10.750  -0.5602   0.02273   0.01831  -0.1250   0.9641   0.0152
 -10.500  -0.5326   0.02157   0.01707  -0.1264   0.9618   0.0154
 -10.250  -0.5040   0.02051   0.01592  -0.1279   0.9598   0.0157
 -10.000  -0.4750   0.01942   0.01472  -0.1292   0.9579   0.0160
  -9.750  -0.4624   0.01867   0.01390  -0.1269   0.9497   0.0162
  -9.500  -0.4367   0.01785   0.01300  -0.1273   0.9455   0.0165
  -9.250  -0.4163   0.01716   0.01223  -0.1264   0.9386   0.0167
  -9.000  -0.3930   0.01656   0.01156  -0.1260   0.9310   0.0169
  -8.750  -0.3699   0.01626   0.01117  -0.1255   0.9211   0.0172
  -8.500  -0.3482   0.01482   0.00967  -0.1251   0.9111   0.0176
  -8.250  -0.3244   0.01405   0.00885  -0.1249   0.8989   0.0179
  -8.000  -0.3013   0.01350   0.00823  -0.1245   0.8854   0.0183
  -7.750  -0.2782   0.01306   0.00771  -0.1240   0.8725   0.0186
  -7.500  -0.2552   0.01265   0.00723  -0.1235   0.8609   0.0189
  -7.250  -0.2320   0.01228   0.00677  -0.1230   0.8504   0.0193
  -7.000  -0.2087   0.01192   0.00635  -0.1224   0.8407   0.0197
  -6.750  -0.1847   0.01159   0.00595  -0.1220   0.8323   0.0201
  -6.500  -0.1602   0.01128   0.00559  -0.1216   0.8245   0.0205
  -6.250  -0.1349   0.01103   0.00528  -0.1213   0.8179   0.0208
  -6.000  -0.1107   0.01059   0.00478  -0.1210   0.8113   0.0215
  -5.750  -0.0855   0.01025   0.00439  -0.1208   0.8051   0.0223
  -5.500  -0.0591   0.00999   0.00411  -0.1207   0.7997   0.0230
  -5.250  -0.0324   0.00977   0.00385  -0.1207   0.7942   0.0238
  -5.000  -0.0052   0.00959   0.00362  -0.1207   0.7891   0.0246
  -4.750   0.0222   0.00941   0.00341  -0.1207   0.7842   0.0254
  -4.500   0.0494   0.00916   0.00315  -0.1208   0.7789   0.0275
  -4.250   0.0769   0.00901   0.00296  -0.1208   0.7732   0.0300
  -4.000   0.1041   0.00871   0.00275  -0.1209   0.7675   0.0497
  -3.750   0.1310   0.00823   0.00252  -0.1212   0.7615   0.1106
  -3.500   0.1584   0.00786   0.00232  -0.1215   0.7553   0.1744
  -3.250   0.1861   0.00721   0.00207  -0.1222   0.7496   0.2897
  -3.000   0.2146   0.00640   0.00183  -0.1232   0.7440   0.4606
  -2.750   0.2436   0.00631   0.00182  -0.1235   0.7388   0.5091
  -2.500   0.2726   0.00629   0.00182  -0.1238   0.7341   0.5305
  -2.250   0.3016   0.00628   0.00182  -0.1240   0.7291   0.5458
  -2.000   0.3304   0.00632   0.00181  -0.1241   0.7241   0.5555
  -1.750   0.3593   0.00634   0.00182  -0.1243   0.7192   0.5640
  -1.500   0.3882   0.00635   0.00184  -0.1245   0.7142   0.5754
  -1.250   0.4169   0.00642   0.00187  -0.1246   0.7089   0.5877
  -1.000   0.4454   0.00651   0.00195  -0.1247   0.7036   0.6005
  -0.750   0.4741   0.00651   0.00196  -0.1248   0.6981   0.6068
  -0.500   0.5024   0.00653   0.00196  -0.1249   0.6921   0.6096
  -0.250   0.5307   0.00656   0.00196  -0.1250   0.6864   0.6124
   0.000   0.5591   0.00658   0.00197  -0.1251   0.6795   0.6150
   0.250   0.5869   0.00664   0.00197  -0.1250   0.6725   0.6176
   0.500   0.6154   0.00666   0.00198  -0.1252   0.6652   0.6199
   0.750   0.6427   0.00669   0.00199  -0.1251   0.6571   0.6231
   1.000   0.6705   0.00671   0.00201  -0.1251   0.6480   0.6259
   1.250   0.6974   0.00677   0.00204  -0.1249   0.6377   0.6287
   1.500   0.7244   0.00683   0.00207  -0.1247   0.6256   0.6316
   1.750   0.7505   0.00693   0.00211  -0.1244   0.6100   0.6346
   2.000   0.7754   0.00707   0.00216  -0.1238   0.5898   0.6373
   2.250   0.7994   0.00721   0.00224  -0.1231   0.5643   0.6410
   2.500   0.8218   0.00746   0.00236  -0.1220   0.5344   0.6442
   2.750   0.8434   0.00775   0.00251  -0.1209   0.5033   0.6475
   3.000   0.8651   0.00806   0.00269  -0.1198   0.4741   0.6508
   3.250   0.8878   0.00835   0.00285  -0.1188   0.4494   0.6539
   3.500   0.9101   0.00860   0.00302  -0.1179   0.4266   0.6579
   3.750   0.9326   0.00886   0.00320  -0.1170   0.4041   0.6619
   4.000   0.9549   0.00913   0.00339  -0.1160   0.3840   0.6661
   4.250   0.9773   0.00939   0.00357  -0.1151   0.3667   0.6700
   4.500   0.9991   0.00963   0.00375  -0.1140   0.3503   0.6741
   4.750   1.0202   0.00986   0.00394  -0.1128   0.3352   0.6785
   5.000   1.0410   0.01009   0.00412  -0.1116   0.3216   0.6832
   5.250   1.0619   0.01033   0.00432  -0.1104   0.3096   0.6877
   5.500   1.0824   0.01059   0.00455  -0.1091   0.2975   0.6926
   5.750   1.1036   0.01084   0.00477  -0.1080   0.2859   0.6981
   6.000   1.1247   0.01110   0.00500  -0.1069   0.2754   0.7038
   6.250   1.1450   0.01138   0.00527  -0.1056   0.2654   0.7093
   6.500   1.1664   0.01162   0.00551  -0.1046   0.2564   0.7154
   6.750   1.1866   0.01192   0.00578  -0.1034   0.2473   0.7215
   7.000   1.2068   0.01221   0.00606  -0.1022   0.2385   0.7278
   7.250   1.2274   0.01248   0.00635  -0.1011   0.2313   0.7348
   7.500   1.2475   0.01279   0.00665  -0.0999   0.2237   0.7417
   7.750   1.2671   0.01310   0.00698  -0.0986   0.2166   0.7493
   8.000   1.2868   0.01342   0.00730  -0.0974   0.2096   0.7573
   8.250   1.3056   0.01378   0.00767  -0.0961   0.2030   0.7661
   8.500   1.3259   0.01408   0.00800  -0.0950   0.1977   0.7752
   8.750   1.3435   0.01448   0.00841  -0.0935   0.1913   0.7851
   9.000   1.3627   0.01482   0.00880  -0.0924   0.1861   0.7951
   9.500   1.3977   0.01567   0.00970  -0.0895   0.1750   0.8185
   9.750   1.4166   0.01602   0.01011  -0.0883   0.1711   0.8318
  10.000   1.4340   0.01643   0.01058  -0.0869   0.1665   0.8471
  10.250   1.4487   0.01695   0.01114  -0.0851   0.1613   0.8665
  10.500   1.4643   0.01734   0.01163  -0.0834   0.1572   0.8930
  10.750   1.4732   0.01761   0.01205  -0.0804   0.1531   1.0000
  11.000   1.4888   0.01827   0.01268  -0.0790   0.1475   1.0000
  11.250   1.5058   0.01885   0.01328  -0.0779   0.1434   1.0000
  11.500   1.5228   0.01944   0.01388  -0.0768   0.1388   1.0000
  11.750   1.5364   0.02024   0.01466  -0.0754   0.1330   1.0000
  12.000   1.5529   0.02088   0.01532  -0.0743   0.1287   1.0000
  12.250   1.5677   0.02163   0.01608  -0.0731   0.1243   1.0000
  12.500   1.5798   0.02257   0.01700  -0.0717   0.1187   1.0000
  12.750   1.5955   0.02330   0.01776  -0.0706   0.1154   1.0000
  13.000   1.6090   0.02418   0.01866  -0.0694   0.1111   1.0000
  13.250   1.6199   0.02527   0.01973  -0.0680   0.1060   1.0000
  13.500   1.6339   0.02615   0.02066  -0.0670   0.1028   1.0000
  13.750   1.6457   0.02721   0.02173  -0.0658   0.0983   1.0000
  14.000   1.6550   0.02849   0.02301  -0.0645   0.0936   1.0000
  14.250   1.6677   0.02953   0.02409  -0.0635   0.0906   1.0000
  14.500   1.6772   0.03085   0.02541  -0.0624   0.0859   1.0000
  14.750   1.6854   0.03231   0.02688  -0.0612   0.0812   1.0000
  15.000   1.6947   0.03371   0.02830  -0.0602   0.0769   1.0000
  15.250   1.7004   0.03544   0.03003  -0.0591   0.0720   1.0000
  15.500   1.7084   0.03702   0.03164  -0.0582   0.0681   1.0000
  15.750   1.7131   0.03893   0.03356  -0.0571   0.0637   1.0000
  16.000   1.7191   0.04079   0.03545  -0.0563   0.0599   1.0000
  16.250   1.7228   0.04289   0.03757  -0.0555   0.0558   1.0000
  16.500   1.7250   0.04521   0.03992  -0.0547   0.0521   1.0000
  16.750   1.7275   0.04758   0.04233  -0.0541   0.0481   1.0000
  17.000   1.7269   0.05034   0.04510  -0.0536   0.0443   1.0000
  17.250   1.7282   0.05297   0.04779  -0.0532   0.0411   1.0000
  17.500   1.7242   0.05629   0.05113  -0.0529   0.0374   1.0000
  17.750   1.7228   0.05941   0.05431  -0.0529   0.0345   1.0000
  18.000   1.7163   0.06328   0.05822  -0.0530   0.0313   1.0000
  18.250   1.7108   0.06715   0.06215  -0.0534   0.0282   1.0000
  18.500   1.7017   0.07163   0.06670  -0.0541   0.0254   1.0000
  18.750   1.6917   0.07642   0.07156  -0.0551   0.0226   1.0000
  19.000   1.6799   0.08163   0.07685  -0.0564   0.0200   1.0000
  19.250   1.6643   0.08757   0.08287  -0.0582   0.0175   1.0000
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