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DRAGONFLY CANARD (drgnfly-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: DRAGONFLY CANARD (drgnfly-il)
Reynolds number: 1,000,000
Max Cl/Cd: 149.08 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-drgnfly-il-1000000-n5.txt
Download as CSV file: xf-drgnfly-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DRAGONFLY CANARD                                
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.4735   0.04534   0.04120  -0.1394   0.5877   0.0140
 -14.250  -0.5183   0.03758   0.03322  -0.1440   0.5870   0.0140
 -14.000  -0.5381   0.03386   0.02936  -0.1448   0.5860   0.0140
 -13.750  -0.5443   0.03179   0.02718  -0.1443   0.5847   0.0141
 -13.500  -0.5525   0.02987   0.02515  -0.1429   0.5835   0.0142
 -13.250  -0.5550   0.02848   0.02367  -0.1410   0.5828   0.0143
 -13.000  -0.5575   0.02717   0.02226  -0.1385   0.5819   0.0143
 -12.750  -0.5570   0.02608   0.02109  -0.1358   0.5810   0.0144
 -12.500  -0.5553   0.02508   0.01999  -0.1328   0.5798   0.0145
 -12.250  -0.5477   0.02444   0.01929  -0.1303   0.5785   0.0147
 -12.000  -0.5428   0.02375   0.01851  -0.1272   0.5772   0.0148
 -11.750  -0.5372   0.02300   0.01766  -0.1242   0.5760   0.0150
 -11.500  -0.5249   0.02232   0.01687  -0.1222   0.5746   0.0151
 -11.250  -0.5128   0.02151   0.01594  -0.1202   0.5734   0.0153
 -11.000  -0.4985   0.02079   0.01511  -0.1185   0.5721   0.0154
 -10.750  -0.4830   0.02009   0.01429  -0.1168   0.5709   0.0155
 -10.500  -0.4660   0.01946   0.01355  -0.1154   0.5696   0.0157
 -10.250  -0.4480   0.01887   0.01285  -0.1141   0.5683   0.0158
 -10.000  -0.4284   0.01832   0.01222  -0.1130   0.5676   0.0159
  -9.750  -0.4079   0.01784   0.01166  -0.1120   0.5667   0.0160
  -9.500  -0.3883   0.01723   0.01097  -0.1109   0.5658   0.0162
  -9.250  -0.3686   0.01662   0.01029  -0.1098   0.5648   0.0164
  -9.000  -0.3469   0.01618   0.00981  -0.1089   0.5636   0.0166
  -8.750  -0.3242   0.01581   0.00939  -0.1082   0.5624   0.0168
  -8.500  -0.3006   0.01553   0.00907  -0.1076   0.5611   0.0170
  -8.250  -0.2771   0.01520   0.00870  -0.1070   0.5598   0.0172
  -8.000  -0.2532   0.01492   0.00837  -0.1064   0.5585   0.0174
  -7.750  -0.2295   0.01460   0.00800  -0.1058   0.5573   0.0176
  -7.500  -0.2052   0.01434   0.00769  -0.1053   0.5561   0.0179
  -7.250  -0.1809   0.01409   0.00739  -0.1048   0.5549   0.0182
  -7.000  -0.1568   0.01381   0.00706  -0.1043   0.5536   0.0185
  -6.750  -0.1320   0.01354   0.00674  -0.1038   0.5528   0.0189
  -6.500  -0.1074   0.01325   0.00642  -0.1034   0.5520   0.0191
  -6.250  -0.0824   0.01299   0.00612  -0.1030   0.5512   0.0193
  -6.000  -0.0572   0.01276   0.00585  -0.1026   0.5502   0.0195
  -5.750  -0.0327   0.01246   0.00552  -0.1021   0.5492   0.0197
  -5.500  -0.0086   0.01214   0.00518  -0.1015   0.5482   0.0202
  -5.250   0.0166   0.01192   0.00495  -0.1012   0.5471   0.0205
  -5.000   0.0422   0.01173   0.00474  -0.1009   0.5458   0.0208
  -4.750   0.0679   0.01156   0.00454  -0.1006   0.5447   0.0212
  -4.500   0.0936   0.01140   0.00436  -0.1003   0.5434   0.0216
  -4.250   0.1193   0.01125   0.00418  -0.1000   0.5422   0.0221
  -4.000   0.1453   0.01112   0.00403  -0.0997   0.5411   0.0227
  -3.750   0.1713   0.01101   0.00389  -0.0995   0.5399   0.0232
  -3.500   0.1972   0.01091   0.00375  -0.0993   0.5387   0.0235
  -3.250   0.2231   0.01074   0.00358  -0.0990   0.5380   0.0239
  -3.000   0.2489   0.01056   0.00340  -0.0987   0.5372   0.0246
  -2.750   0.2752   0.01043   0.00328  -0.0986   0.5364   0.0252
  -2.500   0.3017   0.01033   0.00318  -0.0985   0.5355   0.0260
  -2.250   0.3283   0.01024   0.00308  -0.0983   0.5345   0.0267
  -2.000   0.3550   0.01015   0.00299  -0.0983   0.5335   0.0275
  -1.750   0.3818   0.01009   0.00292  -0.0982   0.5324   0.0283
  -1.500   0.4080   0.00999   0.00282  -0.0980   0.5312   0.0297
  -1.250   0.4344   0.00991   0.00274  -0.0979   0.5300   0.0312
  -1.000   0.4610   0.00986   0.00269  -0.0978   0.5288   0.0326
  -0.750   0.4875   0.00981   0.00264  -0.0977   0.5277   0.0349
  -0.500   0.5136   0.00976   0.00260  -0.0976   0.5267   0.0400
  -0.250   0.5386   0.00963   0.00257  -0.0972   0.5256   0.0708
   0.000   0.5627   0.00946   0.00255  -0.0967   0.5244   0.1269
   0.250   0.5864   0.00923   0.00254  -0.0962   0.5236   0.2050
   0.500   0.6090   0.00892   0.00254  -0.0955   0.5228   0.3092
   0.750   0.6314   0.00864   0.00254  -0.0948   0.5219   0.4106
   1.000   0.6529   0.00836   0.00259  -0.0938   0.5209   0.5201
   1.250   0.6736   0.00812   0.00264  -0.0926   0.5197   0.6174
   1.500   0.6911   0.00785   0.00270  -0.0906   0.5187   0.7225
   1.750   0.7076   0.00758   0.00277  -0.0883   0.5177   0.8242
   2.000   0.7945   0.00755   0.00301  -0.1014   0.5166   0.9334
   2.250   0.8410   0.00766   0.00309  -0.1058   0.5154   0.9446
   2.750   0.9075   0.00787   0.00326  -0.1087   0.5130   0.9606
   3.250   0.9673   0.00810   0.00344  -0.1103   0.5105   0.9721
   3.500   0.9992   0.00821   0.00353  -0.1115   0.5094   0.9760
   3.750   1.0269   0.00830   0.00363  -0.1118   0.5085   0.9807
   4.000   1.0600   0.00839   0.00373  -0.1133   0.5074   0.9830
   4.250   1.0944   0.00847   0.00382  -0.1152   0.5063   0.9848
   4.500   1.1277   0.00856   0.00391  -0.1168   0.5051   0.9870
   4.750   1.1600   0.00865   0.00401  -0.1182   0.5038   0.9893
   5.000   1.1909   0.00875   0.00412  -0.1193   0.5024   0.9915
   5.250   1.2211   0.00886   0.00423  -0.1203   0.5012   0.9934
   5.500   1.2545   0.00895   0.00433  -0.1220   0.4998   0.9948
   5.750   1.2880   0.00906   0.00443  -0.1237   0.4984   0.9965
   6.000   1.3218   0.00917   0.00455  -0.1256   0.4971   0.9982
   6.250   1.3559   0.00931   0.00468  -0.1275   0.4956   0.9996
   6.500   1.3827   0.00941   0.00482  -0.1278   0.4945   1.0000
   6.750   1.4040   0.00950   0.00495  -0.1269   0.4933   1.0000
   7.000   1.4250   0.00961   0.00509  -0.1260   0.4919   1.0000
   7.250   1.4456   0.00972   0.00524  -0.1250   0.4906   1.0000
   7.500   1.4655   0.00983   0.00539  -0.1239   0.4889   1.0000
   7.750   1.4848   0.00996   0.00554  -0.1226   0.4874   1.0000
   8.000   1.5033   0.01010   0.00571  -0.1212   0.4859   1.0000
   8.250   1.5207   0.01025   0.00588  -0.1196   0.4844   1.0000
   8.500   1.5363   0.01042   0.00607  -0.1177   0.4826   1.0000
   8.750   1.5476   0.01059   0.00625  -0.1148   0.4808   1.0000
   9.000   1.5612   0.01072   0.00644  -0.1125   0.4795   1.0000
   9.250   1.5752   0.01087   0.00664  -0.1102   0.4778   1.0000
   9.500   1.5894   0.01104   0.00687  -0.1081   0.4758   1.0000
   9.750   1.6032   0.01125   0.00712  -0.1060   0.4735   1.0000
  10.000   1.6169   0.01150   0.00740  -0.1040   0.4714   1.0000
  10.250   1.6241   0.01191   0.00781  -0.1009   0.4670   1.0000
  10.500   1.6394   0.01221   0.00819  -0.0994   0.4638   1.0000
  10.750   1.6466   0.01278   0.00878  -0.0968   0.4561   1.0000
  11.000   1.6481   0.01370   0.00971  -0.0937   0.4451   1.0000
  11.250   1.6353   0.01563   0.01160  -0.0895   0.4275   1.0000
  11.500   1.6123   0.01880   0.01472  -0.0852   0.4088   1.0000
  11.750   1.5842   0.02254   0.01842  -0.0810   0.3896   1.0000
  12.000   1.5512   0.02665   0.02250  -0.0764   0.3722   1.0000
  12.250   1.5196   0.03070   0.02651  -0.0721   0.3557   1.0000
  12.500   1.4894   0.03495   0.03071  -0.0683   0.3389   1.0000
  12.750   1.4605   0.03931   0.03499  -0.0649   0.3189   1.0000
  13.000   1.4335   0.04369   0.03929  -0.0618   0.2972   1.0000
  13.250   1.4118   0.04774   0.04326  -0.0593   0.2781   1.0000
  13.500   1.3924   0.05172   0.04714  -0.0570   0.2558   1.0000
  13.750   1.3765   0.05545   0.05077  -0.0550   0.2364   1.0000
  14.000   1.3601   0.05936   0.05459  -0.0532   0.2142   1.0000
  14.250   1.3538   0.06234   0.05750  -0.0520   0.1976   1.0000
  14.500   1.3400   0.06614   0.06120  -0.0505   0.1769   1.0000
  14.750   1.3198   0.07065   0.06553  -0.0489   0.1464   1.0000
  15.000   1.3177   0.07342   0.06824  -0.0481   0.1332   1.0000
  15.250   1.3138   0.07638   0.07113  -0.0474   0.1172   1.0000
  15.500   1.3134   0.07908   0.07381  -0.0468   0.1074   1.0000
  15.750   1.3061   0.08251   0.07711  -0.0460   0.0885   1.0000
  16.000   1.2988   0.08599   0.08051  -0.0454   0.0708   1.0000
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