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FX S 03-182 AIRFOIL (fxs03182-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: FX S 03-182 AIRFOIL (fxs03182-il)
Reynolds number: 50,000
Max Cl/Cd: 16.18 at α=12°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxs03182-il-50000-n5.txt
Download as CSV file: xf-fxs03182-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX S 03-182 AIRFOIL                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.3714   0.11835   0.11188  -0.0678   1.0000   0.0350
 -12.500  -0.3870   0.11470   0.10839  -0.0672   1.0000   0.0345
 -12.250  -0.4086   0.11091   0.10473  -0.0661   1.0000   0.0344
 -12.000  -0.4183   0.10349   0.09733  -0.0707   0.9952   0.0331
 -11.750  -0.4354   0.09358   0.08739  -0.0785   0.9873   0.0322
 -11.500  -0.4654   0.08348   0.07707  -0.0864   0.9786   0.0307
 -11.250  -0.4948   0.07517   0.06839  -0.0924   0.9691   0.0296
 -11.000  -0.5089   0.06994   0.06284  -0.0956   0.9587   0.0292
 -10.750  -0.5118   0.06620   0.05890  -0.0980   0.9501   0.0299
 -10.500  -0.5118   0.06281   0.05529  -0.1001   0.9418   0.0308
 -10.250  -0.5141   0.05980   0.05201  -0.1008   0.9323   0.0314
 -10.000  -0.5085   0.05669   0.04857  -0.1023   0.9258   0.0330
  -9.750  -0.5088   0.05430   0.04586  -0.1012   0.9159   0.0341
  -9.500  -0.4912   0.05101   0.04201  -0.1023   0.9112   0.0360
  -9.250  -0.4775   0.04860   0.03907  -0.1009   0.9033   0.0380
  -9.000  -0.4362   0.04605   0.03650  -0.1029   0.9009   0.0421
  -8.750  -0.3971   0.04417   0.03437  -0.1044   0.8984   0.0520
  -8.500  -0.3856   0.04334   0.03326  -0.1032   0.8907   0.0611
  -8.250  -0.3582   0.04218   0.03200  -0.1036   0.8863   0.0742
  -8.000  -0.3219   0.04110   0.03090  -0.1045   0.8835   0.0867
  -7.750  -0.3096   0.04052   0.03032  -0.1024   0.8764   0.0953
  -7.500  -0.2916   0.03967   0.02943  -0.1014   0.8712   0.1068
  -7.250  -0.2798   0.03889   0.02862  -0.0997   0.8658   0.1172
  -7.000  -0.2812   0.03835   0.02811  -0.0962   0.8582   0.1269
  -6.750  -0.2760   0.03721   0.02709  -0.0943   0.8537   0.1470
  -6.500  -0.2948   0.03700   0.02700  -0.0883   0.8446   0.1596
  -6.250  -0.2992   0.03551   0.02589  -0.0857   0.8397   0.2022
  -6.000  -0.3215   0.03511   0.02575  -0.0793   0.8310   0.2307
  -5.750  -0.2874   0.03795   0.03022  -0.0730   0.8289   0.4826
  -5.500  -0.2870   0.03748   0.02945  -0.0707   0.8248   0.5329
  -5.250  -0.3140   0.03744   0.02941  -0.0638   0.8165   0.5515
  -5.000  -0.3000   0.03836   0.03002  -0.0611   0.8128   0.5862
  -4.500  -0.2798   0.04237   0.03376  -0.0501   0.8040   0.6479
  -4.250  -0.2532   0.04451   0.03571  -0.0462   0.8012   0.6744
  -4.000  -0.2295   0.04525   0.03623  -0.0443   0.7987   0.6911
  -3.750  -0.2061   0.04523   0.03593  -0.0438   0.7965   0.7014
  -3.500  -0.2349   0.04532   0.03602  -0.0362   0.7895   0.7119
  -3.250  -0.2153   0.04550   0.03601  -0.0348   0.7863   0.7178
  -3.000  -0.2053   0.04517   0.03550  -0.0333   0.7835   0.7269
  -2.750  -0.1786   0.04516   0.03528  -0.0333   0.7817   0.7318
  -2.500  -0.1990   0.04522   0.03530  -0.0275   0.7759   0.7400
  -2.250  -0.1852   0.04528   0.03522  -0.0258   0.7724   0.7448
  -2.000  -0.1678   0.04521   0.03497  -0.0250   0.7698   0.7506
  -1.750  -0.1489   0.04500   0.03458  -0.0248   0.7676   0.7567
  -1.500  -0.1456   0.04525   0.03476  -0.0219   0.7637   0.7611
  -1.250  -0.1387   0.04529   0.03470  -0.0200   0.7597   0.7663
  -1.000  -0.1224   0.04523   0.03449  -0.0197   0.7567   0.7709
  -0.750  -0.1002   0.04530   0.03442  -0.0195   0.7545   0.7743
  -0.500  -0.0744   0.04531   0.03430  -0.0201   0.7525   0.7779
  -0.250  -0.0749   0.04560   0.03453  -0.0177   0.7475   0.7829
   0.000  -0.0592   0.04578   0.03463  -0.0171   0.7442   0.7863
   0.250  -0.0380   0.04596   0.03470  -0.0171   0.7414   0.7895
   0.500  -0.0115   0.04608   0.03473  -0.0179   0.7390   0.7926
   0.750   0.0019   0.04642   0.03500  -0.0174   0.7352   0.7960
   1.000   0.0163   0.04677   0.03529  -0.0172   0.7311   0.7995
   1.250   0.0369   0.04706   0.03552  -0.0170   0.7278   0.8022
   1.500   0.0640   0.04729   0.03570  -0.0179   0.7251   0.8049
   1.750   0.0817   0.04772   0.03609  -0.0178   0.7212   0.8078
   2.000   0.0967   0.04822   0.03655  -0.0177   0.7163   0.8111
   2.250   0.1225   0.04859   0.03689  -0.0187   0.7127   0.8143
   2.500   0.1509   0.04891   0.03719  -0.0196   0.7100   0.8169
   2.750   0.1604   0.04956   0.03785  -0.0185   0.7043   0.8199
   3.000   0.1817   0.05008   0.03837  -0.0190   0.6998   0.8228
   3.250   0.2114   0.05051   0.03880  -0.0205   0.6965   0.8261
   3.500   0.2289   0.05117   0.03948  -0.0205   0.6916   0.8295
   3.750   0.2445   0.05180   0.04015  -0.0201   0.6861   0.8327
   4.000   0.2731   0.05222   0.04061  -0.0211   0.6823   0.8360
   4.250   0.2905   0.05297   0.04139  -0.0213   0.6765   0.8395
   4.500   0.3122   0.05364   0.04212  -0.0219   0.6706   0.8430
   4.750   0.3416   0.05399   0.04254  -0.0227   0.6669   0.8464
   5.000   0.3506   0.05488   0.04351  -0.0218   0.6589   0.8505
   5.250   0.3779   0.05543   0.04413  -0.0228   0.6541   0.8549
   5.500   0.3970   0.05617   0.04497  -0.0229   0.6480   0.8590
   5.750   0.4148   0.05687   0.04577  -0.0227   0.6413   0.8633
   6.000   0.4483   0.05721   0.04621  -0.0241   0.6375   0.8678
   6.250   0.4566   0.05824   0.04734  -0.0233   0.6275   0.8728
   6.500   0.4893   0.05835   0.04761  -0.0241   0.6232   0.8780
   6.750   0.4976   0.05939   0.04876  -0.0233   0.6128   0.8842
   7.000   0.5305   0.05949   0.04902  -0.0241   0.6086   0.8905
   7.250   0.5369   0.06066   0.05034  -0.0231   0.5979   0.8978
   7.750   0.5797   0.06165   0.05167  -0.0232   0.5820   0.9140
   8.000   0.5937   0.06235   0.05254  -0.0227   0.5713   0.9240
   8.250   0.6302   0.06205   0.05248  -0.0238   0.5656   0.9368
   8.500   0.6447   0.06298   0.05361  -0.0241   0.5534   0.9550
   8.750   0.6620   0.06352   0.05434  -0.0246   0.5411   1.0000
   9.000   0.6854   0.06410   0.05509  -0.0256   0.5292   1.0000
   9.500   0.7488   0.06387   0.05529  -0.0279   0.5088   1.0000
   9.750   0.7715   0.06412   0.05572  -0.0284   0.4949   1.0000
  10.000   0.7948   0.06425   0.05606  -0.0287   0.4809   1.0000
  10.250   0.8204   0.06396   0.05597  -0.0289   0.4663   1.0000
  10.500   0.8475   0.06332   0.05559  -0.0289   0.4513   1.0000
  10.750   0.8607   0.06398   0.05643  -0.0285   0.4308   1.0000
  11.000   0.8869   0.06313   0.05579  -0.0281   0.4126   1.0000
  11.250   0.9171   0.06178   0.05462  -0.0275   0.3920   1.0000
  11.500   0.9386   0.06133   0.05426  -0.0267   0.3605   1.0000
  11.750   0.9648   0.06028   0.05308  -0.0256   0.3193   1.0000
  12.000   0.9814   0.06066   0.05325  -0.0247   0.2779   1.0000
  12.250   0.9878   0.06256   0.05496  -0.0241   0.2418   1.0000
  12.500   0.9920   0.06485   0.05705  -0.0236   0.2118   1.0000
  12.750   0.9945   0.06750   0.05954  -0.0233   0.1860   1.0000
  13.000   0.9970   0.07024   0.06213  -0.0231   0.1655   1.0000
  13.250   1.0004   0.07302   0.06482  -0.0230   0.1473   1.0000
  13.500   1.0044   0.07579   0.06751  -0.0230   0.1319   1.0000
  13.750   1.0083   0.07864   0.07032  -0.0231   0.1181   1.0000
  14.000   1.0115   0.08165   0.07332  -0.0235   0.1057   1.0000
  14.250   1.0142   0.08470   0.07631  -0.0241   0.0959   1.0000
  14.500   1.0204   0.08750   0.07929  -0.0245   0.0868   1.0000
  14.750   1.0282   0.08999   0.08179  -0.0247   0.0808   1.0000
  15.000   1.0379   0.09244   0.08447  -0.0249   0.0747   1.0000
  15.250   1.0462   0.09485   0.08687  -0.0252   0.0702   1.0000
  15.500   1.0535   0.09778   0.09008  -0.0258   0.0654   1.0000
  15.750   1.0584   0.10082   0.09325  -0.0266   0.0613   1.0000
  16.000   1.0631   0.10380   0.09621  -0.0275   0.0576   1.0000
  16.250   1.0639   0.10788   0.10067  -0.0287   0.0542   1.0000
  16.500   1.0631   0.11204   0.10506  -0.0303   0.0512   1.0000
  16.750   1.0633   0.11586   0.10897  -0.0320   0.0483   1.0000
  17.000   1.0652   0.11951   0.11265  -0.0334   0.0460   1.0000
  17.250   1.0570   0.12552   0.11905  -0.0362   0.0445   1.0000
  17.500   1.0469   0.13205   0.12590  -0.0395   0.0434   1.0000
  17.750   1.0332   0.13961   0.13373  -0.0438   0.0425   1.0000
  18.000   1.0155   0.14851   0.14288  -0.0490   0.0424   1.0000
  18.250   0.9922   0.15973   0.15429  -0.0558   0.0433   1.0000
  18.500   0.9700   0.17179   0.16642  -0.0630   0.0446   1.0000
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