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FX 66-182 AIRFOIL (fx66182-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 66-182 AIRFOIL (fx66182-il)
Reynolds number: 500,000
Max Cl/Cd: 104.36 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx66182-il-500000-n5.txt
Download as CSV file: xf-fx66182-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 66-182 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.4996   0.10973   0.10720  -0.0600   0.9264   0.0080
 -15.750  -0.6069   0.09232   0.08969  -0.0600   0.9545   0.0076
 -15.500  -0.6569   0.07693   0.07400  -0.0703   0.9471   0.0076
 -15.250  -0.6657   0.06294   0.05958  -0.0880   0.9226   0.0076
 -15.000  -0.6373   0.05295   0.04890  -0.1073   0.8463   0.0077
 -14.750  -0.6457   0.04965   0.04520  -0.1081   0.7869   0.0077
 -14.500  -0.6553   0.04639   0.04165  -0.1087   0.7549   0.0078
 -14.250  -0.6627   0.04334   0.03835  -0.1091   0.7342   0.0079
 -14.000  -0.6650   0.04090   0.03570  -0.1093   0.7169   0.0080
 -13.750  -0.6661   0.03865   0.03327  -0.1093   0.7023   0.0080
 -13.500  -0.6674   0.03641   0.03083  -0.1091   0.6902   0.0082
 -13.250  -0.6653   0.03454   0.02881  -0.1088   0.6788   0.0081
 -13.000  -0.6615   0.03285   0.02702  -0.1085   0.6689   0.0083
 -12.750  -0.6552   0.03142   0.02548  -0.1081   0.6594   0.0085
 -12.500  -0.6475   0.03010   0.02405  -0.1076   0.6511   0.0086
 -12.250  -0.6389   0.02887   0.02271  -0.1071   0.6433   0.0088
 -12.000  -0.6303   0.02765   0.02138  -0.1064   0.6363   0.0089
 -11.750  -0.6193   0.02665   0.02029  -0.1058   0.6298   0.0091
 -11.500  -0.6085   0.02561   0.01914  -0.1051   0.6242   0.0093
 -11.250  -0.5975   0.02462   0.01805  -0.1043   0.6189   0.0097
 -11.000  -0.5872   0.02361   0.01693  -0.1034   0.6143   0.0099
 -10.750  -0.5763   0.02266   0.01589  -0.1023   0.6100   0.0102
 -10.500  -0.5675   0.02170   0.01482  -0.1009   0.6057   0.0105
 -10.250  -0.5582   0.02099   0.01401  -0.0990   0.6016   0.0108
 -10.000  -0.5464   0.02051   0.01348  -0.0972   0.5979   0.0111
  -9.750  -0.5296   0.02003   0.01294  -0.0961   0.5941   0.0115
  -9.500  -0.5119   0.01955   0.01240  -0.0951   0.5903   0.0119
  -9.250  -0.4934   0.01908   0.01184  -0.0942   0.5869   0.0127
  -8.750  -0.4548   0.01812   0.01071  -0.0924   0.5813   0.0141
  -8.500  -0.4338   0.01771   0.01027  -0.0918   0.5786   0.0147
  -8.250  -0.4117   0.01736   0.00987  -0.0913   0.5758   0.0157
  -8.000  -0.3899   0.01696   0.00940  -0.0907   0.5731   0.0166
  -7.750  -0.3667   0.01668   0.00902  -0.0902   0.5705   0.0174
  -7.250  -0.3247   0.01565   0.00790  -0.0888   0.5658   0.0189
  -7.000  -0.3014   0.01526   0.00747  -0.0884   0.5632   0.0197
  -6.750  -0.2776   0.01492   0.00708  -0.0881   0.5606   0.0205
  -6.500  -0.2533   0.01462   0.00672  -0.0877   0.5583   0.0213
  -6.250  -0.2288   0.01432   0.00636  -0.0874   0.5562   0.0224
  -6.000  -0.2051   0.01395   0.00596  -0.0871   0.5541   0.0240
  -5.500  -0.1544   0.01343   0.00534  -0.0867   0.5504   0.0259
  -5.250  -0.1284   0.01319   0.00506  -0.0866   0.5485   0.0267
  -5.000  -0.1021   0.01297   0.00480  -0.0865   0.5463   0.0275
  -4.750  -0.0760   0.01274   0.00455  -0.0864   0.5441   0.0294
  -4.500  -0.0497   0.01254   0.00433  -0.0863   0.5419   0.0324
  -4.250  -0.0234   0.01233   0.00410  -0.0862   0.5400   0.0396
  -4.000   0.0023   0.01205   0.00388  -0.0862   0.5382   0.0599
  -3.750   0.0276   0.01171   0.00366  -0.0861   0.5365   0.0981
  -3.500   0.0532   0.01132   0.00344  -0.0861   0.5349   0.1480
  -3.250   0.0778   0.01077   0.00318  -0.0860   0.5331   0.2291
  -3.000   0.1023   0.01018   0.00292  -0.0860   0.5311   0.3241
  -2.750   0.1265   0.00961   0.00273  -0.0859   0.5290   0.4370
  -2.500   0.1533   0.00948   0.00278  -0.0858   0.5272   0.5012
  -2.250   0.1814   0.00952   0.00284  -0.0859   0.5255   0.5313
  -2.000   0.2096   0.00960   0.00290  -0.0860   0.5237   0.5510
  -1.750   0.2379   0.00970   0.00294  -0.0862   0.5218   0.5622
  -1.500   0.2664   0.00975   0.00298  -0.0864   0.5201   0.5693
  -1.250   0.2951   0.00979   0.00300  -0.0866   0.5184   0.5753
  -1.000   0.3238   0.00985   0.00301  -0.0869   0.5167   0.5809
  -0.750   0.3523   0.00988   0.00305  -0.0871   0.5150   0.5848
  -0.500   0.3808   0.00991   0.00306  -0.0873   0.5132   0.5874
  -0.250   0.4093   0.00995   0.00306  -0.0876   0.5114   0.5901
   0.000   0.4377   0.01000   0.00306  -0.0878   0.5096   0.5929
   0.250   0.4661   0.01006   0.00307  -0.0880   0.5079   0.5954
   0.500   0.4943   0.01012   0.00309  -0.0883   0.5062   0.5975
   0.750   0.5228   0.01014   0.00314  -0.0885   0.5048   0.5995
   1.000   0.5512   0.01018   0.00319  -0.0888   0.5032   0.6014
   1.250   0.5795   0.01022   0.00324  -0.0890   0.5015   0.6036
   1.500   0.6078   0.01027   0.00329  -0.0893   0.4997   0.6058
   1.750   0.6360   0.01032   0.00334  -0.0895   0.4979   0.6079
   2.000   0.6642   0.01038   0.00338  -0.0897   0.4960   0.6099
   2.250   0.6922   0.01045   0.00343  -0.0900   0.4942   0.6121
   2.500   0.7200   0.01051   0.00350  -0.0901   0.4926   0.6140
   2.750   0.7479   0.01059   0.00358  -0.0903   0.4910   0.6158
   3.000   0.7758   0.01064   0.00368  -0.0905   0.4893   0.6177
   3.250   0.8036   0.01069   0.00378  -0.0907   0.4873   0.6199
   3.500   0.8313   0.01076   0.00387  -0.0909   0.4851   0.6222
   3.750   0.8589   0.01083   0.00397  -0.0911   0.4831   0.6245
   4.000   0.8864   0.01090   0.00406  -0.0912   0.4811   0.6265
   4.250   0.9138   0.01099   0.00416  -0.0914   0.4794   0.6284
   4.500   0.9411   0.01107   0.00427  -0.0915   0.4777   0.6303
   4.750   0.9682   0.01118   0.00440  -0.0916   0.4760   0.6324
   5.000   0.9954   0.01125   0.00456  -0.0917   0.4742   0.6349
   5.250   1.0224   0.01134   0.00471  -0.0918   0.4721   0.6374
   5.500   1.0493   0.01143   0.00486  -0.0919   0.4699   0.6399
   5.750   1.0759   0.01152   0.00499  -0.0919   0.4672   0.6422
   6.000   1.1019   0.01160   0.00510  -0.0918   0.4640   0.6444
   6.250   1.1276   0.01170   0.00524  -0.0916   0.4607   0.6467
   6.500   1.1533   0.01176   0.00541  -0.0915   0.4565   0.6491
   6.750   1.1781   0.01184   0.00554  -0.0912   0.4511   0.6519
   7.000   1.2024   0.01196   0.00567  -0.0907   0.4465   0.6550
   7.250   1.2276   0.01206   0.00586  -0.0905   0.4418   0.6582
   7.500   1.2518   0.01217   0.00605  -0.0901   0.4368   0.6611
   7.750   1.2745   0.01231   0.00623  -0.0895   0.4302   0.6641
   8.000   1.2971   0.01244   0.00644  -0.0888   0.4219   0.6674
   8.250   1.3180   0.01263   0.00665  -0.0878   0.4116   0.6709
   8.500   1.3325   0.01296   0.00693  -0.0857   0.3911   0.6744
   8.750   1.3354   0.01353   0.00738  -0.0816   0.3603   0.6780
   9.000   1.3241   0.01466   0.00829  -0.0753   0.3168   0.6821
   9.250   1.3081   0.01616   0.00959  -0.0690   0.2726   0.6867
   9.500   1.2844   0.01824   0.01147  -0.0625   0.2330   0.6915
   9.750   1.2679   0.02041   0.01357  -0.0580   0.2054   0.6971
  10.000   1.2514   0.02303   0.01614  -0.0544   0.1802   0.7033
  10.250   1.2374   0.02587   0.01894  -0.0517   0.1585   0.7097
  10.500   1.2251   0.02882   0.02187  -0.0495   0.1385   0.7171
  10.750   1.2137   0.03183   0.02487  -0.0477   0.1206   0.7255
  11.000   1.2014   0.03502   0.02804  -0.0460   0.1023   0.7358
  11.250   1.1944   0.03779   0.03085  -0.0447   0.0887   0.7495
  11.750   1.1733   0.04371   0.03701  -0.0415   0.0583   0.8488
  12.000   1.1792   0.04684   0.04025  -0.0434   0.0444   1.0000
  12.250   1.1776   0.04958   0.04298  -0.0429   0.0361   1.0000
  12.500   1.1784   0.05217   0.04557  -0.0425   0.0308   1.0000
  12.750   1.1816   0.05455   0.04797  -0.0422   0.0256   1.0000
  13.000   1.1814   0.05734   0.05074  -0.0420   0.0181   1.0000
  13.250   1.1840   0.05987   0.05328  -0.0418   0.0155   1.0000
  13.500   1.1867   0.06245   0.05589  -0.0417   0.0142   1.0000
  13.750   1.1905   0.06494   0.05842  -0.0417   0.0133   1.0000
  14.000   1.1941   0.06749   0.06102  -0.0417   0.0125   1.0000
  14.250   1.1991   0.06992   0.06351  -0.0418   0.0120   1.0000
  14.500   1.2048   0.07229   0.06595  -0.0419   0.0116   1.0000
  14.750   1.2088   0.07491   0.06864  -0.0421   0.0112   1.0000
  15.000   1.2130   0.07751   0.07130  -0.0423   0.0108   1.0000
  15.250   1.2161   0.08030   0.07414  -0.0426   0.0104   1.0000
  15.500   1.2188   0.08316   0.07707  -0.0430   0.0101   1.0000
  15.750   1.2184   0.08647   0.08045  -0.0434   0.0095   1.0000
  16.000   1.2227   0.08922   0.08327  -0.0439   0.0094   1.0000
  16.250   1.2289   0.09172   0.08584  -0.0443   0.0090   1.0000
  16.500   1.2325   0.09458   0.08877  -0.0449   0.0087   1.0000
  16.750   1.2356   0.09754   0.09180  -0.0455   0.0084   1.0000
  17.000   1.2395   0.10040   0.09472  -0.0462   0.0079   1.0000
  17.250   1.2412   0.10364   0.09803  -0.0470   0.0078   1.0000
  17.500   1.2435   0.10679   0.10123  -0.0478   0.0075   1.0000
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