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RONCZ 1082 VOYAGER ROOT OUTER AFT WING AIRFOIL (r1082-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: RONCZ 1082 VOYAGER ROOT OUTER AFT WING AIRFOIL (r1082-il)
Reynolds number: 500,000
Max Cl/Cd: 105.1 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-r1082-il-500000.txt
Download as CSV file: xf-r1082-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RONCZ 1082 VOYAGER ROOT OUTER AFT WING AIRFOIL  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.2345   0.07467   0.07173  -0.1049   0.8071   0.0218
 -13.000  -0.5814   0.05106   0.04762  -0.1068   0.9376   0.0173
 -12.750  -0.5542   0.04395   0.04015  -0.1189   0.9160   0.0170
 -12.500  -0.5458   0.03851   0.03409  -0.1260   0.8650   0.0169
 -12.250  -0.5559   0.03616   0.03131  -0.1237   0.8261   0.0169
 -12.000  -0.5620   0.03410   0.02896  -0.1210   0.8022   0.0168
 -11.750  -0.5651   0.03245   0.02706  -0.1182   0.7839   0.0168
 -11.500  -0.5671   0.03087   0.02520  -0.1152   0.7694   0.0168
 -11.250  -0.5640   0.02921   0.02329  -0.1126   0.7575   0.0167
 -11.000  -0.5607   0.02798   0.02182  -0.1098   0.7467   0.0169
 -10.750  -0.5543   0.02686   0.02047  -0.1072   0.7376   0.0170
 -10.500  -0.5408   0.02552   0.01895  -0.1056   0.7292   0.0170
 -10.250  -0.5293   0.02456   0.01779  -0.1035   0.7220   0.0171
 -10.000  -0.5146   0.02369   0.01676  -0.1019   0.7150   0.0172
  -9.750  -0.4909   0.02221   0.01512  -0.1018   0.7091   0.0174
  -9.500  -0.4683   0.02099   0.01387  -0.1015   0.7036   0.0179
  -9.250  -0.4504   0.02036   0.01319  -0.1003   0.6980   0.0183
  -9.000  -0.4318   0.01968   0.01242  -0.0992   0.6929   0.0187
  -8.750  -0.4135   0.01911   0.01177  -0.0979   0.6882   0.0192
  -8.500  -0.3950   0.01845   0.01107  -0.0967   0.6836   0.0196
  -8.250  -0.3773   0.01786   0.01039  -0.0952   0.6792   0.0199
  -8.000  -0.3599   0.01737   0.00981  -0.0937   0.6754   0.0204
  -7.750  -0.3432   0.01691   0.00928  -0.0920   0.6719   0.0206
  -7.500  -0.3305   0.01626   0.00861  -0.0896   0.6684   0.0212
  -7.250  -0.3159   0.01577   0.00811  -0.0875   0.6651   0.0220
  -7.000  -0.2979   0.01539   0.00769  -0.0860   0.6620   0.0227
  -6.750  -0.2790   0.01504   0.00727  -0.0846   0.6591   0.0238
  -6.500  -0.2596   0.01470   0.00686  -0.0833   0.6562   0.0250
  -6.250  -0.2410   0.01428   0.00646  -0.0819   0.6538   0.0267
  -6.000  -0.2200   0.01398   0.00614  -0.0808   0.6511   0.0295
  -5.750  -0.2002   0.01360   0.00578  -0.0795   0.6485   0.0347
  -5.500  -0.1827   0.01308   0.00538  -0.0779   0.6460   0.0543
  -5.250  -0.1632   0.01269   0.00511  -0.0767   0.6436   0.0808
  -5.000  -0.1413   0.01245   0.00491  -0.0758   0.6412   0.1033
  -4.750  -0.1194   0.01220   0.00475  -0.0750   0.6391   0.1288
  -4.500  -0.0984   0.01188   0.00457  -0.0740   0.6372   0.1612
  -4.250  -0.0783   0.01150   0.00439  -0.0729   0.6353   0.2063
  -4.000  -0.0599   0.01103   0.00420  -0.0716   0.6333   0.2742
  -3.750  -0.0443   0.01040   0.00397  -0.0698   0.6314   0.3726
  -3.500  -0.0316   0.00961   0.00371  -0.0675   0.6296   0.5053
  -3.250  -0.0171   0.00901   0.00369  -0.0650   0.6279   0.6424
  -3.000   0.0080   0.00913   0.00395  -0.0642   0.6262   0.7075
  -2.750   0.0358   0.00932   0.00406  -0.0642   0.6245   0.7296
  -2.500   0.0640   0.00955   0.00424  -0.0642   0.6227   0.7434
  -2.250   0.0913   0.00969   0.00437  -0.0640   0.6211   0.7540
  -2.000   0.1187   0.00985   0.00449  -0.0638   0.6194   0.7640
  -1.750   0.1466   0.01000   0.00465  -0.0637   0.6179   0.7708
  -1.500   0.1744   0.01017   0.00479  -0.0637   0.6163   0.7779
  -1.250   0.2022   0.01029   0.00486  -0.0637   0.6148   0.7845
  -1.000   0.2303   0.01048   0.00506  -0.0635   0.6133   0.7899
  -0.750   0.2579   0.01069   0.00523  -0.0634   0.6119   0.7979
  -0.500   0.2853   0.01090   0.00544  -0.0631   0.6105   0.8044
  -0.250   0.3130   0.01114   0.00567  -0.0629   0.6090   0.8107
   0.000   0.3414   0.01134   0.00579  -0.0632   0.6074   0.8166
   0.250   0.3688   0.01145   0.00591  -0.0631   0.6059   0.8197
   0.500   0.3956   0.01152   0.00601  -0.0629   0.6048   0.8224
   0.750   0.4226   0.01160   0.00609  -0.0629   0.6035   0.8253
   1.000   0.4499   0.01165   0.00615  -0.0630   0.6020   0.8283
   1.250   0.4775   0.01169   0.00618  -0.0632   0.6003   0.8312
   1.500   0.5058   0.01174   0.00621  -0.0637   0.5987   0.8338
   1.750   0.5330   0.01174   0.00621  -0.0637   0.5972   0.8356
   2.000   0.5607   0.01178   0.00625  -0.0639   0.5956   0.8373
   2.250   0.5888   0.01183   0.00629  -0.0641   0.5940   0.8392
   2.500   0.6174   0.01190   0.00635  -0.0645   0.5925   0.8409
   2.750   0.6465   0.01203   0.00645  -0.0651   0.5907   0.8428
   3.000   0.6739   0.01213   0.00657  -0.0653   0.5890   0.8447
   3.250   0.7001   0.01214   0.00662  -0.0653   0.5871   0.8466
   3.500   0.7269   0.01217   0.00668  -0.0655   0.5850   0.8485
   3.750   0.7544   0.01220   0.00673  -0.0658   0.5828   0.8500
   4.000   0.7820   0.01219   0.00674  -0.0660   0.5805   0.8513
   4.250   0.8096   0.01218   0.00673  -0.0662   0.5783   0.8527
   4.500   0.8383   0.01220   0.00675  -0.0666   0.5760   0.8541
   4.750   0.8680   0.01237   0.00690  -0.0673   0.5734   0.8554
   5.000   0.8915   0.01233   0.00695  -0.0667   0.5709   0.8569
   5.250   0.9163   0.01232   0.00700  -0.0664   0.5678   0.8584
   5.500   0.9428   0.01229   0.00701  -0.0664   0.5646   0.8600
   5.750   0.9707   0.01225   0.00696  -0.0667   0.5613   0.8618
   6.000   1.0003   0.01228   0.00696  -0.0673   0.5579   0.8635
   6.250   1.0235   0.01227   0.00703  -0.0667   0.5542   0.8652
   6.500   1.0476   0.01222   0.00704  -0.0663   0.5498   0.8668
   6.750   1.0732   0.01212   0.00697  -0.0661   0.5456   0.8682
   7.000   1.1009   0.01210   0.00693  -0.0663   0.5414   0.8696
   7.250   1.1203   0.01206   0.00701  -0.0649   0.5369   0.8715
   7.500   1.1421   0.01200   0.00702  -0.0639   0.5315   0.8734
   7.750   1.1662   0.01195   0.00698  -0.0634   0.5265   0.8755
   8.000   1.1854   0.01195   0.00708  -0.0620   0.5207   0.8781
   8.250   1.2046   0.01190   0.00710  -0.0605   0.5139   0.8806
   8.500   1.2241   0.01191   0.00714  -0.0592   0.5067   0.8828
   8.750   1.2385   0.01188   0.00718  -0.0568   0.4976   0.8854
   9.000   1.2496   0.01189   0.00726  -0.0538   0.4874   0.8884
   9.250   1.2600   0.01199   0.00740  -0.0507   0.4755   0.8919
   9.500   1.2679   0.01220   0.00763  -0.0472   0.4585   0.8959
   9.750   1.2714   0.01257   0.00795  -0.0432   0.4376   0.9004
  10.000   1.2669   0.01316   0.00848  -0.0379   0.4143   0.9066
  10.250   1.2574   0.01410   0.00932  -0.0323   0.3897   0.9141
  10.500   1.2479   0.01514   0.01034  -0.0271   0.3670   0.9230
  10.750   1.2379   0.01644   0.01160  -0.0223   0.3454   0.9358
  11.000   1.2355   0.01811   0.01325  -0.0198   0.3214   0.9569
  11.250   1.2393   0.02035   0.01541  -0.0199   0.2947   1.0000
  11.500   1.2349   0.02241   0.01739  -0.0178   0.2733   1.0000
  11.750   1.2290   0.02463   0.01953  -0.0156   0.2533   1.0000
  12.000   1.2232   0.02691   0.02173  -0.0136   0.2352   1.0000
  12.250   1.2159   0.02936   0.02408  -0.0116   0.2147   1.0000
  12.500   1.2143   0.03145   0.02612  -0.0101   0.2003   1.0000
  12.750   1.2108   0.03375   0.02835  -0.0086   0.1827   1.0000
  13.000   1.2082   0.03603   0.03056  -0.0073   0.1667   1.0000
  13.250   1.2068   0.03829   0.03275  -0.0061   0.1517   1.0000
  13.500   1.2071   0.04046   0.03486  -0.0051   0.1382   1.0000
  13.750   1.2083   0.04261   0.03695  -0.0042   0.1264   1.0000
  14.000   1.2099   0.04476   0.03907  -0.0035   0.1158   1.0000
  14.250   1.2126   0.04686   0.04113  -0.0028   0.1059   1.0000
  14.500   1.2173   0.04883   0.04310  -0.0023   0.0977   1.0000
  14.750   1.2207   0.05095   0.04520  -0.0018   0.0899   1.0000
  15.000   1.2242   0.05308   0.04731  -0.0014   0.0828   1.0000
  15.250   1.2293   0.05512   0.04937  -0.0011   0.0767   1.0000
  15.500   1.2323   0.05738   0.05162  -0.0008   0.0710   1.0000
  15.750   1.2377   0.05948   0.05374  -0.0006   0.0658   1.0000
  16.000   1.2403   0.06185   0.05611  -0.0005   0.0613   1.0000
  16.250   1.2462   0.06394   0.05824  -0.0004   0.0574   1.0000
  16.500   1.2490   0.06639   0.06071  -0.0004   0.0535   1.0000
  16.750   1.2536   0.06870   0.06305  -0.0005   0.0498   1.0000
  17.000   1.2569   0.07118   0.06557  -0.0006   0.0466   1.0000
  17.250   1.2586   0.07387   0.06828  -0.0008   0.0435   1.0000
  17.500   1.2630   0.07630   0.07077  -0.0011   0.0404   1.0000
  17.750   1.2624   0.07937   0.07385  -0.0014   0.0375   1.0000
  18.000   1.2662   0.08196   0.07651  -0.0018   0.0344   1.0000
  18.250   1.2652   0.08518   0.07974  -0.0024   0.0320   1.0000
  18.500   1.2664   0.08818   0.08281  -0.0030   0.0288   1.0000
  19.000   1.2633   0.09503   0.08976  -0.0046   0.0242   1.0000
  19.250   1.2598   0.09882   0.09359  -0.0056   0.0227   1.0000
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