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St. CYR 234 (Bartel 17-IC) (stcyr234-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: St. CYR 234 (Bartel 17-IC) (stcyr234-il)
Reynolds number: 100,000
Max Cl/Cd: 42.11 at α=1.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-stcyr234-il-100000-n5.txt
Download as CSV file: xf-stcyr234-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: St. CYR 234 (Bartel 17-IC)                      
  
 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  -0.2126   0.10465   0.09851  -0.0767   0.9629   0.0993
 -14.000  -0.2060   0.10173   0.09557  -0.0783   0.9574   0.1013
 -13.500  -0.2197   0.08920   0.08296  -0.0899   0.9476   0.1058
 -13.250  -0.1897   0.08825   0.08200  -0.0910   0.9456   0.1070
 -13.000  -0.1836   0.08652   0.08029  -0.0905   0.9376   0.1082
 -12.750  -0.1752   0.08297   0.07672  -0.0934   0.9326   0.1093
 -12.500  -0.1679   0.07841   0.07212  -0.0981   0.9289   0.1104
 -12.250  -0.1805   0.07411   0.06783  -0.1001   0.9192   0.1115
 -12.000  -0.3631   0.04445   0.03721  -0.1231   0.8902   0.1136
 -11.750  -0.3818   0.04091   0.03322  -0.1204   0.8774   0.1146
 -11.500  -0.3692   0.03782   0.02964  -0.1211   0.8724   0.1157
 -11.250  -0.3393   0.03642   0.02814  -0.1221   0.8699   0.1164
 -11.000  -0.3357   0.03563   0.02726  -0.1185   0.8593   0.1169
 -10.750  -0.3116   0.03449   0.02600  -0.1183   0.8546   0.1177
 -10.500  -0.2827   0.03328   0.02465  -0.1189   0.8517   0.1187
 -10.250  -0.2510   0.03215   0.02336  -0.1199   0.8495   0.1199
 -10.000  -0.2506   0.03170   0.02282  -0.1154   0.8382   0.1208
  -9.750  -0.2248   0.03073   0.02167  -0.1152   0.8344   0.1223
  -9.500  -0.1950   0.02970   0.02042  -0.1157   0.8318   0.1238
  -9.250  -0.1627   0.02868   0.01919  -0.1165   0.8298   0.1252
  -9.000  -0.1623   0.02846   0.01884  -0.1118   0.8191   0.1259
  -8.750  -0.1356   0.02778   0.01808  -0.1115   0.8155   0.1271
  -8.500  -0.1049   0.02719   0.01749  -0.1118   0.8130   0.1284
  -8.250  -0.0718   0.02660   0.01687  -0.1125   0.8111   0.1299
  -8.000  -0.0650   0.02654   0.01679  -0.1087   0.8026   0.1311
  -7.750  -0.0422   0.02619   0.01639  -0.1077   0.7978   0.1330
  -7.500  -0.0129   0.02573   0.01584  -0.1077   0.7950   0.1357
  -7.250   0.0189   0.02526   0.01523  -0.1080   0.7929   0.1386
  -7.000   0.0518   0.02479   0.01483  -0.1087   0.7913   0.1412
  -6.750   0.0520   0.02511   0.01517  -0.1040   0.7827   0.1429
  -6.500   0.0739   0.02496   0.01502  -0.1028   0.7787   0.1460
  -6.250   0.1022   0.02466   0.01467  -0.1026   0.7760   0.1501
  -6.000   0.1345   0.02422   0.01424  -0.1031   0.7739   0.1545
  -5.750   0.1703   0.02375   0.01381  -0.1041   0.7721   0.1605
  -5.500   0.1706   0.02414   0.01419  -0.0994   0.7628   0.1645
  -5.250   0.1967   0.02386   0.01397  -0.0987   0.7584   0.1718
  -5.000   0.2290   0.02351   0.01364  -0.0991   0.7557   0.1817
  -4.750   0.2642   0.02311   0.01334  -0.1000   0.7536   0.1927
  -4.500   0.3049   0.02261   0.01292  -0.1018   0.7517   0.2065
  -4.250   0.2934   0.02345   0.01380  -0.0952   0.7411   0.2118
  -4.000   0.3270   0.02308   0.01349  -0.0957   0.7372   0.2265
  -3.750   0.3695   0.02251   0.01298  -0.0975   0.7342   0.2456
  -3.500   0.3973   0.02233   0.01284  -0.0971   0.7286   0.2625
  -3.250   0.4090   0.02253   0.01306  -0.0940   0.7198   0.2762
  -3.000   0.4495   0.02202   0.01261  -0.0956   0.7155   0.2990
  -2.750   0.4985   0.02142   0.01205  -0.0987   0.7122   0.3250
  -2.500   0.4940   0.02197   0.01261  -0.0930   0.7014   0.3358
  -2.250   0.5318   0.02149   0.01218  -0.0941   0.6957   0.3559
  -1.750   0.5772   0.02126   0.01209  -0.0917   0.6801   0.3866
  -1.500   0.6202   0.02070   0.01158  -0.0937   0.6734   0.4070
  -1.250   0.6382   0.02075   0.01174  -0.0918   0.6651   0.4241
  -1.000   0.6595   0.02071   0.01187  -0.0904   0.6563   0.4479
  -0.750   0.7030   0.02018   0.01153  -0.0925   0.6497   0.4980
  -0.500   0.7020   0.02075   0.01217  -0.0875   0.6383   0.5377
  -0.250   0.7389   0.02041   0.01180  -0.0885   0.6299   0.5845
   0.000   0.7450   0.02075   0.01226  -0.0848   0.6177   0.6125
   0.250   0.7797   0.02008   0.01190  -0.0855   0.6073   0.6657
   0.750   0.8331   0.02028   0.01261  -0.0858   0.5718   1.0000
   1.000   0.8421   0.02067   0.01295  -0.0827   0.5508   1.0000
   1.250   0.8509   0.02111   0.01331  -0.0796   0.5227   1.0000
   1.500   0.8719   0.02113   0.01310  -0.0781   0.4854   1.0000
   1.750   0.8935   0.02122   0.01280  -0.0767   0.4521   1.0000
   2.000   0.9086   0.02172   0.01299  -0.0746   0.4270   1.0000
   2.250   0.9229   0.02234   0.01339  -0.0726   0.4069   1.0000
   2.500   0.9376   0.02300   0.01386  -0.0708   0.3891   1.0000
   2.750   0.9523   0.02367   0.01439  -0.0690   0.3727   1.0000
   3.000   0.9667   0.02435   0.01499  -0.0673   0.3569   1.0000
   3.250   0.9813   0.02504   0.01558  -0.0657   0.3423   1.0000
   3.500   0.9951   0.02576   0.01617  -0.0640   0.3285   1.0000
   3.750   1.0086   0.02649   0.01682  -0.0623   0.3150   1.0000
   4.000   1.0231   0.02720   0.01745  -0.0608   0.3033   1.0000
   4.250   1.0376   0.02794   0.01808  -0.0594   0.2936   1.0000
   4.500   1.0541   0.02861   0.01872  -0.0583   0.2851   1.0000
   4.750   1.0699   0.02933   0.01936  -0.0571   0.2776   1.0000
   5.000   1.0868   0.03003   0.02000  -0.0560   0.2710   1.0000
   5.250   1.1031   0.03076   0.02072  -0.0550   0.2640   1.0000
   5.500   1.1187   0.03154   0.02142  -0.0539   0.2579   1.0000
   5.750   1.1353   0.03229   0.02215  -0.0530   0.2521   1.0000
   6.000   1.1511   0.03308   0.02298  -0.0520   0.2459   1.0000
   6.250   1.1659   0.03393   0.02377  -0.0510   0.2400   1.0000
   6.500   1.1819   0.03477   0.02455  -0.0501   0.2346   1.0000
   6.750   1.1957   0.03568   0.02554  -0.0490   0.2287   1.0000
   7.000   1.2090   0.03662   0.02649  -0.0480   0.2230   1.0000
   7.250   1.2240   0.03754   0.02729  -0.0471   0.2176   1.0000
   7.500   1.2348   0.03863   0.02853  -0.0460   0.2118   1.0000
   7.750   1.2457   0.03973   0.02967  -0.0449   0.2060   1.0000
   8.000   1.2575   0.04081   0.03070  -0.0439   0.2008   1.0000
   8.250   1.2672   0.04205   0.03204  -0.0428   0.1953   1.0000
   8.500   1.2757   0.04336   0.03344  -0.0418   0.1894   1.0000
   8.750   1.2842   0.04467   0.03473  -0.0408   0.1844   1.0000
   9.000   1.2926   0.04608   0.03624  -0.0398   0.1791   1.0000
   9.250   1.2995   0.04761   0.03788  -0.0389   0.1734   1.0000
   9.500   1.3059   0.04916   0.03943  -0.0380   0.1688   1.0000
   9.750   1.3127   0.05082   0.04119  -0.0372   0.1637   1.0000
  10.000   1.3183   0.05258   0.04304  -0.0365   0.1586   1.0000
  10.250   1.3231   0.05439   0.04486  -0.0358   0.1546   1.0000
  10.500   1.3283   0.05631   0.04688  -0.0352   0.1501   1.0000
  10.750   1.3325   0.05836   0.04901  -0.0346   0.1457   1.0000
  11.000   1.3357   0.06046   0.05113  -0.0342   0.1423   1.0000
  11.250   1.3392   0.06264   0.05336  -0.0337   0.1389   1.0000
  11.500   1.3421   0.06500   0.05584  -0.0334   0.1353   1.0000
  11.750   1.3439   0.06745   0.05835  -0.0332   0.1321   1.0000
  12.000   1.3464   0.06983   0.06072  -0.0331   0.1296   1.0000
  12.250   1.3484   0.07238   0.06334  -0.0330   0.1270   1.0000
  12.500   1.3479   0.07532   0.06642  -0.0330   0.1242   1.0000
  12.750   1.3474   0.07828   0.06947  -0.0331   0.1216   1.0000
  13.000   1.3481   0.08109   0.07232  -0.0334   0.1195   1.0000
  13.250   1.3521   0.08344   0.07465  -0.0336   0.1175   1.0000
  13.500   1.3478   0.08710   0.07847  -0.0341   0.1154   1.0000
  13.750   1.3414   0.09114   0.08268  -0.0348   0.1133   1.0000
  14.000   1.3366   0.09502   0.08668  -0.0357   0.1114   1.0000
  14.250   1.3337   0.09862   0.09037  -0.0366   0.1097   1.0000
  14.500   1.3352   0.10158   0.09338  -0.0373   0.1082   1.0000
  14.750   1.3428   0.10356   0.09533  -0.0378   0.1068   1.0000
  15.000   1.3287   0.10912   0.10109  -0.0396   0.1054   1.0000
  15.250   1.3015   0.11715   0.10943  -0.0427   0.1038   1.0000
  15.500   1.2600   0.12812   0.12072  -0.0474   0.1021   1.0000
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