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SM701 (sm701-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: SM701 (sm701-il)
Reynolds number: 500,000
Max Cl/Cd: 79.64 at α=2°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sm701-il-500000-n5.txt
Download as CSV file: xf-sm701-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.5842   0.07944   0.07657  -0.0782   0.9962   0.0124
 -14.000  -0.6373   0.06347   0.06022  -0.0911   0.9945   0.0122
 -13.750  -0.6530   0.05662   0.05316  -0.0969   0.9928   0.0123
 -13.500  -0.6661   0.05097   0.04730  -0.1012   0.9902   0.0123
 -13.250  -0.6736   0.04612   0.04223  -0.1052   0.9876   0.0124
 -13.000  -0.6706   0.04255   0.03847  -0.1086   0.9854   0.0126
 -12.750  -0.6651   0.03912   0.03482  -0.1120   0.9836   0.0127
 -12.500  -0.6623   0.03652   0.03204  -0.1132   0.9798   0.0130
 -12.250  -0.6551   0.03405   0.02939  -0.1146   0.9760   0.0131
 -12.000  -0.6412   0.03184   0.02698  -0.1166   0.9733   0.0133
 -11.750  -0.6223   0.02987   0.02482  -0.1190   0.9714   0.0134
 -11.500  -0.6140   0.02847   0.02330  -0.1182   0.9650   0.0135
 -11.250  -0.5951   0.02704   0.02170  -0.1193   0.9612   0.0137
 -11.000  -0.5719   0.02553   0.02005  -0.1211   0.9588   0.0139
 -10.750  -0.5623   0.02438   0.01884  -0.1196   0.9513   0.0141
 -10.500  -0.5427   0.02332   0.01773  -0.1199   0.9462   0.0144
 -10.250  -0.5293   0.02252   0.01689  -0.1187   0.9384   0.0146
 -10.000  -0.5101   0.02164   0.01594  -0.1184   0.9313   0.0149
  -9.750  -0.4916   0.02084   0.01506  -0.1177   0.9230   0.0151
  -9.500  -0.4665   0.02000   0.01415  -0.1182   0.9162   0.0154
  -9.250  -0.4429   0.01920   0.01326  -0.1183   0.9078   0.0156
  -9.000  -0.4146   0.01839   0.01237  -0.1192   0.9007   0.0159
  -8.750  -0.3886   0.01769   0.01158  -0.1196   0.8916   0.0162
  -8.500  -0.3606   0.01698   0.01077  -0.1204   0.8832   0.0165
  -8.250  -0.3356   0.01640   0.01010  -0.1205   0.8730   0.0168
  -8.000  -0.3105   0.01588   0.00948  -0.1205   0.8635   0.0170
  -7.750  -0.2872   0.01530   0.00881  -0.1203   0.8537   0.0174
  -7.500  -0.2657   0.01474   0.00820  -0.1197   0.8440   0.0178
  -7.250  -0.2419   0.01431   0.00771  -0.1195   0.8359   0.0183
  -7.000  -0.2188   0.01393   0.00729  -0.1190   0.8281   0.0189
  -6.750  -0.1945   0.01357   0.00685  -0.1187   0.8212   0.0193
  -6.500  -0.1705   0.01321   0.00645  -0.1184   0.8148   0.0198
  -6.250  -0.1458   0.01289   0.00607  -0.1181   0.8082   0.0203
  -6.000  -0.1203   0.01261   0.00571  -0.1179   0.8025   0.0208
  -5.750  -0.0954   0.01228   0.00535  -0.1176   0.7967   0.0213
  -5.500  -0.0698   0.01197   0.00501  -0.1175   0.7914   0.0221
  -5.250  -0.0431   0.01173   0.00472  -0.1175   0.7869   0.0230
  -5.000  -0.0168   0.01151   0.00447  -0.1174   0.7819   0.0243
  -4.750   0.0099   0.01129   0.00422  -0.1174   0.7769   0.0260
  -4.500   0.0370   0.01108   0.00399  -0.1175   0.7726   0.0288
  -4.250   0.0643   0.01085   0.00377  -0.1176   0.7685   0.0349
  -4.000   0.0910   0.01054   0.00356  -0.1177   0.7637   0.0566
  -3.500   0.1457   0.00999   0.00318  -0.1181   0.7539   0.1199
  -3.250   0.1724   0.00954   0.00297  -0.1184   0.7480   0.1845
  -3.000   0.1996   0.00893   0.00270  -0.1190   0.7416   0.2907
  -2.750   0.2276   0.00820   0.00247  -0.1199   0.7353   0.4420
  -2.500   0.2557   0.00807   0.00247  -0.1201   0.7282   0.4975
  -2.250   0.2840   0.00807   0.00246  -0.1201   0.7217   0.5246
  -2.000   0.3124   0.00807   0.00249  -0.1202   0.7156   0.5500
  -1.750   0.3407   0.00812   0.00254  -0.1203   0.7094   0.5705
  -1.500   0.3690   0.00819   0.00259  -0.1203   0.7038   0.5877
  -1.250   0.3970   0.00821   0.00262  -0.1203   0.6976   0.5957
  -1.000   0.4252   0.00825   0.00260  -0.1203   0.6911   0.5988
  -0.750   0.4534   0.00828   0.00257  -0.1204   0.6849   0.6016
  -0.500   0.4813   0.00830   0.00256  -0.1204   0.6777   0.6040
  -0.250   0.5088   0.00833   0.00256  -0.1203   0.6707   0.6066
   0.000   0.5364   0.00835   0.00257  -0.1202   0.6623   0.6094
   0.250   0.5636   0.00841   0.00258  -0.1201   0.6536   0.6121
   0.500   0.5907   0.00845   0.00259  -0.1199   0.6434   0.6148
   0.750   0.6175   0.00851   0.00261  -0.1197   0.6321   0.6177
   1.000   0.6436   0.00859   0.00263  -0.1194   0.6184   0.6206
   1.250   0.6688   0.00867   0.00267  -0.1188   0.6017   0.6233
   1.500   0.6930   0.00880   0.00272  -0.1181   0.5804   0.6261
   1.750   0.7156   0.00899   0.00280  -0.1171   0.5548   0.6291
   2.000   0.7367   0.00925   0.00291  -0.1158   0.5254   0.6322
   2.250   0.7579   0.00954   0.00305  -0.1146   0.4977   0.6353
   2.500   0.7794   0.00982   0.00321  -0.1134   0.4727   0.6383
   2.750   0.8005   0.01010   0.00340  -0.1122   0.4482   0.6415
   3.000   0.8219   0.01039   0.00358  -0.1111   0.4265   0.6451
   3.250   0.8436   0.01066   0.00378  -0.1100   0.4065   0.6488
   3.500   0.8652   0.01093   0.00396  -0.1089   0.3884   0.6523
   3.750   0.8859   0.01119   0.00415  -0.1077   0.3713   0.6557
   4.000   0.9059   0.01145   0.00436  -0.1063   0.3550   0.6592
   4.250   0.9264   0.01170   0.00457  -0.1050   0.3413   0.6631
   4.500   0.9469   0.01197   0.00479  -0.1038   0.3288   0.6675
   5.000   0.9882   0.01253   0.00529  -0.1014   0.3034   0.6762
   5.250   1.0091   0.01281   0.00556  -0.1003   0.2932   0.6809
   5.750   1.0504   0.01341   0.00611  -0.0980   0.2729   0.6903
   6.000   1.0704   0.01373   0.00642  -0.0968   0.2635   0.6952
   6.250   1.0909   0.01403   0.00672  -0.0957   0.2545   0.7007
   6.750   1.1308   0.01469   0.00738  -0.0933   0.2387   0.7117
   7.000   1.1503   0.01504   0.00774  -0.0921   0.2312   0.7183
   7.250   1.1701   0.01540   0.00810  -0.0910   0.2238   0.7246
   7.500   1.1888   0.01578   0.00851  -0.0897   0.2176   0.7315
   7.750   1.2084   0.01614   0.00889  -0.0886   0.2111   0.7385
   8.250   1.2453   0.01697   0.00977  -0.0860   0.1988   0.7532
   8.500   1.2635   0.01740   0.01024  -0.0848   0.1933   0.7608
   8.750   1.2806   0.01789   0.01076  -0.0834   0.1881   0.7696
   9.000   1.2989   0.01832   0.01124  -0.0822   0.1830   0.7788
   9.250   1.3159   0.01884   0.01179  -0.0809   0.1776   0.7892
   9.500   1.3319   0.01938   0.01239  -0.0794   0.1732   0.8001
   9.750   1.3494   0.01986   0.01295  -0.0782   0.1690   0.8116
  10.000   1.3652   0.02044   0.01357  -0.0768   0.1641   0.8243
  10.500   1.3950   0.02163   0.01492  -0.0738   0.1561   0.8560
  10.750   1.4083   0.02221   0.01559  -0.0720   0.1518   0.8797
  11.000   1.4157   0.02276   0.01626  -0.0691   0.1480   0.9428
  11.250   1.4299   0.02350   0.01704  -0.0678   0.1442   1.0000
  11.500   1.4461   0.02424   0.01783  -0.0669   0.1405   1.0000
  11.750   1.4608   0.02509   0.01870  -0.0659   0.1361   1.0000
  12.000   1.4732   0.02611   0.01972  -0.0646   0.1318   1.0000
  12.250   1.4886   0.02695   0.02061  -0.0637   0.1285   1.0000
  12.500   1.5019   0.02794   0.02163  -0.0627   0.1233   1.0000
  12.750   1.5124   0.02916   0.02284  -0.0615   0.1184   1.0000
  13.000   1.5263   0.03015   0.02388  -0.0607   0.1143   1.0000
  13.250   1.5370   0.03140   0.02515  -0.0596   0.1086   1.0000
  13.500   1.5473   0.03271   0.02648  -0.0586   0.1044   1.0000
  13.750   1.5586   0.03397   0.02779  -0.0577   0.0997   1.0000
  14.000   1.5671   0.03549   0.02932  -0.0568   0.0951   1.0000
  14.250   1.5768   0.03695   0.03082  -0.0559   0.0914   1.0000
  14.500   1.5855   0.03851   0.03242  -0.0551   0.0868   1.0000
  14.750   1.5913   0.04039   0.03431  -0.0542   0.0823   1.0000
  15.000   1.5999   0.04205   0.03603  -0.0536   0.0785   1.0000
  15.250   1.6052   0.04405   0.03805  -0.0529   0.0739   1.0000
  15.500   1.6099   0.04617   0.04022  -0.0522   0.0701   1.0000
  15.750   1.6150   0.04830   0.04241  -0.0517   0.0662   1.0000
  16.000   1.6167   0.05085   0.04499  -0.0513   0.0621   1.0000
  16.250   1.6198   0.05331   0.04750  -0.0510   0.0581   1.0000
  16.500   1.6198   0.05620   0.05044  -0.0507   0.0541   1.0000
  16.750   1.6194   0.05922   0.05352  -0.0507   0.0504   1.0000
  17.000   1.6176   0.06252   0.05687  -0.0508   0.0466   1.0000
  17.250   1.6149   0.06602   0.06043  -0.0511   0.0438   1.0000
  17.500   1.6119   0.06967   0.06418  -0.0516   0.0407   1.0000
  17.750   1.6059   0.07386   0.06843  -0.0524   0.0380   1.0000
  18.000   1.6010   0.07801   0.07268  -0.0533   0.0357   1.0000
  18.250   1.5931   0.08272   0.07748  -0.0546   0.0331   1.0000
  18.500   1.5834   0.08782   0.08267  -0.0562   0.0311   1.0000
  18.750   1.5748   0.09287   0.08783  -0.0579   0.0292   1.0000
  19.000   1.5626   0.09863   0.09369  -0.0601   0.0271   1.0000
  19.250   1.5506   0.10443   0.09961  -0.0624   0.0256   1.0000
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