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NACA 63(2)-615 (naca632615-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(2)-615 (naca632615-il)
Reynolds number: 200,000
Max Cl/Cd: 78.13 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca632615-il-200000-n5.txt
Download as CSV file: xf-naca632615-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(2)-615                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.5911   0.07400   0.06978  -0.0747   1.0000   0.0218
 -13.250  -0.6201   0.06584   0.06149  -0.0801   1.0000   0.0216
 -13.000  -0.6532   0.05820   0.05363  -0.0849   1.0000   0.0216
 -12.750  -0.6768   0.05286   0.04810  -0.0875   1.0000   0.0217
 -12.500  -0.6979   0.04849   0.04354  -0.0887   1.0000   0.0217
 -12.250  -0.7195   0.04480   0.03964  -0.0886   1.0000   0.0219
 -12.000  -0.7401   0.04218   0.03684  -0.0868   1.0000   0.0221
 -11.750  -0.7416   0.04022   0.03482  -0.0868   0.9963   0.0224
 -11.500  -0.7235   0.03808   0.03258  -0.0901   0.9858   0.0228
 -11.250  -0.7056   0.03614   0.03049  -0.0929   0.9748   0.0234
 -11.000  -0.6856   0.03390   0.02803  -0.0956   0.9645   0.0240
 -10.750  -0.6634   0.03177   0.02563  -0.0979   0.9559   0.0248
 -10.500  -0.6398   0.02968   0.02317  -0.0999   0.9478   0.0260
 -10.250  -0.6144   0.02834   0.02170  -0.1014   0.9392   0.0270
 -10.000  -0.5857   0.02722   0.02050  -0.1032   0.9322   0.0279
  -9.750  -0.5596   0.02611   0.01923  -0.1043   0.9237   0.0292
  -9.500  -0.5320   0.02483   0.01772  -0.1054   0.9161   0.0305
  -9.250  -0.5069   0.02373   0.01647  -0.1059   0.9075   0.0316
  -9.000  -0.4805   0.02292   0.01564  -0.1067   0.8995   0.0330
  -8.750  -0.4561   0.02219   0.01481  -0.1068   0.8906   0.0346
  -8.500  -0.4308   0.02140   0.01384  -0.1070   0.8825   0.0363
  -8.250  -0.4079   0.02060   0.01297  -0.1067   0.8740   0.0376
  -8.000  -0.3838   0.01994   0.01228  -0.1067   0.8659   0.0393
  -7.750  -0.3601   0.01937   0.01163  -0.1064   0.8579   0.0413
  -7.500  -0.3358   0.01879   0.01093  -0.1062   0.8501   0.0432
  -7.250  -0.3124   0.01812   0.01023  -0.1060   0.8427   0.0453
  -7.000  -0.2882   0.01761   0.00968  -0.1059   0.8349   0.0477
  -6.750  -0.2626   0.01713   0.00909  -0.1058   0.8285   0.0503
  -6.500  -0.2386   0.01659   0.00852  -0.1056   0.8206   0.0530
  -6.250  -0.2127   0.01613   0.00800  -0.1057   0.8141   0.0564
  -6.000  -0.1868   0.01574   0.00752  -0.1057   0.8072   0.0601
  -5.750  -0.1609   0.01525   0.00703  -0.1058   0.8002   0.0652
  -5.500  -0.1337   0.01487   0.00657  -0.1060   0.7943   0.0719
  -5.250  -0.1074   0.01447   0.00618  -0.1061   0.7870   0.0818
  -5.000  -0.0802   0.01402   0.00577  -0.1064   0.7807   0.0999
  -4.750  -0.0530   0.01353   0.00540  -0.1068   0.7745   0.1353
  -4.500  -0.0257   0.01297   0.00504  -0.1074   0.7678   0.1903
  -4.250   0.0023   0.01229   0.00468  -0.1082   0.7621   0.2789
  -4.000   0.0303   0.01179   0.00453  -0.1089   0.7555   0.3725
  -3.750   0.0587   0.01160   0.00446  -0.1092   0.7492   0.4286
  -3.250   0.1158   0.01150   0.00442  -0.1095   0.7371   0.4997
  -3.000   0.1442   0.01151   0.00443  -0.1095   0.7310   0.5274
  -2.750   0.1728   0.01154   0.00443  -0.1095   0.7257   0.5472
  -2.500   0.2010   0.01157   0.00445  -0.1095   0.7192   0.5626
  -2.250   0.2295   0.01161   0.00444  -0.1096   0.7134   0.5773
  -2.000   0.2583   0.01164   0.00440  -0.1097   0.7077   0.5887
  -1.750   0.2863   0.01165   0.00441  -0.1097   0.7014   0.5962
  -1.500   0.3152   0.01168   0.00436  -0.1098   0.6960   0.6047
  -1.250   0.3435   0.01170   0.00435  -0.1099   0.6903   0.6117
  -1.000   0.3718   0.01173   0.00436  -0.1100   0.6840   0.6188
  -0.750   0.4008   0.01176   0.00432  -0.1102   0.6787   0.6263
  -0.500   0.4287   0.01179   0.00437  -0.1102   0.6732   0.6321
  -0.250   0.4572   0.01184   0.00439  -0.1103   0.6670   0.6392
   0.000   0.4857   0.01188   0.00439  -0.1105   0.6618   0.6457
   0.250   0.5137   0.01193   0.00446  -0.1105   0.6562   0.6517
   0.500   0.5422   0.01199   0.00450  -0.1107   0.6503   0.6591
   0.750   0.5703   0.01205   0.00455  -0.1107   0.6451   0.6651
   1.000   0.5983   0.01212   0.00464  -0.1107   0.6394   0.6717
   1.250   0.6267   0.01220   0.00472  -0.1109   0.6336   0.6788
   1.500   0.6544   0.01227   0.00480  -0.1108   0.6286   0.6848
   1.750   0.6823   0.01236   0.00492  -0.1109   0.6229   0.6922
   2.000   0.7100   0.01245   0.00504  -0.1109   0.6170   0.6987
   2.250   0.7378   0.01254   0.00513  -0.1109   0.6119   0.7055
   2.500   0.7657   0.01265   0.00528  -0.1110   0.6060   0.7133
   2.750   0.7925   0.01274   0.00544  -0.1108   0.5999   0.7197
   3.000   0.8205   0.01286   0.00555  -0.1108   0.5947   0.7272
   3.250   0.8472   0.01297   0.00575  -0.1107   0.5882   0.7341
   3.500   0.8740   0.01308   0.00591  -0.1105   0.5821   0.7418
   3.750   0.9014   0.01321   0.00606  -0.1104   0.5766   0.7493
   4.000   0.9272   0.01334   0.00629  -0.1101   0.5697   0.7566
   4.250   0.9544   0.01347   0.00645  -0.1100   0.5633   0.7650
   4.500   0.9796   0.01360   0.00667  -0.1095   0.5555   0.7723
   4.750   1.0059   0.01373   0.00682  -0.1092   0.5467   0.7811
   5.000   1.0300   0.01385   0.00705  -0.1085   0.5369   0.7886
   5.250   1.0556   0.01401   0.00722  -0.1082   0.5275   0.7978
   5.500   1.0789   0.01414   0.00745  -0.1073   0.5163   0.8058
   5.750   1.1028   0.01431   0.00767  -0.1066   0.5040   0.8153
   6.000   1.1249   0.01447   0.00790  -0.1055   0.4907   0.8244
   6.250   1.1462   0.01467   0.00812  -0.1043   0.4731   0.8344
   6.500   1.1649   0.01494   0.00835  -0.1027   0.4493   0.8453
   6.750   1.1814   0.01526   0.00863  -0.1007   0.4210   0.8565
   7.000   1.1968   0.01565   0.00898  -0.0986   0.3930   0.8693
   7.250   1.2094   0.01611   0.00938  -0.0960   0.3637   0.8844
   7.500   1.2175   0.01668   0.00984  -0.0927   0.3306   0.9044
   7.750   1.2205   0.01731   0.01036  -0.0885   0.2975   0.9382
   8.000   1.2252   0.01819   0.01109  -0.0853   0.2619   1.0000
   8.250   1.2303   0.01938   0.01208  -0.0826   0.2265   1.0000
   8.500   1.2351   0.02066   0.01319  -0.0800   0.1949   1.0000
   9.000   1.2451   0.02342   0.01568  -0.0755   0.1421   1.0000
   9.250   1.2503   0.02490   0.01708  -0.0735   0.1212   1.0000
   9.500   1.2558   0.02644   0.01854  -0.0718   0.1027   1.0000
   9.750   1.2612   0.02806   0.02010  -0.0701   0.0876   1.0000
  10.000   1.2666   0.02975   0.02174  -0.0686   0.0754   1.0000
  10.250   1.2726   0.03146   0.02344  -0.0673   0.0659   1.0000
  10.500   1.2788   0.03321   0.02520  -0.0661   0.0589   1.0000
  10.750   1.2839   0.03511   0.02710  -0.0650   0.0532   1.0000
  11.000   1.2906   0.03692   0.02895  -0.0641   0.0485   1.0000
  11.250   1.2958   0.03892   0.03098  -0.0632   0.0450   1.0000
  11.500   1.3026   0.04083   0.03296  -0.0624   0.0419   1.0000
  11.750   1.3069   0.04301   0.03517  -0.0617   0.0395   1.0000
  12.000   1.3123   0.04516   0.03741  -0.0611   0.0375   1.0000
  12.250   1.3181   0.04731   0.03965  -0.0606   0.0356   1.0000
  12.500   1.3222   0.04969   0.04209  -0.0602   0.0339   1.0000
  12.750   1.3244   0.05237   0.04482  -0.0599   0.0325   1.0000
  13.000   1.3298   0.05475   0.04731  -0.0597   0.0311   1.0000
  13.250   1.3341   0.05731   0.04997  -0.0595   0.0299   1.0000
  13.500   1.3373   0.06005   0.05280  -0.0595   0.0288   1.0000
  13.750   1.3390   0.06305   0.05587  -0.0596   0.0278   1.0000
  14.000   1.3405   0.06613   0.05902  -0.0597   0.0270   1.0000
  14.250   1.3443   0.06899   0.06202  -0.0599   0.0260   1.0000
  14.500   1.3473   0.07201   0.06514  -0.0602   0.0251   1.0000
  14.750   1.3498   0.07514   0.06836  -0.0606   0.0244   1.0000
  15.000   1.3518   0.07839   0.07170  -0.0612   0.0237   1.0000
  15.250   1.3526   0.08184   0.07521  -0.0618   0.0231   1.0000
  15.500   1.3541   0.08523   0.07869  -0.0624   0.0225   1.0000
  15.750   1.3571   0.08849   0.08210  -0.0631   0.0218   1.0000
  16.000   1.3595   0.09188   0.08561  -0.0639   0.0212   1.0000
  16.250   1.3615   0.09537   0.08922  -0.0648   0.0206   1.0000
  16.500   1.3629   0.09898   0.09293  -0.0659   0.0200   1.0000
  16.750   1.3640   0.10266   0.09670  -0.0671   0.0196   1.0000
  17.000   1.3648   0.10644   0.10056  -0.0685   0.0192   1.0000
  17.250   1.3657   0.11014   0.10431  -0.0698   0.0189   1.0000
  17.500   1.3666   0.11396   0.10829  -0.0712   0.0185   1.0000
  17.750   1.3666   0.11798   0.11248  -0.0727   0.0182   1.0000
  18.000   1.3661   0.12211   0.11677  -0.0745   0.0179   1.0000
  18.250   1.3649   0.12642   0.12124  -0.0764   0.0176   1.0000
  18.500   1.3631   0.13091   0.12589  -0.0786   0.0173   1.0000
  18.750   1.3606   0.13558   0.13070  -0.0810   0.0171   1.0000
  19.000   1.3576   0.14040   0.13568  -0.0837   0.0169   1.0000
  19.250   1.3539   0.14544   0.14087  -0.0866   0.0167   1.0000
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