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WORTMANN FX 75-193 (fx75193-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 75-193 (fx75193-il)
Reynolds number: 200,000
Max Cl/Cd: 44.09 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx75193-il-200000-n5.txt
Download as CSV file: xf-fx75193-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 75-193                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.2453   0.07984   0.07445  -0.1516   0.8182   0.0132
 -14.500  -0.2831   0.06945   0.06384  -0.1580   0.8177   0.0131
 -14.250  -0.3117   0.06217   0.05634  -0.1618   0.8172   0.0129
 -14.000  -0.3273   0.05750   0.05150  -0.1639   0.8165   0.0129
 -13.750  -0.3409   0.05351   0.04731  -0.1651   0.8157   0.0130
 -13.500  -0.3542   0.04982   0.04341  -0.1656   0.8149   0.0129
 -13.250  -0.3604   0.04718   0.04061  -0.1656   0.8141   0.0130
 -13.000  -0.3657   0.04469   0.03792  -0.1652   0.8131   0.0132
 -12.750  -0.3682   0.04247   0.03551  -0.1645   0.8122   0.0133
 -12.500  -0.3669   0.04059   0.03346  -0.1636   0.8110   0.0133
 -12.250  -0.3628   0.03897   0.03169  -0.1627   0.8097   0.0133
 -12.000  -0.3569   0.03742   0.02997  -0.1616   0.8084   0.0134
 -11.750  -0.3486   0.03610   0.02852  -0.1607   0.8074   0.0135
 -11.500  -0.3388   0.03489   0.02718  -0.1596   0.8064   0.0135
 -11.250  -0.3281   0.03377   0.02594  -0.1586   0.8054   0.0136
 -11.000  -0.3166   0.03278   0.02484  -0.1575   0.8044   0.0138
 -10.750  -0.3045   0.03190   0.02388  -0.1564   0.8035   0.0138
 -10.500  -0.2927   0.03103   0.02291  -0.1552   0.8025   0.0140
 -10.250  -0.2823   0.03016   0.02199  -0.1539   0.8014   0.0141
 -10.000  -0.2721   0.02942   0.02122  -0.1524   0.8000   0.0143
  -9.750  -0.2632   0.02868   0.02045  -0.1507   0.7987   0.0145
  -9.500  -0.2539   0.02801   0.01976  -0.1489   0.7972   0.0148
  -9.250  -0.2442   0.02739   0.01911  -0.1471   0.7954   0.0150
  -9.000  -0.2347   0.02676   0.01845  -0.1452   0.7933   0.0153
  -8.750  -0.2243   0.02619   0.01782  -0.1433   0.7913   0.0156
  -8.500  -0.2134   0.02564   0.01722  -0.1415   0.7895   0.0161
  -8.250  -0.2027   0.02506   0.01660  -0.1396   0.7878   0.0169
  -8.000  -0.1907   0.02456   0.01607  -0.1379   0.7862   0.0175
  -7.750  -0.1785   0.02409   0.01556  -0.1361   0.7848   0.0184
  -7.250  -0.1623   0.02342   0.01491  -0.1312   0.7815   0.0226
  -7.000  -0.1596   0.02324   0.01476  -0.1277   0.7789   0.0259
  -6.750  -0.1564   0.02307   0.01458  -0.1243   0.7762   0.0303
  -6.500  -0.1477   0.02278   0.01428  -0.1219   0.7737   0.0379
  -6.250  -0.1368   0.02240   0.01395  -0.1200   0.7717   0.0464
  -6.000  -0.1223   0.02206   0.01364  -0.1186   0.7700   0.0557
  -5.750  -0.1052   0.02174   0.01331  -0.1176   0.7687   0.0663
  -5.500  -0.0868   0.02140   0.01298  -0.1168   0.7674   0.0776
  -5.250  -0.0724   0.02115   0.01279  -0.1153   0.7653   0.0934
  -5.000  -0.0670   0.02103   0.01283  -0.1124   0.7608   0.1159
  -4.750  -0.0543   0.02048   0.01254  -0.1110   0.7579   0.1682
  -4.500  -0.0404   0.01951   0.01205  -0.1103   0.7556   0.2718
  -4.250  -0.0236   0.01826   0.01155  -0.1102   0.7539   0.4330
  -4.000  -0.0023   0.01854   0.01240  -0.1081   0.7525   0.5474
  -3.750   0.0256   0.01904   0.01292  -0.1073   0.7515   0.5798
  -3.500   0.0370   0.01983   0.01376  -0.1041   0.7468   0.5977
  -3.250   0.0542   0.02049   0.01440  -0.1021   0.7428   0.6144
  -3.000   0.0809   0.02080   0.01460  -0.1020   0.7405   0.6300
  -2.500   0.1379   0.02169   0.01533  -0.1016   0.7376   0.6543
  -2.000   0.1582   0.02294   0.01658  -0.0952   0.7277   0.6690
  -1.750   0.1865   0.02278   0.01627  -0.0962   0.7255   0.6770
  -1.500   0.2128   0.02278   0.01623  -0.0958   0.7240   0.6787
  -1.250   0.2411   0.02272   0.01613  -0.0959   0.7229   0.6807
  -1.000   0.2274   0.02343   0.01689  -0.0891   0.7134   0.6838
  -0.750   0.2533   0.02329   0.01667  -0.0891   0.7113   0.6867
  -0.500   0.2842   0.02304   0.01634  -0.0902   0.7099   0.6898
  -0.250   0.3182   0.02271   0.01591  -0.0921   0.7089   0.6934
   0.000   0.3285   0.02285   0.01604  -0.0893   0.7047   0.6949
   0.250   0.3812   0.02223   0.01535  -0.0935   0.7072   0.6960
   0.750   0.3850   0.02282   0.01596  -0.0853   0.6940   0.7001
   1.000   0.4168   0.02250   0.01561  -0.0861   0.6932   0.7019
   1.250   0.4494   0.02216   0.01523  -0.0872   0.6924   0.7039
   1.750   0.4617   0.02334   0.01635  -0.0821   0.6783   0.7100
   2.000   0.4914   0.02304   0.01605  -0.0825   0.6774   0.7111
   2.250   0.5221   0.02270   0.01571  -0.0830   0.6765   0.7123
   3.250   0.5939   0.02352   0.01657  -0.0783   0.6587   0.7190
   3.750   0.6251   0.02421   0.01728  -0.0757   0.6470   0.7232
   4.000   0.6577   0.02385   0.01692  -0.0766   0.6457   0.7250
   4.250   0.6915   0.02346   0.01653  -0.0778   0.6446   0.7265
   4.750   0.7186   0.02438   0.01751  -0.0747   0.6317   0.7291
   5.000   0.7505   0.02397   0.01713  -0.0753   0.6298   0.7302
   5.250   0.7859   0.02341   0.01660  -0.0764   0.6283   0.7314
   5.750   0.8176   0.02412   0.01741  -0.0737   0.6152   0.7338
   6.000   0.8517   0.02367   0.01699  -0.0748   0.6128   0.7349
   6.250   0.8898   0.02308   0.01643  -0.0763   0.6111   0.7358
   6.750   0.9210   0.02390   0.01736  -0.0737   0.5969   0.7382
   7.000   0.9616   0.02318   0.01666  -0.0756   0.5937   0.7394
   7.250   0.9660   0.02412   0.01767  -0.0729   0.5840   0.7409
   7.500   0.9930   0.02404   0.01764  -0.0731   0.5785   0.7421
   7.750   1.0327   0.02342   0.01704  -0.0748   0.5747   0.7429
   8.000   1.0312   0.02461   0.01830  -0.0715   0.5630   0.7438
   8.250   1.0581   0.02443   0.01812  -0.0715   0.5525   0.7445
   8.500   1.0780   0.02455   0.01825  -0.0706   0.5400   0.7454
   8.750   1.0892   0.02501   0.01870  -0.0686   0.5230   0.7463
   9.000   1.1018   0.02543   0.01909  -0.0668   0.5044   0.7472
   9.250   1.1107   0.02602   0.01960  -0.0646   0.4796   0.7479
   9.500   1.1159   0.02686   0.02032  -0.0620   0.4521   0.7485
   9.750   1.1218   0.02775   0.02108  -0.0596   0.4270   0.7492
  10.000   1.1239   0.02892   0.02216  -0.0570   0.3986   0.7500
  10.250   1.1212   0.03040   0.02348  -0.0539   0.3666   0.7509
  10.500   1.1173   0.03211   0.02501  -0.0509   0.3339   0.7516
  10.750   1.1124   0.03401   0.02674  -0.0481   0.3008   0.7522
  11.000   1.1076   0.03606   0.02862  -0.0455   0.2674   0.7526
  11.250   1.0997   0.03846   0.03081  -0.0429   0.2290   0.7530
  11.500   1.0912   0.04107   0.03319  -0.0404   0.1893   0.7535
  11.750   1.0846   0.04369   0.03559  -0.0384   0.1514   0.7542
  12.000   1.0783   0.04640   0.03808  -0.0366   0.1144   0.7548
  12.250   1.0762   0.04888   0.04041  -0.0352   0.0864   0.7553
  12.500   1.0751   0.05137   0.04277  -0.0340   0.0655   0.7556
  12.750   1.0781   0.05358   0.04492  -0.0332   0.0499   0.7559
  13.000   1.0816   0.05582   0.04713  -0.0325   0.0411   0.7562
  13.250   1.0874   0.05789   0.04924  -0.0320   0.0340   0.7565
  13.500   1.0931   0.06004   0.05142  -0.0315   0.0280   0.7568
  13.750   1.0985   0.06225   0.05366  -0.0312   0.0240   0.7571
  14.250   1.1088   0.06686   0.05839  -0.0307   0.0199   0.7578
  14.500   1.1124   0.06942   0.06100  -0.0305   0.0187   0.7581
  14.750   1.1181   0.07180   0.06348  -0.0305   0.0179   0.7584
  15.000   1.1225   0.07436   0.06615  -0.0305   0.0170   0.7587
  15.250   1.1268   0.07699   0.06887  -0.0306   0.0163   0.7590
  15.500   1.1298   0.07981   0.07178  -0.0308   0.0159   0.7593
  15.750   1.1331   0.08266   0.07472  -0.0311   0.0154   0.7596
  16.000   1.1367   0.08551   0.07768  -0.0315   0.0151   0.7599
  16.250   1.1402   0.08842   0.08069  -0.0319   0.0147   0.7603
  16.500   1.1433   0.09139   0.08378  -0.0324   0.0145   0.7608
  16.750   1.1465   0.09438   0.08687  -0.0331   0.0141   0.7613
  17.000   1.1496   0.09743   0.09001  -0.0338   0.0139   0.7617
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