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FX 61-184 AIRFOIL (fx61184-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 61-184 AIRFOIL (fx61184-il)
Reynolds number: 200,000
Max Cl/Cd: 71.08 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx61184-il-200000-n5.txt
Download as CSV file: xf-fx61184-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 61-184 AIRFOIL                               
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.5386   0.09581   0.09185  -0.0687   1.0000   0.0147
 -14.750  -0.5758   0.08447   0.08030  -0.0756   1.0000   0.0146
 -14.500  -0.6040   0.07617   0.07178  -0.0802   1.0000   0.0145
 -14.250  -0.6252   0.06982   0.06525  -0.0833   1.0000   0.0145
 -14.000  -0.6453   0.06426   0.05947  -0.0856   1.0000   0.0147
 -13.750  -0.6630   0.05954   0.05453  -0.0869   1.0000   0.0148
 -13.500  -0.6729   0.05468   0.04941  -0.0888   0.9812   0.0151
 -13.250  -0.6651   0.04993   0.04429  -0.0946   0.9378   0.0156
 -13.000  -0.6364   0.04701   0.04123  -0.1011   0.9209   0.0160
 -12.750  -0.6074   0.04418   0.03818  -0.1077   0.9043   0.0167
 -12.500  -0.5819   0.04142   0.03512  -0.1129   0.8873   0.0175
 -12.250  -0.5597   0.03895   0.03229  -0.1162   0.8721   0.0182
 -12.000  -0.5384   0.03695   0.02995  -0.1182   0.8601   0.0188
 -11.500  -0.4989   0.03422   0.02699  -0.1208   0.8419   0.0204
 -11.250  -0.4803   0.03308   0.02572  -0.1213   0.8348   0.0211
 -11.000  -0.4626   0.03205   0.02456  -0.1211   0.8282   0.0218
 -10.750  -0.4440   0.03108   0.02344  -0.1208   0.8220   0.0226
 -10.500  -0.4250   0.03020   0.02240  -0.1204   0.8168   0.0232
 -10.250  -0.4090   0.02929   0.02146  -0.1198   0.8115   0.0243
 -10.000  -0.3928   0.02847   0.02060  -0.1193   0.8067   0.0250
  -9.750  -0.3764   0.02770   0.01977  -0.1188   0.8025   0.0261
  -9.500  -0.3612   0.02694   0.01895  -0.1180   0.7979   0.0274
  -9.250  -0.3464   0.02618   0.01811  -0.1170   0.7934   0.0283
  -9.000  -0.3331   0.02536   0.01722  -0.1159   0.7893   0.0292
  -8.750  -0.3210   0.02449   0.01632  -0.1149   0.7857   0.0304
  -8.500  -0.3094   0.02370   0.01552  -0.1137   0.7813   0.0317
  -8.250  -0.2974   0.02295   0.01473  -0.1125   0.7771   0.0338
  -8.000  -0.2856   0.02222   0.01393  -0.1111   0.7732   0.0358
  -7.750  -0.2774   0.02139   0.01306  -0.1095   0.7698   0.0380
  -7.500  -0.2696   0.02075   0.01240  -0.1075   0.7658   0.0403
  -7.250  -0.2581   0.02009   0.01168  -0.1062   0.7619   0.0435
  -7.000  -0.2451   0.01932   0.01091  -0.1054   0.7582   0.0482
  -6.750  -0.2282   0.01867   0.01022  -0.1050   0.7550   0.0557
  -6.500  -0.2101   0.01805   0.00959  -0.1046   0.7521   0.0674
  -6.250  -0.1928   0.01737   0.00901  -0.1041   0.7484   0.0892
  -6.000  -0.1761   0.01639   0.00831  -0.1040   0.7447   0.1426
  -5.750  -0.1590   0.01489   0.00738  -0.1048   0.7413   0.2641
  -5.500  -0.1360   0.01369   0.00685  -0.1060   0.7385   0.4086
  -5.250  -0.1089   0.01373   0.00716  -0.1059   0.7358   0.4810
  -5.000  -0.0815   0.01390   0.00735  -0.1058   0.7321   0.5125
  -4.750  -0.0529   0.01417   0.00755  -0.1058   0.7286   0.5376
  -4.500  -0.0244   0.01469   0.00803  -0.1055   0.7255   0.5590
  -4.250   0.0047   0.01508   0.00831  -0.1055   0.7227   0.5728
  -4.000   0.0327   0.01535   0.00852  -0.1052   0.7202   0.5771
  -3.750   0.0597   0.01541   0.00853  -0.1051   0.7164   0.5817
  -3.500   0.0892   0.01529   0.00826  -0.1060   0.7128   0.5878
  -3.250   0.1167   0.01537   0.00830  -0.1058   0.7096   0.5901
  -3.000   0.1451   0.01543   0.00829  -0.1059   0.7068   0.5926
  -2.750   0.1744   0.01544   0.00821  -0.1062   0.7042   0.5957
  -2.500   0.2018   0.01540   0.00813  -0.1065   0.7001   0.5996
  -2.250   0.2313   0.01529   0.00791  -0.1073   0.6963   0.6039
  -2.000   0.2590   0.01532   0.00791  -0.1073   0.6929   0.6057
  -1.750   0.2876   0.01533   0.00787  -0.1074   0.6900   0.6077
  -1.500   0.3156   0.01535   0.00785  -0.1076   0.6866   0.6101
  -1.250   0.3429   0.01534   0.00784  -0.1077   0.6823   0.6127
  -1.000   0.3719   0.01529   0.00773  -0.1083   0.6784   0.6158
  -0.750   0.4028   0.01518   0.00752  -0.1093   0.6751   0.6193
  -0.500   0.4318   0.01516   0.00745  -0.1096   0.6722   0.6209
  -0.250   0.4576   0.01520   0.00754  -0.1094   0.6673   0.6225
   0.000   0.4851   0.01521   0.00756  -0.1095   0.6631   0.6243
   0.250   0.5137   0.01519   0.00752  -0.1098   0.6596   0.6263
   0.500   0.5432   0.01516   0.00744  -0.1103   0.6564   0.6284
   0.750   0.5700   0.01518   0.00750  -0.1104   0.6510   0.6309
   1.000   0.5989   0.01516   0.00745  -0.1109   0.6465   0.6336
   1.250   0.6294   0.01509   0.00731  -0.1117   0.6426   0.6360
   1.500   0.6562   0.01511   0.00738  -0.1117   0.6380   0.6373
   1.750   0.6826   0.01515   0.00747  -0.1116   0.6327   0.6389
   2.000   0.7105   0.01516   0.00748  -0.1117   0.6283   0.6406
   2.250   0.7387   0.01517   0.00750  -0.1119   0.6241   0.6424
   2.500   0.7651   0.01523   0.00761  -0.1119   0.6183   0.6443
   2.750   0.7933   0.01523   0.00763  -0.1122   0.6135   0.6462
   3.000   0.8222   0.01525   0.00762  -0.1127   0.6089   0.6486
   3.250   0.8491   0.01531   0.00773  -0.1128   0.6024   0.6511
   3.500   0.8771   0.01532   0.00774  -0.1131   0.5968   0.6529
   3.750   0.9032   0.01538   0.00786  -0.1129   0.5907   0.6543
   4.000   0.9291   0.01545   0.00799  -0.1128   0.5843   0.6558
   4.250   0.9567   0.01549   0.00803  -0.1128   0.5788   0.6574
   4.500   0.9813   0.01559   0.00822  -0.1125   0.5705   0.6592
   4.750   1.0084   0.01564   0.00825  -0.1125   0.5635   0.6613
   5.000   1.0328   0.01576   0.00844  -0.1121   0.5540   0.6636
   5.250   1.0587   0.01586   0.00853  -0.1120   0.5453   0.6660
   5.500   1.0839   0.01599   0.00867  -0.1118   0.5361   0.6681
   5.750   1.1079   0.01613   0.00888  -0.1113   0.5280   0.6696
   6.000   1.1316   0.01629   0.00909  -0.1108   0.5196   0.6711
   6.250   1.1545   0.01648   0.00935  -0.1102   0.5108   0.6728
   6.500   1.1776   0.01668   0.00958  -0.1095   0.5018   0.6747
   6.750   1.1988   0.01691   0.00988  -0.1086   0.4912   0.6769
   7.000   1.2197   0.01716   0.01017  -0.1077   0.4801   0.6794
   7.250   1.2396   0.01745   0.01045  -0.1065   0.4682   0.6819
   7.750   1.2734   0.01809   0.01118  -0.1033   0.4427   0.6859
   8.000   1.2863   0.01845   0.01159  -0.1010   0.4298   0.6877
   8.250   1.2980   0.01890   0.01207  -0.0986   0.4159   0.6897
   8.500   1.3074   0.01948   0.01266  -0.0959   0.3995   0.6919
   8.750   1.3143   0.02019   0.01335  -0.0931   0.3811   0.6944
   9.000   1.3189   0.02108   0.01419  -0.0901   0.3620   0.6971
   9.250   1.3223   0.02213   0.01519  -0.0873   0.3419   0.6999
   9.500   1.3235   0.02336   0.01639  -0.0845   0.3207   0.7020
   9.750   1.3222   0.02486   0.01782  -0.0816   0.2993   0.7042
  10.000   1.3224   0.02644   0.01937  -0.0793   0.2779   0.7066
  10.250   1.3225   0.02815   0.02103  -0.0771   0.2578   0.7090
  10.500   1.3231   0.02996   0.02279  -0.0752   0.2398   0.7116
  10.750   1.3243   0.03182   0.02461  -0.0735   0.2234   0.7142
  11.000   1.3262   0.03371   0.02647  -0.0721   0.2074   0.7167
  11.250   1.3281   0.03562   0.02839  -0.0706   0.1923   0.7190
  11.500   1.3297   0.03765   0.03041  -0.0693   0.1784   0.7217
  11.750   1.3326   0.03966   0.03243  -0.0682   0.1650   0.7247
  12.000   1.3358   0.04172   0.03451  -0.0673   0.1518   0.7279
  12.250   1.3386   0.04391   0.03671  -0.0665   0.1387   0.7311
  12.500   1.3407   0.04621   0.03903  -0.0657   0.1262   0.7338
  12.750   1.3425   0.04862   0.04146  -0.0650   0.1145   0.7366
  13.000   1.3442   0.05115   0.04400  -0.0645   0.1037   0.7397
  13.250   1.3455   0.05382   0.04668  -0.0641   0.0936   0.7431
  13.500   1.3475   0.05650   0.04938  -0.0639   0.0841   0.7466
  13.750   1.3495   0.05923   0.05217  -0.0637   0.0757   0.7499
  14.000   1.3500   0.06220   0.05519  -0.0636   0.0685   0.7533
  14.250   1.3512   0.06516   0.05822  -0.0636   0.0622   0.7574
  14.500   1.3518   0.06830   0.06141  -0.0638   0.0573   0.7619
  14.750   1.3528   0.07142   0.06461  -0.0640   0.0528   0.7663
  15.000   1.3509   0.07497   0.06823  -0.0643   0.0493   0.7711
  15.250   1.3538   0.07799   0.07139  -0.0647   0.0462   0.7769
  15.500   1.3540   0.08141   0.07491  -0.0652   0.0435   0.7825
  15.750   1.3519   0.08518   0.07877  -0.0659   0.0412   0.7887
  16.250   1.3531   0.09212   0.08598  -0.0674   0.0372   0.8041
  16.500   1.3522   0.09585   0.08984  -0.0683   0.0353   0.8138
  16.750   1.3489   0.09992   0.09401  -0.0693   0.0337   0.8257
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