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FX 78-PK-188/20 (fx78pk188-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: FX 78-PK-188/20 (fx78pk188-il)
Reynolds number: 100,000
Max Cl/Cd: 22.88 at α=11°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx78pk188-il-100000-n5.txt
Download as CSV file: xf-fx78pk188-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 78-PK-188/20                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.3234   0.10580   0.10019  -0.1011   0.8501   0.0328
 -14.000  -0.3715   0.08933   0.08370  -0.1101   0.8491   0.0318
 -13.750  -0.4258   0.07696   0.07113  -0.1173   0.8471   0.0309
 -13.500  -0.4631   0.06981   0.06374  -0.1203   0.8447   0.0305
 -13.250  -0.4901   0.06476   0.05846  -0.1212   0.8422   0.0304
 -13.000  -0.5091   0.06094   0.05443  -0.1212   0.8399   0.0306
 -12.750  -0.5262   0.05750   0.05074  -0.1204   0.8378   0.0307
 -12.500  -0.5385   0.05468   0.04770  -0.1192   0.8358   0.0311
 -12.250  -0.5486   0.05204   0.04484  -0.1178   0.8333   0.0315
 -12.000  -0.5556   0.04966   0.04222  -0.1162   0.8308   0.0322
 -11.750  -0.5605   0.04750   0.03978  -0.1144   0.8284   0.0331
 -11.500  -0.5636   0.04552   0.03749  -0.1123   0.8260   0.0342
 -11.250  -0.5659   0.04372   0.03531  -0.1098   0.8237   0.0354
 -11.000  -0.5597   0.04179   0.03311  -0.1081   0.8218   0.0365
 -10.750  -0.5443   0.04019   0.03145  -0.1077   0.8198   0.0378
 -10.500  -0.5321   0.03907   0.03023  -0.1067   0.8176   0.0395
 -10.250  -0.5185   0.03796   0.02895  -0.1057   0.8155   0.0415
 -10.000  -0.4987   0.03666   0.02739  -0.1052   0.8138   0.0434
  -9.750  -0.4758   0.03548   0.02594  -0.1049   0.8122   0.0451
  -9.500  -0.4484   0.03419   0.02464  -0.1054   0.8109   0.0477
  -9.250  -0.4261   0.03332   0.02373  -0.1052   0.8094   0.0500
  -9.000  -0.4011   0.03247   0.02278  -0.1051   0.8081   0.0521
  -8.750  -0.3774   0.03172   0.02188  -0.1047   0.8067   0.0544
  -8.500  -0.3572   0.03114   0.02123  -0.1041   0.8047   0.0570
  -8.250  -0.3417   0.03050   0.02065  -0.1031   0.8026   0.0600
  -8.000  -0.3265   0.03001   0.02013  -0.1019   0.8006   0.0631
  -7.750  -0.3119   0.02954   0.01959  -0.1005   0.7988   0.0663
  -7.500  -0.2988   0.02905   0.01906  -0.0988   0.7970   0.0699
  -7.250  -0.2869   0.02854   0.01855  -0.0971   0.7952   0.0754
  -7.000  -0.2740   0.02807   0.01806  -0.0953   0.7934   0.0837
  -6.750  -0.2617   0.02755   0.01758  -0.0934   0.7919   0.0970
  -6.500  -0.2560   0.02728   0.01744  -0.0907   0.7892   0.1167
  -6.250  -0.2537   0.02711   0.01745  -0.0874   0.7865   0.1446
  -6.000  -0.2555   0.02686   0.01746  -0.0834   0.7838   0.1894
  -5.750  -0.2621   0.02653   0.01741  -0.0784   0.7811   0.2430
  -5.500  -0.2720   0.02593   0.01719  -0.0727   0.7786   0.3153
  -5.250  -0.2805   0.02528   0.01705  -0.0668   0.7767   0.4129
  -5.000  -0.2183   0.02721   0.01990  -0.0686   0.7767   0.5959
  -4.750  -0.2381   0.02823   0.02099  -0.0612   0.7718   0.6173
  -4.500  -0.2560   0.02861   0.02135  -0.0540   0.7674   0.6427
  -4.250  -0.2567   0.02905   0.02168  -0.0491   0.7647   0.6719
  -4.000  -0.2399   0.03004   0.02255  -0.0462   0.7632   0.6960
  -3.750  -0.2245   0.03069   0.02306  -0.0435   0.7619   0.7146
  -3.500  -0.2461   0.03214   0.02458  -0.0353   0.7553   0.7220
  -3.250  -0.2356   0.03306   0.02543  -0.0317   0.7522   0.7357
  -3.000  -0.2189   0.03381   0.02610  -0.0292   0.7503   0.7487
  -2.750  -0.2063   0.03408   0.02624  -0.0265   0.7486   0.7605
  -2.500  -0.1717   0.03460   0.02664  -0.0272   0.7476   0.7649
  -2.250  -0.1544   0.03466   0.02657  -0.0257   0.7460   0.7728
  -2.000  -0.2006   0.03556   0.02757  -0.0139   0.7374   0.7811
  -1.750  -0.1856   0.03551   0.02740  -0.0123   0.7351   0.7875
  -1.500  -0.1644   0.03538   0.02714  -0.0117   0.7334   0.7919
  -1.250  -0.1364   0.03543   0.02709  -0.0120   0.7323   0.7945
  -1.000  -0.1533   0.03598   0.02764  -0.0058   0.7261   0.8004
  -0.750  -0.1441   0.03593   0.02749  -0.0037   0.7225   0.8058
  -0.500  -0.1218   0.03607   0.02754  -0.0032   0.7204   0.8082
  -0.250  -0.0966   0.03612   0.02752  -0.0032   0.7187   0.8109
   0.000  -0.0693   0.03611   0.02742  -0.0036   0.7174   0.8137
   0.250  -0.0787   0.03656   0.02784   0.0010   0.7108   0.8193
   0.500  -0.0609   0.03670   0.02792   0.0019   0.7075   0.8221
   0.750  -0.0365   0.03680   0.02797   0.0020   0.7052   0.8244
   1.000  -0.0101   0.03687   0.02798   0.0018   0.7036   0.8269
   1.250   0.0188   0.03689   0.02795   0.0011   0.7022   0.8293
   1.500   0.0109   0.03751   0.02856   0.0052   0.6943   0.8338
   1.750   0.0338   0.03763   0.02863   0.0052   0.6915   0.8364
   2.000   0.0610   0.03770   0.02868   0.0049   0.6895   0.8382
   2.250   0.0906   0.03774   0.02869   0.0042   0.6880   0.8399
   2.500   0.0880   0.03843   0.02940   0.0076   0.6801   0.8433
   2.750   0.1120   0.03857   0.02952   0.0075   0.6771   0.8457
   3.000   0.1404   0.03863   0.02956   0.0069   0.6750   0.8476
   3.250   0.1714   0.03864   0.02956   0.0058   0.6734   0.8497
   3.500   0.1696   0.03938   0.03032   0.0090   0.6646   0.8527
   3.750   0.1959   0.03948   0.03045   0.0087   0.6618   0.8546
   4.000   0.2265   0.03948   0.03046   0.0079   0.6599   0.8562
   4.500   0.2571   0.04026   0.03130   0.0097   0.6481   0.8610
   4.750   0.2879   0.04023   0.03130   0.0088   0.6459   0.8633
   5.250   0.3224   0.04087   0.03202   0.0102   0.6337   0.8680
   5.500   0.3545   0.04069   0.03190   0.0094   0.6314   0.8697
   5.750   0.3612   0.04138   0.03265   0.0112   0.6219   0.8723
   6.000   0.3904   0.04130   0.03262   0.0106   0.6186   0.8745
   6.250   0.4230   0.04109   0.03250   0.0097   0.6166   0.8769
   6.500   0.4279   0.04196   0.03342   0.0115   0.6061   0.8804
   6.750   0.4592   0.04173   0.03329   0.0108   0.6034   0.8826
   7.000   0.4681   0.04250   0.03414   0.0121   0.5937   0.8854
   7.250   0.4977   0.04231   0.03407   0.0116   0.5900   0.8879
   7.500   0.5310   0.04196   0.03382   0.0107   0.5878   0.8904
   7.750   0.5382   0.04285   0.03481   0.0121   0.5765   0.8939
   8.000   0.5717   0.04238   0.03448   0.0113   0.5739   0.8967
   8.250   0.5827   0.04299   0.03520   0.0125   0.5623   0.9005
   8.750   0.6361   0.04199   0.03446   0.0126   0.5461   0.9085
   9.250   0.6769   0.04165   0.03441   0.0137   0.5210   0.9172
   9.500   0.7011   0.04117   0.03405   0.0140   0.5060   0.9224
  10.000   0.7583   0.04027   0.03345   0.0132   0.4738   0.9336
  10.250   0.7921   0.03962   0.03289   0.0123   0.4540   0.9406
  10.500   0.8292   0.03880   0.03211   0.0109   0.4248   0.9486
  10.750   0.8641   0.03810   0.03129   0.0098   0.3793   0.9603
  11.000   0.8793   0.03843   0.03137   0.0107   0.3328   1.0000
  11.250   0.8860   0.03971   0.03237   0.0120   0.2853   1.0000
  11.500   0.8888   0.04145   0.03383   0.0133   0.2382   1.0000
  11.750   0.8907   0.04339   0.03548   0.0145   0.1989   1.0000
  12.000   0.8946   0.04528   0.03717   0.0154   0.1685   1.0000
  12.250   0.9004   0.04710   0.03885   0.0162   0.1460   1.0000
  12.500   0.9077   0.04884   0.04054   0.0168   0.1286   1.0000
  12.750   0.9153   0.05059   0.04223   0.0173   0.1149   1.0000
  13.000   0.9230   0.05237   0.04398   0.0178   0.1045   1.0000
  13.250   0.9322   0.05405   0.04568   0.0182   0.0952   1.0000
  13.500   0.9395   0.05591   0.04752   0.0187   0.0870   1.0000
  13.750   0.9466   0.05782   0.04944   0.0190   0.0789   1.0000
  14.000   0.9550   0.05969   0.05136   0.0192   0.0703   1.0000
  14.250   0.9602   0.06188   0.05354   0.0194   0.0635   1.0000
  14.500   0.9686   0.06382   0.05561   0.0194   0.0564   1.0000
  14.750   0.9739   0.06607   0.05788   0.0196   0.0515   1.0000
  15.000   0.9809   0.06823   0.06015   0.0197   0.0462   1.0000
  15.250   0.9840   0.07081   0.06273   0.0197   0.0423   1.0000
  15.500   0.9903   0.07313   0.06520   0.0197   0.0379   1.0000
  15.750   0.9923   0.07594   0.06804   0.0194   0.0349   1.0000
  16.000   0.9965   0.07855   0.07076   0.0194   0.0319   1.0000
  16.250   1.0002   0.08125   0.07357   0.0192   0.0296   1.0000
  16.500   1.0031   0.08409   0.07649   0.0189   0.0281   1.0000
  16.750   1.0042   0.08715   0.07961   0.0184   0.0269   1.0000
  17.000   1.0083   0.08998   0.08263   0.0181   0.0254   1.0000
  17.250   1.0100   0.09317   0.08600   0.0175   0.0239   1.0000
  17.500   1.0105   0.09655   0.08951   0.0167   0.0228   1.0000
  17.750   1.0085   0.10033   0.09338   0.0154   0.0217   1.0000
  18.000   1.0073   0.10399   0.09712   0.0142   0.0210   1.0000
  18.250   1.0065   0.10768   0.10092   0.0130   0.0205   1.0000
  18.500   1.0030   0.11199   0.10549   0.0116   0.0200   1.0000
  18.750   0.9971   0.11680   0.11054   0.0097   0.0196   1.0000
  19.000   0.9905   0.12184   0.11578   0.0075   0.0194   1.0000
  19.250   0.9802   0.12771   0.12188   0.0047   0.0191   1.0000
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