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RONCZ 1082T VOYAGER TIP OUTER AFT WING AIRFOIL (r1082t-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: RONCZ 1082T VOYAGER TIP OUTER AFT WING AIRFOIL (r1082t-il)
Reynolds number: 1,000,000
Max Cl/Cd: 134.96 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-r1082t-il-1000000.txt
Download as CSV file: xf-r1082t-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RONCZ 1082T VOYAGER TIP OUTER AFT WING AIRFOIL  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.2376   0.08536   0.08309  -0.0860   0.8120   0.0172
 -12.500  -0.2415   0.08106   0.07872  -0.0875   0.7951   0.0173
 -12.250  -0.2462   0.07649   0.07411  -0.0891   0.7815   0.0175
 -11.000  -0.6302   0.02718   0.02248  -0.0990   0.7769   0.0109
 -10.750  -0.6287   0.02601   0.02111  -0.0955   0.7615   0.0109
 -10.500  -0.6256   0.02482   0.01971  -0.0920   0.7486   0.0108
 -10.000  -0.6035   0.02259   0.01711  -0.0876   0.7263   0.0107
  -9.750  -0.5889   0.02157   0.01592  -0.0859   0.7170   0.0107
  -9.500  -0.5730   0.02018   0.01439  -0.0845   0.7082   0.0109
  -9.250  -0.5552   0.01933   0.01344  -0.0833   0.7006   0.0111
  -9.000  -0.5365   0.01855   0.01256  -0.0821   0.6932   0.0113
  -8.750  -0.5173   0.01785   0.01177  -0.0810   0.6867   0.0115
  -8.500  -0.4970   0.01704   0.01087  -0.0800   0.6807   0.0115
  -8.250  -0.4769   0.01635   0.01009  -0.0789   0.6749   0.0115
  -8.000  -0.4564   0.01574   0.00940  -0.0778   0.6699   0.0118
  -7.750  -0.4354   0.01518   0.00878  -0.0769   0.6650   0.0120
  -7.500  -0.4144   0.01468   0.00821  -0.0759   0.6602   0.0123
  -7.250  -0.3931   0.01425   0.00771  -0.0749   0.6557   0.0127
  -7.000  -0.3715   0.01375   0.00716  -0.0740   0.6522   0.0128
  -6.750  -0.3489   0.01339   0.00675  -0.0732   0.6482   0.0131
  -6.500  -0.3265   0.01304   0.00634  -0.0724   0.6443   0.0133
  -6.250  -0.3042   0.01271   0.00595  -0.0715   0.6404   0.0134
  -6.000  -0.2844   0.01209   0.00527  -0.0703   0.6375   0.0139
  -5.750  -0.2619   0.01167   0.00483  -0.0694   0.6346   0.0144
  -5.500  -0.2382   0.01138   0.00452  -0.0688   0.6317   0.0149
  -5.250  -0.2140   0.01113   0.00423  -0.0683   0.6288   0.0154
  -5.000  -0.1896   0.01093   0.00398  -0.0678   0.6259   0.0162
  -4.750  -0.1652   0.01068   0.00369  -0.0672   0.6233   0.0174
  -4.500  -0.1403   0.01043   0.00344  -0.0668   0.6213   0.0189
  -4.250  -0.1147   0.01023   0.00322  -0.0665   0.6191   0.0206
  -4.000  -0.0907   0.00991   0.00298  -0.0659   0.6168   0.0337
  -3.750  -0.0684   0.00947   0.00275  -0.0651   0.6146   0.0815
  -3.500  -0.0443   0.00919   0.00260  -0.0647   0.6123   0.1193
  -3.250  -0.0208   0.00888   0.00246  -0.0641   0.6098   0.1694
  -3.000   0.0020   0.00848   0.00232  -0.0635   0.6077   0.2443
  -2.750   0.0234   0.00791   0.00215  -0.0627   0.6062   0.3499
  -2.500   0.0441   0.00729   0.00197  -0.0618   0.6045   0.4764
  -2.250   0.0649   0.00667   0.00181  -0.0608   0.6028   0.6064
  -2.000   0.0891   0.00644   0.00187  -0.0602   0.6011   0.6979
  -1.750   0.1169   0.00648   0.00193  -0.0601   0.5995   0.7285
  -1.500   0.1450   0.00655   0.00200  -0.0602   0.5978   0.7456
  -1.250   0.1736   0.00664   0.00204  -0.0604   0.5961   0.7547
  -1.000   0.2021   0.00671   0.00208  -0.0606   0.5941   0.7608
  -0.750   0.2308   0.00682   0.00216  -0.0608   0.5921   0.7668
  -0.500   0.2595   0.00688   0.00219  -0.0610   0.5909   0.7728
  -0.250   0.2879   0.00691   0.00225  -0.0611   0.5896   0.7787
   0.000   0.3163   0.00700   0.00235  -0.0613   0.5882   0.7857
   0.250   0.3447   0.00707   0.00240  -0.0614   0.5868   0.7914
   0.500   0.3730   0.00713   0.00248  -0.0615   0.5852   0.7961
   0.750   0.4015   0.00719   0.00253  -0.0617   0.5835   0.7999
   1.000   0.4302   0.00725   0.00257  -0.0620   0.5820   0.8030
   1.250   0.4590   0.00732   0.00262  -0.0624   0.5804   0.8054
   1.500   0.4876   0.00737   0.00264  -0.0627   0.5784   0.8077
   1.750   0.5163   0.00744   0.00272  -0.0630   0.5763   0.8099
   2.000   0.5445   0.00745   0.00275  -0.0632   0.5747   0.8119
   2.250   0.5728   0.00746   0.00279  -0.0634   0.5727   0.8139
   2.500   0.6012   0.00748   0.00282  -0.0637   0.5706   0.8157
   2.750   0.6296   0.00750   0.00284  -0.0640   0.5683   0.8174
   3.000   0.6579   0.00753   0.00286  -0.0642   0.5659   0.8189
   3.250   0.6863   0.00760   0.00291  -0.0646   0.5632   0.8203
   3.500   0.7148   0.00768   0.00298  -0.0649   0.5603   0.8215
   3.750   0.7426   0.00765   0.00299  -0.0651   0.5578   0.8228
   4.000   0.7702   0.00763   0.00301  -0.0652   0.5547   0.8243
   4.250   0.7978   0.00763   0.00303  -0.0653   0.5513   0.8257
   4.500   0.8251   0.00768   0.00307  -0.0654   0.5474   0.8272
   4.750   0.8525   0.00772   0.00314  -0.0655   0.5437   0.8287
   5.000   0.8798   0.00771   0.00318  -0.0655   0.5395   0.8302
   5.250   0.9069   0.00772   0.00321  -0.0656   0.5350   0.8317
   5.500   0.9335   0.00780   0.00328  -0.0656   0.5301   0.8332
   5.750   0.9608   0.00779   0.00334  -0.0656   0.5253   0.8347
   6.000   0.9876   0.00782   0.00339  -0.0656   0.5194   0.8362
   6.250   1.0138   0.00789   0.00347  -0.0655   0.5129   0.8377
   6.500   1.0397   0.00791   0.00352  -0.0653   0.5033   0.8396
   6.750   1.0651   0.00796   0.00361  -0.0651   0.4928   0.8414
   7.000   1.0891   0.00807   0.00371  -0.0646   0.4776   0.8432
   7.250   1.1103   0.00828   0.00386  -0.0635   0.4545   0.8452
   7.500   1.1246   0.00876   0.00416  -0.0612   0.4125   0.8475
   7.750   1.1363   0.00935   0.00458  -0.0585   0.3722   0.8501
   8.000   1.1439   0.01006   0.00508  -0.0551   0.3293   0.8528
   8.250   1.1455   0.01074   0.00557  -0.0505   0.2902   0.8562
   8.500   1.1499   0.01134   0.00606  -0.0465   0.2611   0.8599
   8.750   1.1511   0.01208   0.00666  -0.0420   0.2298   0.8642
   9.000   1.1538   0.01281   0.00727  -0.0381   0.2033   0.8684
   9.250   1.1563   0.01355   0.00794  -0.0342   0.1808   0.8731
   9.500   1.1568   0.01440   0.00872  -0.0303   0.1598   0.8788
   9.750   1.1591   0.01531   0.00957  -0.0269   0.1424   0.8849
  10.000   1.1608   0.01626   0.01051  -0.0236   0.1264   0.8925
  10.250   1.1629   0.01731   0.01154  -0.0206   0.1122   0.9020
  10.500   1.1647   0.01838   0.01263  -0.0177   0.0999   0.9166
  10.750   1.1702   0.01948   0.01380  -0.0157   0.0888   0.9492
  11.000   1.1911   0.02083   0.01514  -0.0173   0.0764   1.0000
  11.250   1.1987   0.02210   0.01639  -0.0160   0.0691   1.0000
  11.500   1.2071   0.02336   0.01764  -0.0148   0.0622   1.0000
  11.750   1.2138   0.02475   0.01900  -0.0135   0.0559   1.0000
  12.000   1.2219   0.02608   0.02034  -0.0124   0.0507   1.0000
  12.250   1.2294   0.02747   0.02172  -0.0113   0.0461   1.0000
  12.500   1.2373   0.02885   0.02311  -0.0103   0.0421   1.0000
  12.750   1.2440   0.03034   0.02460  -0.0093   0.0380   1.0000
  13.000   1.2518   0.03178   0.02606  -0.0084   0.0348   1.0000
  13.250   1.2584   0.03335   0.02763  -0.0075   0.0311   1.0000
  13.500   1.2647   0.03496   0.02924  -0.0066   0.0275   1.0000
  13.750   1.2700   0.03670   0.03098  -0.0058   0.0231   1.0000
  14.000   1.2752   0.03848   0.03277  -0.0050   0.0196   1.0000
  14.250   1.2789   0.04044   0.03472  -0.0043   0.0161   1.0000
  14.500   1.2819   0.04251   0.03680  -0.0036   0.0139   1.0000
  14.750   1.2888   0.04427   0.03861  -0.0031   0.0127   1.0000
  15.000   1.2937   0.04626   0.04063  -0.0026   0.0118   1.0000
  15.250   1.2963   0.04850   0.04291  -0.0021   0.0108   1.0000
  15.500   1.3028   0.05041   0.04490  -0.0018   0.0104   1.0000
  15.750   1.3085   0.05244   0.04698  -0.0016   0.0100   1.0000
  16.000   1.3130   0.05463   0.04923  -0.0014   0.0097   1.0000
  16.250   1.3177   0.05683   0.05149  -0.0013   0.0094   1.0000
  16.500   1.3201   0.05934   0.05404  -0.0013   0.0090   1.0000
  16.750   1.3212   0.06202   0.05680  -0.0013   0.0088   1.0000
  17.000   1.3183   0.06525   0.06012  -0.0014   0.0085   1.0000
  17.250   1.3211   0.06790   0.06283  -0.0016   0.0083   1.0000
  17.500   1.3239   0.07058   0.06560  -0.0020   0.0083   1.0000
  17.750   1.3248   0.07355   0.06865  -0.0024   0.0081   1.0000
  18.000   1.3255   0.07658   0.07177  -0.0029   0.0080   1.0000
  18.250   1.3254   0.07981   0.07508  -0.0036   0.0079   1.0000
  18.500   1.3251   0.08312   0.07847  -0.0044   0.0077   1.0000
  18.750   1.3247   0.08650   0.08193  -0.0053   0.0076   1.0000
  19.000   1.3208   0.09045   0.08597  -0.0064   0.0074   1.0000
  19.250   1.3176   0.09436   0.08997  -0.0076   0.0074   1.0000
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