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S1048 14% (Danny Howell) (s1048-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: S1048 14% (Danny Howell) (s1048-il)
Reynolds number: 200,000
Max Cl/Cd: 55.99 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1048-il-200000.txt
Download as CSV file: xf-s1048-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1048 14% (Danny Howell)                        
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.8646   0.11654   0.11252  -0.0050   1.0000   0.0223
 -16.000  -0.8834   0.10817   0.10398  -0.0109   1.0000   0.0221
 -15.750  -0.9013   0.10056   0.09621  -0.0154   1.0000   0.0219
 -15.500  -0.9219   0.09294   0.08841  -0.0201   1.0000   0.0218
 -15.250  -0.9403   0.08607   0.08137  -0.0240   1.0000   0.0217
 -15.000  -0.9569   0.07996   0.07507  -0.0274   1.0000   0.0217
 -14.750  -0.9710   0.07445   0.06938  -0.0300   1.0000   0.0215
 -14.500  -0.9877   0.06917   0.06388  -0.0328   1.0000   0.0218
 -14.250  -0.9989   0.06470   0.05920  -0.0347   1.0000   0.0218
 -14.000  -1.0092   0.06064   0.05494  -0.0361   1.0000   0.0219
 -13.750  -1.0206   0.05644   0.05052  -0.0371   1.0000   0.0222
 -13.500  -1.0221   0.05256   0.04649  -0.0371   1.0000   0.0228
 -13.250  -1.0200   0.04967   0.04348  -0.0370   1.0000   0.0230
 -13.000  -1.0170   0.04727   0.04105  -0.0370   1.0000   0.0240
 -12.750  -1.0137   0.04487   0.03853  -0.0367   1.0000   0.0245
 -12.500  -1.0085   0.04256   0.03609  -0.0362   1.0000   0.0250
 -12.250  -1.0022   0.04038   0.03377  -0.0355   1.0000   0.0258
 -12.000  -0.9942   0.03836   0.03162  -0.0346   1.0000   0.0265
 -11.750  -0.9860   0.03649   0.02960  -0.0337   1.0000   0.0274
 -11.500  -0.9777   0.03483   0.02777  -0.0327   1.0000   0.0283
 -11.250  -0.9737   0.03240   0.02539  -0.0312   1.0000   0.0299
 -11.000  -0.9687   0.03078   0.02376  -0.0300   1.0000   0.0317
 -10.750  -0.9627   0.02930   0.02220  -0.0285   1.0000   0.0337
 -10.500  -0.9550   0.02802   0.02079  -0.0267   1.0000   0.0356
 -10.250  -0.9580   0.02613   0.01894  -0.0238   1.0000   0.0382
 -10.000  -0.9549   0.02490   0.01768  -0.0210   1.0000   0.0412
  -9.750  -0.9488   0.02379   0.01647  -0.0182   1.0000   0.0454
  -9.500  -0.9454   0.02235   0.01508  -0.0153   1.0000   0.0520
  -9.250  -0.9387   0.02101   0.01376  -0.0127   1.0000   0.0623
  -9.000  -0.9316   0.01960   0.01247  -0.0100   1.0000   0.0824
  -8.750  -0.9222   0.01833   0.01141  -0.0077   1.0000   0.1126
  -8.500  -0.9085   0.01740   0.01062  -0.0059   1.0000   0.1439
  -8.250  -0.8928   0.01666   0.00999  -0.0042   1.0000   0.1724
  -8.000  -0.8761   0.01603   0.00945  -0.0026   1.0000   0.1980
  -7.750  -0.8585   0.01551   0.00898  -0.0011   1.0000   0.2221
  -7.500  -0.8398   0.01509   0.00857   0.0004   1.0000   0.2454
  -7.250  -0.8220   0.01468   0.00824   0.0019   1.0000   0.2674
  -7.000  -0.8031   0.01438   0.00794   0.0034   1.0000   0.2902
  -6.750  -0.7850   0.01408   0.00769   0.0050   1.0000   0.3099
  -6.500  -0.7665   0.01382   0.00743   0.0066   1.0000   0.3272
  -6.250  -0.7487   0.01359   0.00720   0.0083   1.0000   0.3432
  -6.000  -0.7320   0.01339   0.00701   0.0101   1.0000   0.3585
  -5.750  -0.7167   0.01324   0.00687   0.0121   1.0000   0.3731
  -5.500  -0.6994   0.01312   0.00675   0.0136   0.9993   0.3875
  -5.250  -0.6541   0.01300   0.00657   0.0097   0.9909   0.4074
  -5.000  -0.6089   0.01284   0.00642   0.0060   0.9827   0.4252
  -4.750  -0.5669   0.01265   0.00624   0.0029   0.9726   0.4418
  -4.500  -0.5244   0.01246   0.00606  -0.0001   0.9631   0.4581
  -4.250  -0.4799   0.01227   0.00587  -0.0034   0.9553   0.4742
  -4.000  -0.4414   0.01208   0.00567  -0.0055   0.9428   0.4891
  -3.750  -0.4043   0.01190   0.00549  -0.0072   0.9295   0.5035
  -3.500  -0.3700   0.01175   0.00533  -0.0083   0.9147   0.5174
  -3.250  -0.3391   0.01163   0.00517  -0.0086   0.8987   0.5311
  -3.000  -0.3111   0.01154   0.00504  -0.0082   0.8820   0.5446
  -2.750  -0.2846   0.01147   0.00495  -0.0076   0.8653   0.5571
  -2.500  -0.2588   0.01140   0.00486  -0.0068   0.8491   0.5695
  -2.250  -0.2333   0.01135   0.00479  -0.0060   0.8327   0.5820
  -2.000  -0.2077   0.01132   0.00472  -0.0052   0.8167   0.5948
  -1.750  -0.1821   0.01129   0.00465  -0.0045   0.8013   0.6079
  -1.500  -0.1563   0.01127   0.00459  -0.0038   0.7864   0.6213
  -1.250  -0.1305   0.01126   0.00454  -0.0031   0.7717   0.6346
  -1.000  -0.1044   0.01124   0.00452  -0.0024   0.7575   0.6473
  -0.750  -0.0784   0.01122   0.00450  -0.0018   0.7429   0.6602
  -0.500  -0.0523   0.01121   0.00449  -0.0012   0.7286   0.6734
  -0.250  -0.0262   0.01120   0.00447  -0.0006   0.7144   0.6868
   0.000   0.0000   0.01120   0.00447   0.0000   0.7006   0.7006
   0.250   0.0261   0.01120   0.00447   0.0006   0.6868   0.7144
   0.500   0.0523   0.01121   0.00449   0.0012   0.6734   0.7286
   0.750   0.0784   0.01122   0.00450   0.0018   0.6602   0.7429
   1.000   0.1044   0.01124   0.00452   0.0024   0.6473   0.7575
   1.250   0.1304   0.01126   0.00454   0.0031   0.6345   0.7717
   1.500   0.1563   0.01127   0.00459   0.0038   0.6213   0.7864
   1.750   0.1821   0.01129   0.00464   0.0045   0.6079   0.8013
   2.000   0.2077   0.01131   0.00472   0.0052   0.5948   0.8167
   2.250   0.2333   0.01135   0.00479   0.0060   0.5820   0.8327
   2.500   0.2588   0.01140   0.00486   0.0068   0.5696   0.8491
   2.750   0.2846   0.01147   0.00495   0.0076   0.5571   0.8653
   3.000   0.3111   0.01154   0.00504   0.0082   0.5446   0.8820
   3.250   0.3391   0.01163   0.00517   0.0086   0.5311   0.8987
   3.500   0.3700   0.01175   0.00533   0.0083   0.5174   0.9147
   3.750   0.4043   0.01190   0.00549   0.0072   0.5035   0.9295
   4.000   0.4414   0.01208   0.00567   0.0055   0.4891   0.9428
   4.250   0.4800   0.01227   0.00587   0.0034   0.4741   0.9553
   4.500   0.5244   0.01246   0.00606   0.0001   0.4581   0.9631
   4.750   0.5668   0.01265   0.00624  -0.0029   0.4418   0.9726
   5.000   0.6090   0.01284   0.00642  -0.0060   0.4253   0.9827
   5.250   0.6542   0.01300   0.00657  -0.0097   0.4075   0.9909
   5.500   0.6995   0.01312   0.00675  -0.0136   0.3876   0.9993
   5.750   0.7167   0.01324   0.00686  -0.0121   0.3730   1.0000
   6.000   0.7320   0.01339   0.00701  -0.0101   0.3585   1.0000
   6.250   0.7487   0.01359   0.00720  -0.0083   0.3433   1.0000
   6.500   0.7665   0.01382   0.00743  -0.0066   0.3273   1.0000
   6.750   0.7850   0.01408   0.00769  -0.0050   0.3099   1.0000
   7.000   0.8032   0.01438   0.00794  -0.0034   0.2903   1.0000
   7.250   0.8220   0.01468   0.00823  -0.0019   0.2673   1.0000
   7.500   0.8399   0.01509   0.00857  -0.0004   0.2453   1.0000
   7.750   0.8585   0.01551   0.00898   0.0011   0.2221   1.0000
   8.000   0.8761   0.01603   0.00945   0.0026   0.1980   1.0000
   8.250   0.8928   0.01666   0.00999   0.0042   0.1724   1.0000
   8.500   0.9085   0.01740   0.01062   0.0059   0.1439   1.0000
   8.750   0.9222   0.01833   0.01141   0.0077   0.1123   1.0000
   9.000   0.9317   0.01959   0.01246   0.0100   0.0824   1.0000
   9.250   0.9388   0.02100   0.01375   0.0127   0.0625   1.0000
   9.500   0.9453   0.02235   0.01508   0.0153   0.0519   1.0000
   9.750   0.9493   0.02376   0.01645   0.0181   0.0456   1.0000
  10.000   0.9551   0.02489   0.01767   0.0210   0.0415   1.0000
  10.250   0.9584   0.02611   0.01892   0.0238   0.0382   1.0000
  10.500   0.9553   0.02800   0.02078   0.0267   0.0356   1.0000
  10.750   0.9633   0.02922   0.02213   0.0284   0.0332   1.0000
  11.000   0.9691   0.03071   0.02368   0.0298   0.0313   1.0000
  11.250   0.9735   0.03242   0.02540   0.0311   0.0297   1.0000
  11.500   0.9783   0.03480   0.02776   0.0327   0.0283   1.0000
  11.750   0.9866   0.03648   0.02958   0.0336   0.0274   1.0000
  12.000   0.9951   0.03838   0.03164   0.0346   0.0266   1.0000
  12.250   1.0030   0.04036   0.03375   0.0354   0.0259   1.0000
  12.500   1.0096   0.04251   0.03603   0.0361   0.0252   1.0000
  12.750   1.0146   0.04484   0.03850   0.0367   0.0246   1.0000
  13.000   1.0177   0.04725   0.04103   0.0369   0.0239   1.0000
  13.250   1.0202   0.04978   0.04365   0.0370   0.0234   1.0000
  13.500   1.0239   0.05309   0.04697   0.0373   0.0221   1.0000
  13.750   1.0213   0.05646   0.05054   0.0371   0.0222   1.0000
  14.000   1.0118   0.06055   0.05483   0.0362   0.0220   1.0000
  14.250   1.0002   0.06461   0.05911   0.0346   0.0218   1.0000
  14.500   0.9878   0.06930   0.06402   0.0327   0.0217   1.0000
  14.750   0.9748   0.07430   0.06920   0.0304   0.0218   1.0000
  15.000   0.9581   0.07991   0.07503   0.0272   0.0217   1.0000
  15.250   0.9412   0.08607   0.08137   0.0238   0.0217   1.0000
  15.500   0.9229   0.09293   0.08841   0.0199   0.0218   1.0000
  15.750   0.9029   0.10047   0.09611   0.0154   0.0219   1.0000
  16.000   0.8851   0.10805   0.10385   0.0108   0.0221   1.0000
  16.250   0.8649   0.11668   0.11266   0.0048   0.0223   1.0000
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