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WORTMANN FX 73-170 A (fx73170a-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 73-170 A (fx73170a-il)
Reynolds number: 200,000
Max Cl/Cd: 51.19 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx73170a-il-200000-n5.txt
Download as CSV file: xf-fx73170a-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 73-170 A                            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.0115   0.12572   0.12055  -0.1227   0.7669   0.0248
 -13.250  -0.0107   0.12255   0.11737  -0.1252   0.7651   0.0250
 -13.000  -0.0055   0.11944   0.11424  -0.1272   0.7632   0.0251
 -12.750  -0.0016   0.11606   0.11089  -0.1290   0.7608   0.0252
 -12.500   0.0020   0.11261   0.10746  -0.1309   0.7586   0.0252
 -12.000   0.0115   0.10587   0.10074  -0.1340   0.7538   0.0253
 -11.750   0.0186   0.10252   0.09738  -0.1348   0.7518   0.0254
 -11.500   0.0300   0.09982   0.09463  -0.1346   0.7498   0.0259
 -11.250   0.0347   0.09670   0.09150  -0.1362   0.7479   0.0259
 -11.000   0.0372   0.09332   0.08815  -0.1379   0.7456   0.0258
 -10.750   0.0973   0.07454   0.06967  -0.1292   0.7336   0.0193
 -10.500   0.0986   0.07117   0.06632  -0.1299   0.7317   0.0187
 -10.000   0.0303   0.07466   0.06956  -0.1443   0.7372   0.0157
  -9.750   0.0350   0.07242   0.06732  -0.1451   0.7353   0.0155
  -9.500   0.0427   0.07079   0.06566  -0.1457   0.7335   0.0149
  -9.250   0.0348   0.06601   0.06094  -0.1481   0.7311   0.0149
  -9.000   0.0224   0.06042   0.05542  -0.1518   0.7282   0.0146
  -8.750   0.0019   0.05500   0.04997  -0.1543   0.7253   0.0146
  -8.500  -0.0158   0.05162   0.04654  -0.1536   0.7227   0.0143
  -8.250  -0.0361   0.04872   0.04353  -0.1508   0.7204   0.0142
  -8.000  -0.0472   0.04558   0.04019  -0.1486   0.7186   0.0137
  -7.750  -0.0587   0.04193   0.03632  -0.1458   0.7164   0.0137
  -7.500  -0.0646   0.03856   0.03270  -0.1429   0.7139   0.0136
  -7.250  -0.0654   0.03536   0.02919  -0.1401   0.7115   0.0135
  -7.000  -0.0605   0.03261   0.02607  -0.1376   0.7093   0.0137
  -6.750  -0.0514   0.03004   0.02311  -0.1354   0.7073   0.0137
  -6.500  -0.0376   0.02793   0.02059  -0.1337   0.7054   0.0146
  -6.250  -0.0209   0.02583   0.01791  -0.1320   0.7038   0.0157
  -6.000  -0.0007   0.02437   0.01616  -0.1310   0.7022   0.0159
  -5.750   0.0186   0.02372   0.01549  -0.1301   0.6998   0.0167
  -5.500   0.0395   0.02274   0.01436  -0.1292   0.6976   0.0171
  -5.250   0.0617   0.02183   0.01330  -0.1284   0.6955   0.0177
  -5.000   0.0846   0.02094   0.01226  -0.1277   0.6937   0.0185
  -4.750   0.1079   0.02017   0.01137  -0.1270   0.6921   0.0190
  -4.500   0.1312   0.01944   0.01050  -0.1263   0.6905   0.0201
  -4.250   0.1546   0.01891   0.00996  -0.1259   0.6890   0.0219
  -4.000   0.1793   0.01852   0.00949  -0.1256   0.6877   0.0243
  -3.750   0.1979   0.01813   0.00912  -0.1242   0.6852   0.0264
  -3.500   0.2179   0.01782   0.00880  -0.1231   0.6829   0.0287
  -3.250   0.2391   0.01753   0.00846  -0.1221   0.6810   0.0326
  -3.000   0.2613   0.01726   0.00818  -0.1213   0.6792   0.0392
  -2.750   0.2839   0.01696   0.00786  -0.1206   0.6776   0.0473
  -2.500   0.3070   0.01665   0.00758  -0.1200   0.6761   0.0662
  -2.250   0.3289   0.01619   0.00734  -0.1194   0.6747   0.1246
  -2.000   0.3455   0.01533   0.00713  -0.1180   0.6735   0.3066
  -1.750   0.3537   0.01453   0.00716  -0.1147   0.6715   0.5301
  -1.500   0.3628   0.01444   0.00771  -0.1107   0.6689   0.6928
  -1.250   0.3812   0.01469   0.00801  -0.1086   0.6668   0.7517
  -1.000   0.3997   0.01497   0.00830  -0.1064   0.6649   0.7920
  -0.750   0.4168   0.01527   0.00861  -0.1037   0.6632   0.8271
  -0.500   0.4361   0.01544   0.00874  -0.1016   0.6618   0.8489
  -0.250   0.4602   0.01551   0.00874  -0.1008   0.6605   0.8593
   0.000   0.4864   0.01553   0.00865  -0.1007   0.6593   0.8659
   0.250   0.5148   0.01553   0.00855  -0.1009   0.6582   0.8706
   0.500   0.5288   0.01578   0.00881  -0.0987   0.6555   0.8769
   0.750   0.5443   0.01603   0.00907  -0.0967   0.6530   0.8820
   1.000   0.5635   0.01622   0.00923  -0.0955   0.6509   0.8869
   1.250   0.5842   0.01636   0.00934  -0.0945   0.6490   0.8922
   1.500   0.6081   0.01645   0.00939  -0.0941   0.6475   0.8966
   1.750   0.6347   0.01649   0.00939  -0.0942   0.6461   0.9009
   2.000   0.6628   0.01652   0.00936  -0.0946   0.6449   0.9052
   2.250   0.6917   0.01654   0.00933  -0.0951   0.6438   0.9095
   2.500   0.7204   0.01665   0.00943  -0.0957   0.6427   0.9132
   2.750   0.7171   0.01747   0.01037  -0.0909   0.6383   0.9222
   3.000   0.7372   0.01786   0.01080  -0.0903   0.6356   0.9279
   3.250   0.7644   0.01806   0.01100  -0.0909   0.6336   0.9329
   3.500   0.7928   0.01820   0.01115  -0.0916   0.6321   0.9383
   3.750   0.8270   0.01833   0.01128  -0.0934   0.6310   0.9425
   4.000   0.8621   0.01844   0.01139  -0.0955   0.6300   0.9467
   4.250   0.8987   0.01850   0.01147  -0.0977   0.6291   0.9513
   4.750   0.9326   0.02061   0.01379  -0.0977   0.6206   1.0000
   5.000   0.9497   0.02101   0.01420  -0.0966   0.6181   1.0000
   5.250   0.9769   0.02108   0.01430  -0.0970   0.6166   1.0000
   5.500   1.0063   0.02111   0.01434  -0.0977   0.6154   1.0000
   5.750   1.0386   0.02105   0.01429  -0.0989   0.6144   1.0000
   6.000   1.0730   0.02096   0.01423  -0.1004   0.6136   1.0000
   6.500   1.0483   0.02451   0.01789  -0.0910   0.6004   1.0000
   6.750   1.0832   0.02415   0.01758  -0.0922   0.5995   1.0000
   7.000   1.1195   0.02375   0.01722  -0.0936   0.5988   1.0000
   7.500   1.0948   0.02852   0.02214  -0.0862   0.5822   1.0000
   7.750   1.1420   0.02714   0.02080  -0.0884   0.5833   1.0000
   8.250   1.1409   0.03078   0.02458  -0.0839   0.5678   1.0000
   8.500   1.1898   0.02910   0.02297  -0.0860   0.5691   1.0000
   9.000   1.1972   0.03221   0.02623  -0.0825   0.5539   1.0000
   9.500   1.2147   0.03468   0.02886  -0.0800   0.5390   1.0000
   9.750   1.2080   0.03720   0.03146  -0.0777   0.5270   1.0000
  10.750   1.2490   0.04197   0.03653  -0.0737   0.4858   1.0000
  11.000   1.2695   0.04219   0.03681  -0.0733   0.4720   1.0000
  11.250   1.3046   0.04081   0.03538  -0.0737   0.4489   1.0000
  11.500   1.3392   0.03929   0.03359  -0.0736   0.4098   1.0000
  11.750   1.3476   0.04034   0.03443  -0.0720   0.3754   1.0000
  12.000   1.3462   0.04243   0.03633  -0.0701   0.3447   1.0000
  12.500   1.3345   0.04783   0.04141  -0.0660   0.2859   1.0000
  12.750   1.3279   0.05076   0.04420  -0.0643   0.2582   1.0000
  13.000   1.3247   0.05348   0.04684  -0.0628   0.2350   1.0000
  13.250   1.3185   0.05657   0.04980  -0.0613   0.2081   1.0000
  13.500   1.3142   0.05953   0.05265  -0.0601   0.1856   1.0000
  13.750   1.3113   0.06240   0.05542  -0.0590   0.1630   1.0000
  14.000   1.3073   0.06545   0.05837  -0.0579   0.1415   1.0000
  14.250   1.3062   0.06825   0.06112  -0.0570   0.1215   1.0000
  14.500   1.3053   0.07108   0.06389  -0.0562   0.1049   1.0000
  14.750   1.3030   0.07407   0.06680  -0.0555   0.0885   1.0000
  15.000   1.3034   0.07684   0.06954  -0.0549   0.0765   1.0000
  15.500   1.3048   0.08242   0.07511  -0.0540   0.0566   1.0000
  15.750   1.3063   0.08516   0.07787  -0.0536   0.0496   1.0000
  16.000   1.3057   0.08820   0.08093  -0.0533   0.0435   1.0000
  16.250   1.3085   0.09084   0.08362  -0.0532   0.0385   1.0000
  16.500   1.3084   0.09389   0.08672  -0.0530   0.0359   1.0000
  16.750   1.3121   0.09651   0.08944  -0.0530   0.0327   1.0000
  17.000   1.3134   0.09944   0.09242  -0.0531   0.0296   1.0000
  17.250   1.3135   0.10256   0.09560  -0.0532   0.0272   1.0000
  17.500   1.3160   0.10539   0.09856  -0.0534   0.0253   1.0000
  17.750   1.3169   0.10845   0.10169  -0.0537   0.0232   1.0000
  18.000   1.3155   0.11185   0.10515  -0.0541   0.0215   1.0000
  18.250   1.3170   0.11488   0.10832  -0.0545   0.0202   1.0000
  18.500   1.3183   0.11798   0.11153  -0.0551   0.0182   1.0000
  18.750   1.3164   0.12157   0.11518  -0.0558   0.0170   1.0000
  19.000   1.3170   0.12483   0.11856  -0.0566   0.0157   1.0000
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