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US1000ROOT (us1000root-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: US1000ROOT (us1000root-il)
Reynolds number: 200,000
Max Cl/Cd: 49.15 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-us1000root-il-200000.txt
Download as CSV file: xf-us1000root-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: US1000ROOT                                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.7853   0.16282   0.15870   0.0012   1.0000   0.0162
 -19.250  -0.8015   0.15461   0.15035  -0.0036   1.0000   0.0159
 -19.000  -0.8138   0.14769   0.14330  -0.0076   1.0000   0.0155
 -18.750  -0.8295   0.14018   0.13564  -0.0119   1.0000   0.0152
 -18.500  -0.8447   0.13301   0.12829  -0.0157   1.0000   0.0149
 -18.250  -0.8585   0.12632   0.12142  -0.0192   1.0000   0.0145
 -18.000  -0.8677   0.12069   0.11562  -0.0220   1.0000   0.0143
 -17.750  -0.8788   0.11481   0.10952  -0.0247   1.0000   0.0138
 -17.500  -0.8877   0.10941   0.10388  -0.0269   1.0000   0.0134
 -17.250  -0.8880   0.10570   0.10003  -0.0281   1.0000   0.0133
 -17.000  -0.8864   0.10227   0.09644  -0.0288   1.0000   0.0131
 -16.750  -0.8824   0.09934   0.09336  -0.0292   1.0000   0.0128
 -16.500  -0.8762   0.09695   0.09091  -0.0293   1.0000   0.0130
 -16.250  -0.8681   0.09485   0.08872  -0.0291   1.0000   0.0128
 -16.000  -0.8580   0.09321   0.08703  -0.0286   1.0000   0.0129
 -15.750  -0.8476   0.09167   0.08546  -0.0281   1.0000   0.0130
 -15.500  -0.8356   0.09036   0.08410  -0.0275   1.0000   0.0128
 -15.250  -0.8255   0.08918   0.08297  -0.0265   1.0000   0.0133
 -15.000  -0.8197   0.08698   0.08075  -0.0266   1.0000   0.0138
 -14.750  -0.8147   0.08472   0.07849  -0.0265   1.0000   0.0144
 -14.500  -0.8090   0.08254   0.07630  -0.0266   1.0000   0.0142
 -14.250  -0.8087   0.07951   0.07324  -0.0271   1.0000   0.0147
 -14.000  -0.8082   0.07643   0.07013  -0.0279   1.0000   0.0148
 -13.750  -0.8099   0.07306   0.06671  -0.0287   1.0000   0.0146
 -13.500  -0.8153   0.06923   0.06281  -0.0297   1.0000   0.0145
 -13.250  -0.8251   0.06479   0.05830  -0.0309   1.0000   0.0153
 -13.000  -0.8340   0.06051   0.05393  -0.0321   1.0000   0.0160
 -12.750  -0.8378   0.05701   0.05033  -0.0330   1.0000   0.0149
 -12.500  -0.8510   0.05238   0.04558  -0.0341   1.0000   0.0163
 -12.250  -0.8588   0.04857   0.04165  -0.0350   1.0000   0.0157
 -12.000  -0.8668   0.04485   0.03780  -0.0356   1.0000   0.0166
 -11.750  -0.8735   0.04146   0.03427  -0.0359   1.0000   0.0172
 -11.500  -0.8873   0.03764   0.03028  -0.0358   1.0000   0.0180
 -11.250  -0.8968   0.03457   0.02706  -0.0350   1.0000   0.0189
 -11.000  -0.9007   0.03223   0.02460  -0.0339   1.0000   0.0197
 -10.750  -0.9045   0.03010   0.02235  -0.0322   1.0000   0.0215
 -10.500  -0.9229   0.02725   0.01937  -0.0288   1.0000   0.0304
 -10.250  -0.9453   0.02464   0.01685  -0.0241   1.0000   0.0473
 -10.000  -0.9687   0.02248   0.01500  -0.0183   1.0000   0.0990
  -9.750  -0.9913   0.02079   0.01370  -0.0113   1.0000   0.1453
  -9.500  -1.0185   0.01975   0.01312  -0.0025   1.0000   0.2112
  -9.250  -1.0181   0.01944   0.01287   0.0021   1.0000   0.2291
  -9.000  -1.0171   0.01929   0.01270   0.0066   1.0000   0.2414
  -8.750  -1.0231   0.01928   0.01262   0.0123   1.0000   0.2508
  -8.500  -1.0283   0.01926   0.01261   0.0178   1.0000   0.2590
  -8.250  -1.0239   0.01927   0.01250   0.0214   0.9993   0.2683
  -8.000  -0.9837   0.01921   0.01235   0.0183   0.9923   0.2814
  -7.750  -0.9467   0.01919   0.01228   0.0158   0.9839   0.2961
  -7.500  -0.9109   0.01899   0.01213   0.0138   0.9755   0.3064
  -7.250  -0.8735   0.01875   0.01184   0.0115   0.9681   0.3156
  -7.000  -0.8370   0.01850   0.01147   0.0095   0.9603   0.3241
  -6.750  -0.7974   0.01806   0.01103   0.0070   0.9538   0.3300
  -6.500  -0.7581   0.01771   0.01063   0.0046   0.9472   0.3369
  -6.250  -0.7138   0.01724   0.01011   0.0011   0.9430   0.3439
  -6.000  -0.6753   0.01690   0.00974  -0.0011   0.9349   0.3504
  -5.750  -0.6264   0.01643   0.00919  -0.0055   0.9302   0.3575
  -5.500  -0.5812   0.01605   0.00882  -0.0091   0.9226   0.3642
  -5.250  -0.5313   0.01563   0.00832  -0.0138   0.9155   0.3718
  -5.000  -0.4883   0.01533   0.00802  -0.0169   0.9046   0.3789
  -4.750  -0.4484   0.01506   0.00767  -0.0195   0.8926   0.3863
  -4.500  -0.4129   0.01486   0.00747  -0.0210   0.8792   0.3934
  -4.250  -0.3840   0.01471   0.00724  -0.0212   0.8650   0.4011
  -4.000  -0.3573   0.01457   0.00710  -0.0209   0.8505   0.4085
  -3.750  -0.3330   0.01442   0.00690  -0.0200   0.8358   0.4161
  -3.500  -0.3093   0.01427   0.00673  -0.0190   0.8210   0.4238
  -3.250  -0.2864   0.01409   0.00654  -0.0178   0.8061   0.4320
  -3.000  -0.2646   0.01395   0.00636  -0.0163   0.7907   0.4414
  -2.750  -0.2417   0.01376   0.00619  -0.0151   0.7751   0.4501
  -2.500  -0.2199   0.01360   0.00598  -0.0137   0.7587   0.4603
  -2.250  -0.1974   0.01344   0.00580  -0.0124   0.7419   0.4702
  -2.000  -0.1744   0.01327   0.00563  -0.0112   0.7251   0.4803
  -1.750  -0.1523   0.01314   0.00547  -0.0098   0.7074   0.4915
  -1.500  -0.1310   0.01305   0.00534  -0.0083   0.6889   0.5036
  -1.250  -0.1092   0.01295   0.00522  -0.0069   0.6704   0.5159
  -1.000  -0.0871   0.01288   0.00513  -0.0056   0.6526   0.5284
  -0.750  -0.0649   0.01283   0.00505  -0.0042   0.6353   0.5412
  -0.500  -0.0435   0.01279   0.00501  -0.0028   0.6177   0.5547
  -0.250  -0.0221   0.01276   0.00499  -0.0013   0.6008   0.5691
   0.000  -0.0008   0.01276   0.00498   0.0002   0.5847   0.5845
   0.250   0.0205   0.01276   0.00499   0.0017   0.5693   0.6008
   0.500   0.0419   0.01279   0.00501   0.0031   0.5549   0.6175
   0.750   0.0633   0.01283   0.00505   0.0046   0.5415   0.6352
   1.000   0.0853   0.01288   0.00513   0.0059   0.5284   0.6524
   1.250   0.1074   0.01295   0.00523   0.0073   0.5160   0.6704
   1.500   0.1292   0.01304   0.00534   0.0087   0.5036   0.6888
   1.750   0.1505   0.01314   0.00547   0.0102   0.4916   0.7074
   2.000   0.1726   0.01327   0.00564   0.0116   0.4805   0.7252
   2.250   0.1956   0.01343   0.00581   0.0128   0.4704   0.7421
   2.500   0.2180   0.01359   0.00599   0.0141   0.4602   0.7588
   2.750   0.2399   0.01375   0.00619   0.0155   0.4502   0.7749
   3.000   0.2627   0.01395   0.00637   0.0168   0.4415   0.7907
   3.250   0.2845   0.01409   0.00655   0.0182   0.4321   0.8061
   3.500   0.3073   0.01426   0.00675   0.0194   0.4239   0.8212
   3.750   0.3310   0.01441   0.00691   0.0205   0.4162   0.8361
   4.000   0.3553   0.01456   0.00711   0.0213   0.4085   0.8506
   4.250   0.3821   0.01470   0.00725   0.0216   0.4012   0.8653
   4.500   0.4112   0.01485   0.00748   0.0214   0.3934   0.8794
   4.750   0.4470   0.01505   0.00768   0.0198   0.3863   0.8927
   5.000   0.4874   0.01532   0.00804   0.0172   0.3790   0.9047
   5.250   0.5292   0.01553   0.00822   0.0142   0.3684   0.9158
   5.500   0.5757   0.01574   0.00841   0.0103   0.3552   0.9236
   5.750   0.6194   0.01592   0.00866   0.0069   0.3425   0.9313
   6.000   0.6654   0.01625   0.00906   0.0031   0.3325   0.9370
   6.250   0.7032   0.01650   0.00931   0.0010   0.3206   0.9449
   6.500   0.7426   0.01670   0.00953  -0.0015   0.3037   0.9510
   6.750   0.7783   0.01697   0.00981  -0.0034   0.2897   0.9593
   7.000   0.8175   0.01732   0.01017  -0.0059   0.2793   0.9664
   7.250   0.8537   0.01758   0.01049  -0.0080   0.2599   0.9748
   7.500   0.8866   0.01804   0.01079  -0.0098   0.2235   0.9845
   7.750   0.9065   0.01996   0.01192  -0.0108   0.1094   0.9951
   8.000   0.8872   0.02204   0.01350  -0.0050   0.0254   1.0000
   8.250   0.8780   0.02192   0.01345   0.0011   0.0297   1.0000
   8.500   0.8560   0.02254   0.01405   0.0093   0.0208   1.0000
   8.750   0.8497   0.02329   0.01484   0.0146   0.0179   1.0000
   9.000   0.8510   0.02401   0.01564   0.0185   0.0166   1.0000
   9.250   0.8545   0.02479   0.01651   0.0217   0.0161   1.0000
   9.500   0.8575   0.02574   0.01755   0.0246   0.0157   1.0000
   9.750   0.8595   0.02691   0.01882   0.0272   0.0150   1.0000
  10.000   0.8610   0.02826   0.02028   0.0295   0.0144   1.0000
  10.250   0.8618   0.02980   0.02194   0.0315   0.0140   1.0000
  10.500   0.8627   0.03150   0.02378   0.0330   0.0140   1.0000
  10.750   0.8628   0.03342   0.02580   0.0343   0.0138   1.0000
  11.000   0.8592   0.03584   0.02835   0.0352   0.0136   1.0000
  11.250   0.8547   0.03858   0.03121   0.0356   0.0134   1.0000
  11.500   0.8435   0.04223   0.03500   0.0356   0.0131   1.0000
  11.750   0.8385   0.04546   0.03835   0.0352   0.0131   1.0000
  12.000   0.8324   0.04899   0.04198   0.0346   0.0131   1.0000
  12.250   0.8253   0.05274   0.04585   0.0337   0.0131   1.0000
  12.500   0.8165   0.05680   0.05000   0.0327   0.0131   1.0000
  12.750   0.8032   0.06144   0.05472   0.0316   0.0128   1.0000
  13.000   0.8002   0.06491   0.05825   0.0307   0.0129   1.0000
  13.250   0.7972   0.06835   0.06176   0.0299   0.0130   1.0000
  13.500   0.7940   0.07173   0.06516   0.0293   0.0129   1.0000
  13.750   0.7945   0.07452   0.06795   0.0291   0.0127   1.0000
  14.000   0.7991   0.07684   0.07028   0.0290   0.0128   1.0000
  14.250   0.8052   0.07909   0.07258   0.0287   0.0129   1.0000
  14.500   0.8142   0.08059   0.07407   0.0294   0.0128   1.0000
  14.750   0.8251   0.08197   0.07546   0.0301   0.0129   1.0000
  15.000   0.8358   0.08345   0.07698   0.0306   0.0129   1.0000
  15.250   0.8492   0.08447   0.07801   0.0317   0.0129   1.0000
  15.500   0.8578   0.08654   0.08017   0.0315   0.0132   1.0000
  15.750   0.8699   0.08796   0.08166   0.0324   0.0134   1.0000
  16.000   0.8790   0.08997   0.08378   0.0327   0.0136   1.0000
  16.250   0.8856   0.09247   0.08642   0.0329   0.0140   1.0000
  16.500   0.8882   0.09564   0.08976   0.0326   0.0144   1.0000
  16.750   0.8887   0.09911   0.09335   0.0314   0.0146   1.0000
  17.000   0.8862   0.10323   0.09765   0.0303   0.0150   1.0000
  17.250   0.8820   0.10762   0.10219   0.0287   0.0153   1.0000
  17.500   0.8754   0.11251   0.10724   0.0268   0.0157   1.0000
  17.750   0.8666   0.11785   0.11274   0.0244   0.0160   1.0000
  18.000   0.8579   0.12327   0.11830   0.0219   0.0163   1.0000
  18.250   0.8481   0.12899   0.12416   0.0191   0.0167   1.0000
  18.500   0.8376   0.13500   0.13030   0.0160   0.0169   1.0000
  18.750   0.8511   0.13662   0.13194   0.0167   0.0179   1.0000
  19.000   0.8394   0.14306   0.13853   0.0123   0.0182   1.0000
  19.250   0.8166   0.15256   0.14827   0.0059   0.0188   1.0000
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