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FX 38-153 AIRFOIL (fx38153-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 38-153 AIRFOIL (fx38153-il)
Reynolds number: 500,000
Max Cl/Cd: 60.76 at α=1°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx38153-il-500000-n5.txt
Download as CSV file: xf-fx38153-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 38-153 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.5175   0.04621   0.04269  -0.1277   0.9617   0.0053
 -12.000  -0.5410   0.04111   0.03723  -0.1268   0.9585   0.0053
 -11.750  -0.5523   0.03749   0.03330  -0.1254   0.9560   0.0053
 -11.500  -0.5569   0.03471   0.03025  -0.1239   0.9536   0.0053
 -11.250  -0.5586   0.03253   0.02784  -0.1218   0.9505   0.0053
 -11.000  -0.5557   0.03055   0.02563  -0.1199   0.9474   0.0054
 -10.750  -0.5483   0.02882   0.02368  -0.1184   0.9449   0.0054
 -10.500  -0.5373   0.02724   0.02191  -0.1171   0.9430   0.0055
 -10.250  -0.5233   0.02582   0.02028  -0.1161   0.9414   0.0056
 -10.000  -0.5068   0.02455   0.01884  -0.1152   0.9399   0.0057
  -9.750  -0.4915   0.02351   0.01766  -0.1139   0.9378   0.0058
  -9.500  -0.4756   0.02258   0.01660  -0.1126   0.9356   0.0059
  -9.250  -0.4583   0.02173   0.01563  -0.1114   0.9334   0.0060
  -9.000  -0.4396   0.02090   0.01469  -0.1105   0.9314   0.0061
  -8.750  -0.4198   0.02013   0.01381  -0.1097   0.9296   0.0062
  -8.500  -0.3996   0.01941   0.01301  -0.1089   0.9282   0.0063
  -8.250  -0.3789   0.01873   0.01225  -0.1083   0.9268   0.0064
  -8.000  -0.3580   0.01809   0.01154  -0.1076   0.9256   0.0065
  -7.750  -0.3366   0.01753   0.01091  -0.1071   0.9243   0.0066
  -7.500  -0.3259   0.01725   0.01059  -0.1044   0.9207   0.0068
  -7.250  -0.3142   0.01682   0.01012  -0.1019   0.9176   0.0070
  -7.000  -0.2986   0.01632   0.00959  -0.1002   0.9153   0.0072
  -6.750  -0.2788   0.01584   0.00907  -0.0993   0.9134   0.0073
  -6.500  -0.2563   0.01539   0.00857  -0.0989   0.9119   0.0073
  -6.250  -0.2323   0.01497   0.00810  -0.0987   0.9107   0.0074
  -6.000  -0.2071   0.01458   0.00767  -0.0988   0.9096   0.0075
  -5.750  -0.1978   0.01448   0.00756  -0.0956   0.9053   0.0076
  -5.500  -0.1802   0.01426   0.00731  -0.0940   0.9023   0.0077
  -5.250  -0.1575   0.01399   0.00701  -0.0934   0.9002   0.0078
  -5.000  -0.1328   0.01372   0.00671  -0.0932   0.8986   0.0080
  -4.750  -0.1068   0.01346   0.00643  -0.0933   0.8974   0.0082
  -4.500  -0.0794   0.01321   0.00616  -0.0936   0.8963   0.0086
  -4.250  -0.0505   0.01295   0.00590  -0.0943   0.8953   0.0094
  -4.000  -0.0200   0.01270   0.00566  -0.0952   0.8943   0.0143
  -3.750  -0.0137   0.01272   0.00568  -0.0911   0.8877   0.0157
  -3.500   0.0125   0.01254   0.00547  -0.0910   0.8852   0.0175
  -3.250   0.0412   0.01231   0.00524  -0.0916   0.8833   0.0198
  -3.000   0.0724   0.01197   0.00495  -0.0926   0.8816   0.0306
  -2.750   0.1064   0.01166   0.00466  -0.0942   0.8800   0.0436
  -2.500   0.1205   0.01147   0.00457  -0.0917   0.8739   0.0708
  -2.250   0.1445   0.01087   0.00429  -0.0917   0.8700   0.1618
  -2.000   0.1779   0.00924   0.00367  -0.0951   0.8676   0.4404
  -1.750   0.2210   0.00811   0.00349  -0.0998   0.8661   0.6769
  -1.500   0.2501   0.00811   0.00355  -0.1001   0.8635   0.7022
  -1.250   0.2717   0.00821   0.00368  -0.0988   0.8579   0.7176
  -1.000   0.3015   0.00818   0.00365  -0.0992   0.8536   0.7298
  -0.750   0.3320   0.00810   0.00354  -0.0998   0.8472   0.7406
  -0.500   0.3580   0.00811   0.00353  -0.0993   0.8374   0.7504
  -0.250   0.3826   0.00815   0.00356  -0.0985   0.8267   0.7571
   0.000   0.4097   0.00818   0.00358  -0.0983   0.8162   0.7619
   0.250   0.4406   0.00818   0.00352  -0.0990   0.8029   0.7684
   0.500   0.4678   0.00824   0.00353  -0.0987   0.7855   0.7720
   0.750   0.4955   0.00831   0.00348  -0.0986   0.7589   0.7741
   1.000   0.5177   0.00852   0.00343  -0.0973   0.7069   0.7757
   1.250   0.5297   0.00896   0.00355  -0.0941   0.6471   0.7779
   1.500   0.5393   0.00941   0.00372  -0.0905   0.5939   0.7805
   1.750   0.5544   0.00982   0.00390  -0.0883   0.5477   0.7830
   2.000   0.5737   0.01020   0.00407  -0.0870   0.5092   0.7851
   2.250   0.5926   0.01055   0.00429  -0.0855   0.4779   0.7861
   2.500   0.6141   0.01085   0.00449  -0.0845   0.4523   0.7872
   2.750   0.6343   0.01122   0.00473  -0.0834   0.4213   0.7884
   3.000   0.6530   0.01170   0.00502  -0.0820   0.3798   0.7896
   3.250   0.6711   0.01225   0.00532  -0.0806   0.3316   0.7908
   3.500   0.6904   0.01278   0.00562  -0.0794   0.2847   0.7920
   3.750   0.7117   0.01322   0.00590  -0.0787   0.2484   0.7933
   4.000   0.7327   0.01370   0.00621  -0.0779   0.2145   0.7949
   4.250   0.7535   0.01422   0.00653  -0.0771   0.1784   0.7963
   4.500   0.7768   0.01459   0.00681  -0.0768   0.1574   0.7977
   4.750   0.7993   0.01503   0.00712  -0.0763   0.1339   0.7992
   5.000   0.8234   0.01538   0.00740  -0.0762   0.1225   0.8005
   5.250   0.8466   0.01566   0.00768  -0.0757   0.1110   0.8013
   5.500   0.8671   0.01611   0.00804  -0.0748   0.0933   0.8022
   5.750   0.8885   0.01649   0.00838  -0.0741   0.0840   0.8030
   6.000   0.9092   0.01693   0.00877  -0.0732   0.0655   0.8040
   6.250   0.9296   0.01739   0.00919  -0.0723   0.0556   0.8050
   6.500   0.9508   0.01781   0.00959  -0.0716   0.0497   0.8061
   6.750   0.9733   0.01813   0.00994  -0.0711   0.0460   0.8072
   7.000   0.9924   0.01870   0.01046  -0.0700   0.0319   0.8082
   7.250   1.0136   0.01913   0.01090  -0.0694   0.0296   0.8092
   7.500   1.0347   0.01956   0.01135  -0.0687   0.0276   0.8103
   7.750   1.0561   0.01999   0.01180  -0.0681   0.0262   0.8114
   8.000   1.0778   0.02038   0.01225  -0.0676   0.0254   0.8125
   8.250   1.0992   0.02080   0.01272  -0.0670   0.0245   0.8135
   8.500   1.1201   0.02125   0.01321  -0.0664   0.0222   0.8146
   8.750   1.1382   0.02192   0.01387  -0.0654   0.0163   0.8156
   9.000   1.1565   0.02253   0.01449  -0.0644   0.0156   0.8166
   9.250   1.1736   0.02316   0.01516  -0.0631   0.0148   0.8176
   9.500   1.1903   0.02382   0.01587  -0.0619   0.0140   0.8185
   9.750   1.2074   0.02446   0.01657  -0.0607   0.0136   0.8194
  10.000   1.2242   0.02513   0.01731  -0.0596   0.0133   0.8203
  10.250   1.2403   0.02585   0.01809  -0.0583   0.0130   0.8212
  10.500   1.2565   0.02657   0.01889  -0.0572   0.0129   0.8222
  10.750   1.2719   0.02736   0.01976  -0.0559   0.0126   0.8232
  11.000   1.2862   0.02821   0.02069  -0.0546   0.0122   0.8242
  11.250   1.2998   0.02914   0.02171  -0.0533   0.0117   0.8252
  11.500   1.3121   0.03017   0.02282  -0.0518   0.0113   0.8263
  11.750   1.3234   0.03129   0.02402  -0.0503   0.0109   0.8273
  12.000   1.3339   0.03248   0.02529  -0.0488   0.0106   0.8284
  12.250   1.3433   0.03377   0.02668  -0.0472   0.0103   0.8296
  12.500   1.3507   0.03526   0.02825  -0.0456   0.0101   0.8308
  12.750   1.3628   0.03639   0.02947  -0.0445   0.0099   0.8319
  13.000   1.3737   0.03758   0.03076  -0.0433   0.0097   0.8327
  13.250   1.3835   0.03888   0.03216  -0.0420   0.0095   0.8336
  13.500   1.3928   0.04026   0.03364  -0.0409   0.0092   0.8345
  13.750   1.4012   0.04177   0.03526  -0.0397   0.0090   0.8354
  14.000   1.4088   0.04339   0.03699  -0.0386   0.0087   0.8363
  14.250   1.4157   0.04511   0.03881  -0.0376   0.0083   0.8372
  14.500   1.4218   0.04696   0.04077  -0.0367   0.0079   0.8382
  14.750   1.4266   0.04901   0.04291  -0.0358   0.0076   0.8393
  15.000   1.4318   0.05109   0.04509  -0.0351   0.0073   0.8406
  15.250   1.4395   0.05296   0.04707  -0.0346   0.0069   0.8418
  15.500   1.4451   0.05512   0.04937  -0.0342   0.0064   0.8430
  15.750   1.4483   0.05761   0.05201  -0.0339   0.0057   0.8441
  16.000   1.4475   0.06067   0.05521  -0.0336   0.0044   0.8451
  16.250   1.4564   0.06258   0.05713  -0.0338   0.0033   0.8461
  16.500   1.4575   0.06554   0.06011  -0.0340   0.0029   0.8470
  16.750   1.4539   0.06917   0.06382  -0.0343   0.0027   0.8478
  17.000   1.4492   0.07303   0.06781  -0.0348   0.0025   0.8486
  17.250   1.4421   0.07731   0.07223  -0.0355   0.0024   0.8494
  17.500   1.4334   0.08199   0.07706  -0.0366   0.0024   0.8502
  17.750   1.4234   0.08702   0.08223  -0.0380   0.0023   0.8510
  18.000   1.4118   0.09243   0.08779  -0.0398   0.0023   0.8518
  18.250   1.3983   0.09824   0.09376  -0.0419   0.0022   0.8525
  18.500   1.3842   0.10428   0.09996  -0.0443   0.0022   0.8533
  18.750   1.3696   0.11057   0.10640  -0.0470   0.0022   0.8540
  19.000   1.3532   0.11732   0.11330  -0.0501   0.0022   0.8548
  19.250   1.3373   0.12411   0.12024  -0.0535   0.0022   0.8557
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