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FX S 03-182 AIRFOIL (fxs03182-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX S 03-182 AIRFOIL (fxs03182-il)
Reynolds number: 500,000
Max Cl/Cd: 89.48 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxs03182-il-500000-n5.txt
Download as CSV file: xf-fxs03182-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.4842   0.10495   0.10246  -0.0706   0.9815   0.0030
 -15.000  -0.5284   0.08780   0.08507  -0.0804   0.9713   0.0029
 -14.750  -0.5465   0.07620   0.07323  -0.0903   0.9582   0.0029
 -14.500  -0.5506   0.06705   0.06382  -0.1003   0.9466   0.0028
 -14.250  -0.5480   0.05887   0.05533  -0.1107   0.9356   0.0028
 -14.000  -0.5395   0.05195   0.04807  -0.1205   0.9210   0.0028
 -13.750  -0.5297   0.04665   0.04240  -0.1278   0.9006   0.0028
 -13.500  -0.5246   0.04337   0.03882  -0.1306   0.8767   0.0028
 -13.250  -0.5242   0.04086   0.03606  -0.1311   0.8563   0.0028
 -13.000  -0.5235   0.03876   0.03373  -0.1309   0.8402   0.0028
 -12.750  -0.5234   0.03668   0.03143  -0.1302   0.8266   0.0028
 -12.500  -0.5207   0.03490   0.02946  -0.1295   0.8144   0.0028
 -12.250  -0.5183   0.03306   0.02741  -0.1284   0.8039   0.0029
 -12.000  -0.5100   0.03186   0.02608  -0.1277   0.7941   0.0028
 -11.750  -0.5031   0.03047   0.02454  -0.1267   0.7852   0.0028
 -11.500  -0.4946   0.02922   0.02315  -0.1257   0.7776   0.0028
 -11.250  -0.4865   0.02794   0.02172  -0.1246   0.7702   0.0029
 -11.000  -0.4751   0.02696   0.02064  -0.1237   0.7637   0.0029
 -10.750  -0.4647   0.02589   0.01945  -0.1226   0.7571   0.0029
 -10.500  -0.4540   0.02488   0.01832  -0.1214   0.7512   0.0030
 -10.250  -0.4418   0.02398   0.01734  -0.1204   0.7453   0.0030
 -10.000  -0.4300   0.02308   0.01634  -0.1191   0.7399   0.0031
  -9.750  -0.4171   0.02227   0.01544  -0.1180   0.7348   0.0031
  -9.500  -0.4039   0.02150   0.01459  -0.1169   0.7295   0.0031
  -9.250  -0.3917   0.02071   0.01370  -0.1155   0.7246   0.0032
  -9.000  -0.3775   0.02004   0.01297  -0.1144   0.7201   0.0033
  -8.750  -0.3641   0.01934   0.01220  -0.1131   0.7154   0.0033
  -8.500  -0.3503   0.01871   0.01149  -0.1118   0.7112   0.0033
  -8.250  -0.3366   0.01808   0.01079  -0.1104   0.7075   0.0034
  -8.000  -0.3221   0.01752   0.01018  -0.1091   0.7038   0.0035
  -7.750  -0.3106   0.01687   0.00946  -0.1073   0.7000   0.0037
  -7.500  -0.3044   0.01621   0.00870  -0.1046   0.6965   0.0039
  -7.250  -0.2917   0.01575   0.00818  -0.1029   0.6935   0.0040
  -7.000  -0.2750   0.01529   0.00766  -0.1018   0.6904   0.0041
  -6.750  -0.2576   0.01483   0.00712  -0.1007   0.6873   0.0046
  -6.500  -0.2373   0.01449   0.00673  -0.1000   0.6845   0.0047
  -6.250  -0.2165   0.01416   0.00631  -0.0994   0.6818   0.0051
  -6.000  -0.1941   0.01387   0.00595  -0.0989   0.6793   0.0054
  -5.750  -0.1726   0.01345   0.00554  -0.0985   0.6766   0.0075
  -5.500  -0.1488   0.01318   0.00527  -0.0983   0.6739   0.0143
  -5.250  -0.1238   0.01298   0.00504  -0.0982   0.6715   0.0162
  -5.000  -0.0988   0.01277   0.00481  -0.0982   0.6693   0.0187
  -4.750  -0.0730   0.01261   0.00459  -0.0982   0.6673   0.0205
  -4.500  -0.0474   0.01239   0.00438  -0.0983   0.6655   0.0255
  -4.250  -0.0215   0.01214   0.00418  -0.0985   0.6635   0.0363
  -4.000   0.0054   0.01200   0.00402  -0.0988   0.6615   0.0411
  -3.750   0.0313   0.01168   0.00379  -0.0990   0.6596   0.0677
  -3.500   0.0567   0.01119   0.00352  -0.0994   0.6577   0.1272
  -3.250   0.0821   0.01049   0.00317  -0.1001   0.6559   0.2282
  -3.000   0.1084   0.00901   0.00253  -0.1020   0.6542   0.4561
  -2.750   0.1377   0.00883   0.00260  -0.1028   0.6525   0.5435
  -2.500   0.1673   0.00888   0.00265  -0.1034   0.6508   0.5667
  -2.250   0.1967   0.00892   0.00268  -0.1039   0.6491   0.5773
  -2.000   0.2260   0.00896   0.00270  -0.1044   0.6474   0.5843
  -1.750   0.2555   0.00901   0.00273  -0.1049   0.6458   0.5918
  -1.500   0.2847   0.00908   0.00281  -0.1054   0.6442   0.6000
  -1.250   0.3143   0.00917   0.00285  -0.1060   0.6427   0.6084
  -1.000   0.3432   0.00923   0.00292  -0.1064   0.6413   0.6132
  -0.750   0.3724   0.00928   0.00296  -0.1069   0.6399   0.6166
  -0.500   0.4018   0.00934   0.00298  -0.1074   0.6386   0.6199
   0.000   0.4604   0.00942   0.00303  -0.1085   0.6357   0.6249
   0.250   0.4893   0.00944   0.00307  -0.1090   0.6342   0.6260
   0.500   0.5184   0.00947   0.00311  -0.1095   0.6328   0.6271
   0.750   0.5474   0.00950   0.00316  -0.1101   0.6314   0.6282
   1.000   0.5761   0.00952   0.00319  -0.1105   0.6292   0.6294
   1.250   0.6044   0.00954   0.00319  -0.1108   0.6255   0.6306
   1.500   0.6326   0.00957   0.00321  -0.1111   0.6215   0.6320
   1.750   0.6606   0.00958   0.00326  -0.1114   0.6180   0.6335
   2.000   0.6887   0.00961   0.00329  -0.1118   0.6143   0.6350
   2.250   0.7166   0.00964   0.00330  -0.1120   0.6098   0.6364
   2.500   0.7429   0.00964   0.00331  -0.1119   0.6011   0.6377
   2.750   0.7685   0.00966   0.00331  -0.1117   0.5910   0.6389
   3.000   0.7951   0.00968   0.00337  -0.1117   0.5835   0.6401
   3.250   0.8215   0.00972   0.00344  -0.1116   0.5757   0.6413
   3.500   0.8469   0.00978   0.00349  -0.1114   0.5653   0.6426
   3.750   0.8716   0.00985   0.00356  -0.1110   0.5507   0.6441
   4.000   0.8939   0.00999   0.00366  -0.1102   0.5253   0.6457
   4.250   0.9049   0.01049   0.00389  -0.1073   0.4679   0.6475
   4.500   0.9008   0.01161   0.00458  -0.1018   0.3868   0.6493
   4.750   0.8899   0.01276   0.00534  -0.0950   0.3108   0.6511
   5.000   0.8866   0.01381   0.00612  -0.0900   0.2536   0.6527
   5.250   0.8797   0.01507   0.00709  -0.0847   0.1917   0.6542
   5.750   0.8720   0.01773   0.00929  -0.0762   0.0897   0.6575
   6.000   0.8804   0.01867   0.01015  -0.0740   0.0651   0.6593
   6.250   0.8887   0.01967   0.01108  -0.0719   0.0458   0.6612
   6.500   0.9018   0.02047   0.01186  -0.0705   0.0344   0.6632
   6.750   0.9151   0.02129   0.01266  -0.0692   0.0294   0.6653
   7.000   0.9305   0.02202   0.01341  -0.0681   0.0244   0.6675
   7.500   0.9546   0.02393   0.01535  -0.0655   0.0120   0.6717
   7.750   0.9682   0.02483   0.01629  -0.0644   0.0102   0.6739
   8.000   0.9832   0.02566   0.01715  -0.0635   0.0093   0.6763
   8.250   0.9988   0.02648   0.01800  -0.0627   0.0090   0.6787
   8.500   1.0143   0.02732   0.01888  -0.0620   0.0081   0.6812
   8.750   1.0294   0.02819   0.01982  -0.0612   0.0072   0.6835
   9.000   1.0412   0.02930   0.02097  -0.0602   0.0028   0.6859
   9.250   1.0542   0.03036   0.02208  -0.0593   0.0026   0.6887
   9.500   1.0666   0.03148   0.02326  -0.0584   0.0023   0.6916
   9.750   1.0801   0.03255   0.02438  -0.0576   0.0023   0.6946
  10.000   1.0933   0.03366   0.02554  -0.0568   0.0022   0.6975
  10.250   1.1061   0.03481   0.02677  -0.0561   0.0022   0.7006
  10.500   1.1187   0.03601   0.02806  -0.0554   0.0021   0.7041
  10.750   1.1312   0.03724   0.02936  -0.0547   0.0021   0.7080
  11.250   1.1551   0.03986   0.03213  -0.0533   0.0020   0.7155
  11.500   1.1668   0.04122   0.03358  -0.0527   0.0020   0.7197
  11.750   1.1780   0.04266   0.03510  -0.0521   0.0019   0.7239
  12.000   1.1890   0.04416   0.03668  -0.0516   0.0019   0.7281
  12.250   1.1994   0.04572   0.03833  -0.0510   0.0018   0.7326
  12.500   1.2092   0.04737   0.04009  -0.0505   0.0017   0.7376
  12.750   1.2188   0.04907   0.04189  -0.0500   0.0017   0.7424
  13.000   1.2277   0.05087   0.04380  -0.0495   0.0016   0.7475
  13.250   1.2371   0.05266   0.04568  -0.0491   0.0016   0.7532
  13.500   1.2455   0.05458   0.04771  -0.0488   0.0015   0.7588
  13.750   1.2535   0.05656   0.04981  -0.0484   0.0015   0.7650
  14.000   1.2607   0.05868   0.05204  -0.0481   0.0015   0.7713
  14.250   1.2674   0.06089   0.05436  -0.0479   0.0014   0.7782
  14.500   1.2735   0.06323   0.05682  -0.0477   0.0014   0.7855
  14.750   1.2795   0.06560   0.05931  -0.0476   0.0014   0.7933
  15.000   1.2834   0.06827   0.06213  -0.0476   0.0014   0.8014
  15.250   1.2871   0.07101   0.06500  -0.0476   0.0014   0.8103
  15.500   1.2901   0.07390   0.06803  -0.0477   0.0013   0.8200
  15.750   1.2906   0.07716   0.07144  -0.0479   0.0013   0.8308
  16.000   1.2919   0.08036   0.07479  -0.0482   0.0013   0.8437
  16.250   1.2903   0.08394   0.07853  -0.0486   0.0013   0.8585
  16.500   1.2870   0.08768   0.08245  -0.0489   0.0013   0.8789
  16.750   1.2789   0.09061   0.08559  -0.0476   0.0013   0.9776
  17.000   1.2735   0.09522   0.09033  -0.0489   0.0012   1.0000
  17.250   1.2684   0.09988   0.09511  -0.0502   0.0012   1.0000
  17.500   1.2645   0.10444   0.09979  -0.0518   0.0012   1.0000
  17.750   1.2556   0.10993   0.10540  -0.0537   0.0012   1.0000
  18.000   1.2465   0.11555   0.11115  -0.0559   0.0012   1.0000
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