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SM701 (sm701-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: SM701 (sm701-il)
Reynolds number: 200,000
Max Cl/Cd: 64.37 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sm701-il-200000-n5.txt
Download as CSV file: xf-sm701-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.5078   0.06842   0.06440  -0.0819   0.9929   0.0199
 -11.500  -0.5323   0.05962   0.05531  -0.0903   0.9874   0.0198
 -11.250  -0.5504   0.05254   0.04788  -0.0974   0.9821   0.0199
 -11.000  -0.5630   0.04763   0.04264  -0.1010   0.9739   0.0202
 -10.750  -0.5715   0.04382   0.03849  -0.1029   0.9651   0.0203
 -10.500  -0.5726   0.04034   0.03460  -0.1047   0.9577   0.0206
 -10.250  -0.5723   0.03778   0.03170  -0.1037   0.9466   0.0208
 -10.000  -0.5633   0.03544   0.02900  -0.1034   0.9387   0.0210
  -9.750  -0.5468   0.03334   0.02674  -0.1035   0.9325   0.0212
  -9.500  -0.5221   0.03154   0.02479  -0.1048   0.9295   0.0215
  -9.250  -0.5093   0.03026   0.02339  -0.1032   0.9204   0.0218
  -9.000  -0.4842   0.02880   0.02178  -0.1040   0.9166   0.0221
  -8.750  -0.4602   0.02750   0.02034  -0.1042   0.9120   0.0226
  -8.500  -0.4401   0.02635   0.01906  -0.1035   0.9049   0.0230
  -8.250  -0.4107   0.02522   0.01779  -0.1046   0.9016   0.0238
  -8.000  -0.3814   0.02415   0.01656  -0.1055   0.8980   0.0247
  -7.750  -0.3597   0.02332   0.01559  -0.1048   0.8910   0.0252
  -7.500  -0.3309   0.02220   0.01445  -0.1056   0.8874   0.0258
  -7.250  -0.2995   0.02122   0.01346  -0.1069   0.8846   0.0264
  -7.000  -0.2777   0.02051   0.01273  -0.1063   0.8775   0.0270
  -6.750  -0.2495   0.01973   0.01190  -0.1069   0.8728   0.0278
  -6.500  -0.2176   0.01895   0.01105  -0.1083   0.8695   0.0287
  -6.250  -0.1932   0.01837   0.01040  -0.1081   0.8635   0.0298
  -6.000  -0.1669   0.01773   0.00974  -0.1084   0.8582   0.0312
  -5.750  -0.1358   0.01713   0.00909  -0.1096   0.8545   0.0330
  -5.500  -0.1080   0.01663   0.00853  -0.1101   0.8495   0.0350
  -5.250  -0.0828   0.01617   0.00803  -0.1100   0.8434   0.0370
  -5.000  -0.0529   0.01569   0.00751  -0.1108   0.8393   0.0408
  -4.750  -0.0218   0.01520   0.00701  -0.1118   0.8358   0.0486
  -4.500   0.0010   0.01477   0.00668  -0.1113   0.8295   0.0675
  -4.250   0.0284   0.01423   0.00630  -0.1119   0.8246   0.1069
  -4.000   0.0588   0.01366   0.00590  -0.1130   0.8209   0.1611
  -3.750   0.0839   0.01297   0.00557  -0.1134   0.8159   0.2505
  -3.500   0.1084   0.01194   0.00546  -0.1140   0.8105   0.4639
  -3.250   0.1385   0.01195   0.00556  -0.1144   0.8063   0.5320
  -3.000   0.1693   0.01204   0.00562  -0.1148   0.8022   0.5625
  -2.750   0.1952   0.01215   0.00570  -0.1143   0.7962   0.5815
  -2.500   0.2242   0.01225   0.00575  -0.1143   0.7910   0.5966
  -2.250   0.2550   0.01241   0.00585  -0.1145   0.7865   0.6157
  -2.000   0.2789   0.01259   0.00606  -0.1134   0.7793   0.6297
  -1.750   0.3092   0.01259   0.00592  -0.1139   0.7733   0.6367
  -1.500   0.3372   0.01257   0.00584  -0.1138   0.7667   0.6397
  -1.250   0.3642   0.01256   0.00579  -0.1136   0.7593   0.6428
  -1.000   0.3947   0.01253   0.00567  -0.1140   0.7532   0.6461
  -0.750   0.4204   0.01253   0.00563  -0.1136   0.7456   0.6495
  -0.500   0.4504   0.01251   0.00551  -0.1141   0.7393   0.6533
  -0.250   0.4770   0.01252   0.00549  -0.1138   0.7322   0.6563
   0.000   0.5043   0.01252   0.00547  -0.1137   0.7250   0.6589
   0.250   0.5322   0.01253   0.00544  -0.1137   0.7180   0.6618
   0.500   0.5586   0.01254   0.00543  -0.1134   0.7098   0.6654
   0.750   0.5871   0.01255   0.00538  -0.1135   0.7022   0.6694
   1.000   0.6131   0.01257   0.00538  -0.1132   0.6932   0.6727
   1.250   0.6396   0.01259   0.00539  -0.1128   0.6843   0.6754
   1.500   0.6657   0.01261   0.00540  -0.1124   0.6744   0.6786
   1.750   0.6909   0.01265   0.00544  -0.1119   0.6637   0.6823
   2.000   0.7171   0.01269   0.00543  -0.1116   0.6522   0.6866
   2.250   0.7423   0.01274   0.00545  -0.1110   0.6393   0.6903
   2.500   0.7659   0.01279   0.00551  -0.1102   0.6240   0.6936
   2.750   0.7896   0.01286   0.00555  -0.1093   0.6071   0.6974
   3.000   0.8127   0.01296   0.00560  -0.1084   0.5862   0.7017
   3.250   0.8352   0.01311   0.00564  -0.1074   0.5622   0.7061
   3.500   0.8552   0.01330   0.00574  -0.1058   0.5362   0.7098
   3.750   0.8741   0.01358   0.00588  -0.1041   0.5103   0.7144
   4.000   0.8931   0.01389   0.00607  -0.1025   0.4850   0.7196
   4.250   0.9107   0.01424   0.00630  -0.1007   0.4616   0.7243
   4.500   0.9279   0.01458   0.00657  -0.0988   0.4399   0.7287
   4.750   0.9444   0.01492   0.00684  -0.0969   0.4203   0.7340
   5.000   0.9613   0.01529   0.00713  -0.0950   0.4023   0.7398
   5.250   0.9771   0.01566   0.00747  -0.0930   0.3854   0.7448
   5.500   0.9940   0.01606   0.00783  -0.0912   0.3695   0.7511
   5.750   1.0115   0.01647   0.00820  -0.0895   0.3552   0.7577
   6.000   1.0282   0.01688   0.00861  -0.0878   0.3424   0.7639
   6.250   1.0451   0.01733   0.00902  -0.0861   0.3297   0.7714
   6.500   1.0621   0.01775   0.00945  -0.0845   0.3176   0.7780
   6.750   1.0794   0.01818   0.00989  -0.0829   0.3066   0.7859
   7.000   1.0956   0.01866   0.01037  -0.0813   0.2968   0.7937
   7.250   1.1126   0.01910   0.01084  -0.0797   0.2866   0.8029
   7.500   1.1286   0.01958   0.01135  -0.0780   0.2774   0.8125
   7.750   1.1444   0.02010   0.01188  -0.0764   0.2686   0.8234
   8.000   1.1603   0.02057   0.01241  -0.0747   0.2608   0.8351
   8.250   1.1745   0.02111   0.01297  -0.0729   0.2528   0.8481
   8.500   1.1891   0.02160   0.01353  -0.0710   0.2458   0.8633
   8.750   1.2016   0.02212   0.01411  -0.0688   0.2386   0.8834
   9.250   1.2250   0.02302   0.01516  -0.0644   0.2263   1.0000
   9.500   1.2409   0.02383   0.01594  -0.0634   0.2199   1.0000
   9.750   1.2592   0.02451   0.01667  -0.0627   0.2136   1.0000
  10.000   1.2754   0.02530   0.01747  -0.0618   0.2077   1.0000
  10.250   1.2906   0.02617   0.01834  -0.0608   0.2026   1.0000
  10.500   1.3077   0.02693   0.01917  -0.0601   0.1970   1.0000
  10.750   1.3218   0.02786   0.02012  -0.0590   0.1915   1.0000
  11.000   1.3363   0.02880   0.02108  -0.0581   0.1869   1.0000
  11.250   1.3521   0.02968   0.02204  -0.0572   0.1821   1.0000
  11.500   1.3651   0.03072   0.02311  -0.0562   0.1771   1.0000
  11.750   1.3775   0.03184   0.02425  -0.0552   0.1730   1.0000
  12.000   1.3924   0.03281   0.02533  -0.0545   0.1682   1.0000
  12.250   1.4046   0.03397   0.02653  -0.0535   0.1638   1.0000
  12.500   1.4144   0.03532   0.02789  -0.0525   0.1598   1.0000
  12.750   1.4281   0.03643   0.02911  -0.0518   0.1557   1.0000
  13.000   1.4396   0.03770   0.03048  -0.0510   0.1513   1.0000
  13.250   1.4488   0.03917   0.03199  -0.0501   0.1475   1.0000
  13.500   1.4583   0.04067   0.03355  -0.0493   0.1438   1.0000
  13.750   1.4694   0.04206   0.03507  -0.0486   0.1395   1.0000
  14.000   1.4779   0.04370   0.03678  -0.0479   0.1357   1.0000
  14.250   1.4834   0.04563   0.03872  -0.0472   0.1321   1.0000
  14.500   1.4930   0.04726   0.04050  -0.0467   0.1284   1.0000
  14.750   1.5006   0.04909   0.04245  -0.0462   0.1245   1.0000
  15.000   1.5053   0.05124   0.04466  -0.0458   0.1209   1.0000
  15.250   1.5090   0.05354   0.04701  -0.0454   0.1177   1.0000
  15.500   1.5162   0.05558   0.04920  -0.0451   0.1139   1.0000
  15.750   1.5199   0.05802   0.05175  -0.0450   0.1101   1.0000
  16.000   1.5203   0.06087   0.05465  -0.0449   0.1068   1.0000
  16.250   1.5231   0.06355   0.05746  -0.0450   0.1034   1.0000
  16.500   1.5254   0.06637   0.06042  -0.0452   0.0995   1.0000
  16.750   1.5233   0.06980   0.06392  -0.0457   0.0957   1.0000
  17.000   1.5208   0.07339   0.06759  -0.0463   0.0924   1.0000
  17.250   1.5208   0.07677   0.07113  -0.0470   0.0885   1.0000
  17.500   1.5162   0.08086   0.07532  -0.0481   0.0849   1.0000
  17.750   1.5089   0.08545   0.07996  -0.0495   0.0819   1.0000
  18.000   1.5061   0.08950   0.08418  -0.0508   0.0782   1.0000
  18.250   1.4987   0.09433   0.08913  -0.0525   0.0748   1.0000
  18.500   1.4880   0.09979   0.09466  -0.0547   0.0720   1.0000
  18.750   1.4811   0.10471   0.09973  -0.0568   0.0689   1.0000
  19.000   1.4718   0.11015   0.10531  -0.0592   0.0658   1.0000
  19.250   1.4592   0.11621   0.11148  -0.0621   0.0631   1.0000
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