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FX 61-184 AIRFOIL (fx61184-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 61-184 AIRFOIL (fx61184-il)
Reynolds number: 1,000,000
Max Cl/Cd: 120.66 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx61184-il-1000000-n5.txt
Download as CSV file: xf-fx61184-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.8997   0.10700   0.10411  -0.0550   1.0000   0.0048
 -19.500  -0.9229   0.09902   0.09599  -0.0593   1.0000   0.0048
 -19.250  -0.9447   0.09160   0.08842  -0.0632   1.0000   0.0047
 -19.000  -0.9605   0.08534   0.08204  -0.0665   1.0000   0.0047
 -18.750  -0.9684   0.08053   0.07713  -0.0689   1.0000   0.0050
 -18.500  -0.9817   0.07504   0.07153  -0.0716   1.0000   0.0048
 -18.250  -0.9870   0.07088   0.06727  -0.0736   1.0000   0.0049
 -18.000  -0.9918   0.06691   0.06320  -0.0753   1.0000   0.0049
 -17.750  -0.9928   0.06358   0.05979  -0.0767   1.0000   0.0051
 -17.500  -0.9954   0.06010   0.05622  -0.0780   1.0000   0.0051
 -17.250  -0.9929   0.05705   0.05309  -0.0796   0.9999   0.0053
 -17.000  -0.9783   0.05358   0.04953  -0.0838   0.9979   0.0053
 -16.750  -0.9584   0.05026   0.04612  -0.0885   0.9386   0.0056
 -16.500  -0.9140   0.04708   0.04265  -0.0983   0.8884   0.0059
 -16.250  -0.8829   0.04470   0.03999  -0.1044   0.8453   0.0060
 -16.000  -0.8644   0.04248   0.03761  -0.1078   0.8252   0.0061
 -15.750  -0.8468   0.04086   0.03586  -0.1098   0.8116   0.0065
 -15.250  -0.8174   0.03768   0.03248  -0.1124   0.7939   0.0069
 -14.750  -0.7897   0.03474   0.02935  -0.1143   0.7811   0.0071
 -14.500  -0.7762   0.03337   0.02792  -0.1149   0.7753   0.0073
 -14.000  -0.7495   0.03079   0.02520  -0.1159   0.7656   0.0077
 -13.750  -0.7340   0.02978   0.02416  -0.1162   0.7615   0.0080
 -13.500  -0.7189   0.02878   0.02311  -0.1164   0.7575   0.0082
 -13.000  -0.6902   0.02676   0.02097  -0.1164   0.7508   0.0085
 -12.750  -0.6738   0.02595   0.02012  -0.1164   0.7474   0.0089
 -12.500  -0.6589   0.02505   0.01916  -0.1163   0.7440   0.0091
 -12.250  -0.6430   0.02425   0.01830  -0.1161   0.7405   0.0093
 -12.000  -0.6261   0.02353   0.01753  -0.1159   0.7376   0.0095
 -11.750  -0.6119   0.02266   0.01662  -0.1155   0.7351   0.0096
 -11.500  -0.5984   0.02176   0.01569  -0.1150   0.7326   0.0100
 -11.250  -0.5831   0.02100   0.01491  -0.1146   0.7299   0.0103
 -11.000  -0.5678   0.02027   0.01414  -0.1140   0.7269   0.0105
 -10.750  -0.5517   0.01961   0.01345  -0.1134   0.7241   0.0108
 -10.500  -0.5358   0.01897   0.01277  -0.1128   0.7213   0.0111
 -10.250  -0.5179   0.01843   0.01221  -0.1123   0.7190   0.0118
 -10.000  -0.5027   0.01776   0.01151  -0.1115   0.7163   0.0120
  -9.750  -0.4871   0.01714   0.01086  -0.1106   0.7136   0.0122
  -9.500  -0.4745   0.01642   0.01011  -0.1094   0.7109   0.0127
  -9.250  -0.4614   0.01582   0.00950  -0.1081   0.7082   0.0134
  -9.000  -0.4508   0.01526   0.00891  -0.1063   0.7057   0.0137
  -8.750  -0.4335   0.01470   0.00831  -0.1058   0.7033   0.0142
  -8.500  -0.4134   0.01416   0.00775  -0.1058   0.7012   0.0147
  -8.250  -0.3916   0.01367   0.00722  -0.1058   0.6988   0.0152
  -8.000  -0.3691   0.01325   0.00677  -0.1058   0.6962   0.0157
  -7.750  -0.3460   0.01286   0.00636  -0.1057   0.6936   0.0165
  -7.500  -0.3218   0.01253   0.00601  -0.1057   0.6912   0.0176
  -7.250  -0.2968   0.01224   0.00568  -0.1058   0.6886   0.0187
  -7.000  -0.2710   0.01193   0.00537  -0.1060   0.6864   0.0203
  -6.750  -0.2447   0.01163   0.00508  -0.1063   0.6840   0.0225
  -6.500  -0.2180   0.01136   0.00480  -0.1066   0.6814   0.0252
  -6.250  -0.1910   0.01110   0.00454  -0.1069   0.6788   0.0289
  -6.000  -0.1638   0.01084   0.00429  -0.1072   0.6762   0.0342
  -5.750  -0.1364   0.01059   0.00406  -0.1076   0.6736   0.0415
  -5.500  -0.1085   0.01033   0.00382  -0.1081   0.6714   0.0518
  -5.250  -0.0801   0.01004   0.00359  -0.1087   0.6691   0.0668
  -5.000  -0.0516   0.00967   0.00333  -0.1095   0.6665   0.0943
  -4.750  -0.0228   0.00919   0.00302  -0.1104   0.6636   0.1428
  -4.500   0.0066   0.00864   0.00270  -0.1116   0.6607   0.2090
  -4.250   0.0375   0.00784   0.00228  -0.1134   0.6579   0.3150
  -4.000   0.0700   0.00710   0.00191  -0.1155   0.6553   0.4246
  -3.750   0.1015   0.00680   0.00181  -0.1167   0.6522   0.4846
  -3.500   0.1321   0.00672   0.00181  -0.1174   0.6487   0.5211
  -3.250   0.1621   0.00673   0.00181  -0.1179   0.6453   0.5343
  -3.000   0.1918   0.00675   0.00179  -0.1184   0.6421   0.5418
  -2.750   0.2217   0.00676   0.00178  -0.1189   0.6391   0.5459
  -2.500   0.2517   0.00676   0.00177  -0.1194   0.6355   0.5499
  -2.250   0.2815   0.00678   0.00175  -0.1199   0.6317   0.5533
  -2.000   0.3111   0.00681   0.00172  -0.1203   0.6281   0.5559
  -1.750   0.3406   0.00683   0.00172  -0.1208   0.6245   0.5583
  -1.500   0.3704   0.00683   0.00172  -0.1213   0.6205   0.5606
  -1.250   0.4000   0.00686   0.00173  -0.1217   0.6158   0.5631
  -1.000   0.4291   0.00690   0.00173  -0.1220   0.6111   0.5656
  -0.750   0.4587   0.00693   0.00174  -0.1225   0.6064   0.5679
  -0.500   0.4881   0.00696   0.00175  -0.1229   0.6013   0.5699
  -0.250   0.5171   0.00702   0.00176  -0.1233   0.5962   0.5715
   0.000   0.5465   0.00704   0.00178  -0.1237   0.5915   0.5732
   0.250   0.5757   0.00707   0.00181  -0.1241   0.5860   0.5749
   0.500   0.6045   0.00713   0.00184  -0.1244   0.5807   0.5766
   0.750   0.6336   0.00717   0.00188  -0.1248   0.5757   0.5782
   1.000   0.6625   0.00723   0.00193  -0.1251   0.5695   0.5798
   1.250   0.6908   0.00731   0.00198  -0.1253   0.5629   0.5815
   1.500   0.7197   0.00737   0.00203  -0.1256   0.5560   0.5831
   1.750   0.7477   0.00747   0.00209  -0.1258   0.5489   0.5845
   2.000   0.7764   0.00754   0.00215  -0.1261   0.5427   0.5859
   2.250   0.8043   0.00764   0.00222  -0.1263   0.5350   0.5872
   2.500   0.8325   0.00772   0.00230  -0.1265   0.5273   0.5887
   3.000   0.8873   0.00796   0.00249  -0.1267   0.5065   0.5915
   3.250   0.9146   0.00808   0.00260  -0.1268   0.4977   0.5929
   3.500   0.9421   0.00820   0.00271  -0.1269   0.4899   0.5945
   3.750   0.9693   0.00833   0.00283  -0.1270   0.4820   0.5960
   4.000   0.9961   0.00847   0.00296  -0.1269   0.4724   0.5975
   4.250   1.0233   0.00860   0.00308  -0.1270   0.4650   0.5988
   4.500   1.0498   0.00876   0.00323  -0.1269   0.4559   0.6001
   4.750   1.0762   0.00892   0.00337  -0.1269   0.4457   0.6014
   5.000   1.1016   0.00913   0.00354  -0.1266   0.4331   0.6025
   5.250   1.1261   0.00937   0.00373  -0.1262   0.4183   0.6035
   5.500   1.1505   0.00961   0.00395  -0.1258   0.4041   0.6052
   5.750   1.1743   0.00987   0.00417  -0.1253   0.3892   0.6068
   6.000   1.1972   0.01017   0.00442  -0.1247   0.3724   0.6083
   6.250   1.2192   0.01051   0.00471  -0.1239   0.3543   0.6098
   6.500   1.2397   0.01089   0.00502  -0.1228   0.3345   0.6112
   6.750   1.2581   0.01135   0.00538  -0.1214   0.3118   0.6127
   7.000   1.2726   0.01196   0.00584  -0.1193   0.2830   0.6141
   7.250   1.2859   0.01252   0.00629  -0.1170   0.2569   0.6154
   7.500   1.2931   0.01317   0.00680  -0.1136   0.2301   0.6168
   7.750   1.2995   0.01392   0.00741  -0.1102   0.2040   0.6180
   8.000   1.3077   0.01463   0.00802  -0.1072   0.1835   0.6192
   8.250   1.3198   0.01521   0.00857  -0.1050   0.1716   0.6208
   8.500   1.3308   0.01586   0.00920  -0.1027   0.1600   0.6226
   8.750   1.3398   0.01664   0.00994  -0.1002   0.1467   0.6242
   9.000   1.3464   0.01758   0.01083  -0.0977   0.1313   0.6257
   9.250   1.3530   0.01862   0.01182  -0.0953   0.1175   0.6273
   9.500   1.3593   0.01976   0.01292  -0.0931   0.1045   0.6288
   9.750   1.3640   0.02108   0.01419  -0.0909   0.0899   0.6304
  10.000   1.3692   0.02246   0.01552  -0.0889   0.0769   0.6319
  10.250   1.3754   0.02385   0.01686  -0.0872   0.0664   0.6333
  10.500   1.3821   0.02525   0.01824  -0.0856   0.0579   0.6347
  10.750   1.3901   0.02661   0.01959  -0.0842   0.0513   0.6359
  11.000   1.3990   0.02794   0.02093  -0.0830   0.0454   0.6378
  11.250   1.4060   0.02944   0.02245  -0.0817   0.0397   0.6397
  11.500   1.4127   0.03101   0.02401  -0.0804   0.0343   0.6415
  11.750   1.4213   0.03246   0.02549  -0.0794   0.0309   0.6433
  12.000   1.4288   0.03404   0.02708  -0.0783   0.0278   0.6450
  12.250   1.4369   0.03559   0.02867  -0.0774   0.0252   0.6467
  12.500   1.4457   0.03714   0.03025  -0.0766   0.0233   0.6485
  12.750   1.4524   0.03891   0.03204  -0.0757   0.0211   0.6500
  13.000   1.4611   0.04054   0.03372  -0.0751   0.0195   0.6515
  13.250   1.4687   0.04233   0.03555  -0.0744   0.0182   0.6532
  13.500   1.4763   0.04418   0.03744  -0.0739   0.0170   0.6551
  13.750   1.4851   0.04596   0.03928  -0.0734   0.0162   0.6573
  14.000   1.4929   0.04786   0.04124  -0.0730   0.0153   0.6596
  14.250   1.4997   0.04991   0.04334  -0.0726   0.0143   0.6618
  14.500   1.5059   0.05209   0.04556  -0.0723   0.0134   0.6640
  14.750   1.5139   0.05411   0.04765  -0.0721   0.0129   0.6661
  15.000   1.5203   0.05635   0.04995  -0.0720   0.0122   0.6679
  15.250   1.5258   0.05873   0.05237  -0.0719   0.0112   0.6700
  15.500   1.5304   0.06128   0.05498  -0.0719   0.0104   0.6722
  15.750   1.5361   0.06376   0.05754  -0.0720   0.0096   0.6746
  16.000   1.5404   0.06644   0.06027  -0.0721   0.0086   0.6770
  16.250   1.5435   0.06932   0.06322  -0.0724   0.0077   0.6794
  16.500   1.5453   0.07241   0.06636  -0.0727   0.0062   0.6817
  16.750   1.5437   0.07603   0.07002  -0.0732   0.0042   0.6837
  17.000   1.5421   0.07975   0.07381  -0.0738   0.0033   0.6859
  17.250   1.5424   0.08328   0.07744  -0.0745   0.0030   0.6886
  17.500   1.5424   0.08688   0.08112  -0.0753   0.0027   0.6914
  17.750   1.5420   0.09059   0.08493  -0.0762   0.0025   0.6945
  18.000   1.5407   0.09452   0.08894  -0.0773   0.0024   0.6975
  18.500   1.5401   0.10220   0.09682  -0.0797   0.0022   0.7041
  18.750   1.5389   0.10623   0.10095  -0.0811   0.0021   0.7078
  19.000   1.5370   0.11042   0.10524  -0.0826   0.0020   0.7115
  19.250   1.5352   0.11461   0.10953  -0.0842   0.0020   0.7151
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