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WORTMANN FX 73-170 A (fx73170a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 73-170 A (fx73170a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 151.72 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx73170a-il-1000000.txt
Download as CSV file: xf-fx73170a-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 73-170 A                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250   0.0011   0.09199   0.08884  -0.1272   0.7144   0.0114
 -11.000   0.0033   0.08854   0.08539  -0.1287   0.7125   0.0119
 -10.750   0.0094   0.08440   0.08123  -0.1320   0.7103   0.0118
 -10.500   0.0196   0.08185   0.07867  -0.1341   0.7085   0.0120
 -10.250   0.0239   0.07816   0.07501  -0.1366   0.7069   0.0121
 -10.000   0.0264   0.07370   0.07056  -0.1399   0.7052   0.0120
  -9.750   0.0332   0.07086   0.06773  -0.1420   0.7030   0.0125
  -9.500   0.0348   0.06626   0.06314  -0.1459   0.7011   0.0125
  -9.250   0.0364   0.06147   0.05836  -0.1505   0.6992   0.0130
  -9.000   0.0240   0.05295   0.04982  -0.1608   0.6970   0.0127
  -8.750   0.0049   0.04718   0.04393  -0.1644   0.6945   0.0125
  -8.500  -0.0142   0.04388   0.04056  -0.1621   0.6925   0.0125
  -8.250  -0.0232   0.04095   0.03754  -0.1600   0.6907   0.0128
  -8.000  -0.0290   0.03790   0.03435  -0.1576   0.6887   0.0133
  -7.750  -0.1300   0.01944   0.01431  -0.1409   0.6868   0.0094
  -7.500  -0.1034   0.02013   0.01510  -0.1411   0.6849   0.0100
  -7.250  -0.0899   0.01826   0.01291  -0.1390   0.6828   0.0103
  -7.000  -0.0717   0.01696   0.01138  -0.1377   0.6805   0.0104
  -6.750  -0.0514   0.01583   0.01005  -0.1366   0.6786   0.0105
  -6.500  -0.0302   0.01482   0.00890  -0.1357   0.6772   0.0106
  -6.250  -0.0062   0.01447   0.00846  -0.1352   0.6755   0.0111
  -6.000   0.0169   0.01386   0.00776  -0.1345   0.6737   0.0112
  -5.750   0.0400   0.01324   0.00705  -0.1339   0.6720   0.0113
  -5.500   0.0607   0.01237   0.00610  -0.1328   0.6703   0.0116
  -5.250   0.0828   0.01188   0.00558  -0.1320   0.6686   0.0123
  -5.000   0.1072   0.01165   0.00531  -0.1316   0.6667   0.0130
  -4.750   0.1310   0.01134   0.00494  -0.1311   0.6644   0.0135
  -4.500   0.1547   0.01104   0.00462  -0.1305   0.6631   0.0141
  -4.250   0.1795   0.01084   0.00439  -0.1301   0.6616   0.0146
  -4.000   0.2006   0.01034   0.00386  -0.1290   0.6600   0.0159
  -3.750   0.2253   0.01014   0.00365  -0.1286   0.6585   0.0168
  -3.500   0.2504   0.00997   0.00346  -0.1282   0.6569   0.0183
  -3.250   0.2746   0.00975   0.00322  -0.1277   0.6553   0.0209
  -3.000   0.3001   0.00963   0.00308  -0.1275   0.6538   0.0232
  -2.750   0.3249   0.00945   0.00289  -0.1270   0.6521   0.0288
  -2.500   0.3498   0.00929   0.00276  -0.1267   0.6502   0.0419
  -2.250   0.3740   0.00911   0.00266  -0.1262   0.6488   0.0684
  -2.000   0.3956   0.00878   0.00257  -0.1253   0.6475   0.1362
  -1.500   0.4260   0.00758   0.00238  -0.1212   0.6444   0.4604
  -1.250   0.4381   0.00704   0.00234  -0.1182   0.6429   0.6261
  -1.000   0.4564   0.00686   0.00241  -0.1163   0.6414   0.7150
  -0.750   0.4800   0.00689   0.00248  -0.1154   0.6400   0.7538
  -0.500   0.5056   0.00695   0.00252  -0.1151   0.6386   0.7696
  -0.250   0.5315   0.00704   0.00259  -0.1148   0.6370   0.7828
   0.000   0.5574   0.00719   0.00272  -0.1145   0.6351   0.7981
   0.250   0.5813   0.00726   0.00282  -0.1137   0.6339   0.8103
   0.500   0.6056   0.00733   0.00288  -0.1131   0.6326   0.8182
   0.750   0.6312   0.00736   0.00294  -0.1128   0.6313   0.8246
   1.000   0.6566   0.00743   0.00300  -0.1125   0.6299   0.8309
   1.250   0.6821   0.00748   0.00304  -0.1122   0.6285   0.8347
   1.500   0.7088   0.00750   0.00305  -0.1122   0.6271   0.8376
   1.750   0.7358   0.00753   0.00307  -0.1123   0.6257   0.8400
   2.000   0.7624   0.00757   0.00310  -0.1124   0.6242   0.8426
   2.250   0.7897   0.00763   0.00315  -0.1126   0.6227   0.8451
   2.500   0.8179   0.00774   0.00322  -0.1130   0.6211   0.8475
   2.750   0.8448   0.00784   0.00331  -0.1132   0.6197   0.8498
   3.000   0.8701   0.00786   0.00336  -0.1130   0.6186   0.8523
   3.250   0.8958   0.00789   0.00342  -0.1128   0.6173   0.8547
   3.500   0.9214   0.00793   0.00348  -0.1127   0.6158   0.8573
   3.750   0.9472   0.00797   0.00356  -0.1126   0.6143   0.8599
   4.000   0.9732   0.00803   0.00362  -0.1126   0.6128   0.8626
   4.250   0.9990   0.00809   0.00368  -0.1126   0.6113   0.8649
   4.500   1.0258   0.00813   0.00375  -0.1127   0.6097   0.8673
   4.750   1.0542   0.00820   0.00383  -0.1133   0.6082   0.8695
   5.000   1.0843   0.00833   0.00394  -0.1142   0.6060   0.8716
   5.250   1.1083   0.00837   0.00404  -0.1139   0.6040   0.8743
   5.500   1.1312   0.00840   0.00412  -0.1132   0.6016   0.8769
   5.750   1.1556   0.00844   0.00420  -0.1130   0.5991   0.8794
   6.000   1.1804   0.00847   0.00425  -0.1128   0.5963   0.8819
   6.250   1.2091   0.00852   0.00432  -0.1135   0.5932   0.8846
   6.500   1.2380   0.00862   0.00444  -0.1142   0.5900   0.8870
   6.750   1.2599   0.00865   0.00456  -0.1135   0.5866   0.8903
   7.000   1.2857   0.00872   0.00468  -0.1137   0.5832   0.8934
   7.500   1.3413   0.00893   0.00497  -0.1150   0.5721   0.9001
   7.750   1.3715   0.00904   0.00515  -0.1163   0.5667   0.9035
   8.000   1.3996   0.00923   0.00537  -0.1172   0.5586   0.9074
   8.500   1.4594   0.00967   0.00592  -0.1200   0.5398   0.9160
   8.750   1.4874   0.00999   0.00627  -0.1212   0.5298   0.9222
   9.000   1.5108   0.01045   0.00677  -0.1216   0.5142   0.9323
   9.250   1.5301   0.01137   0.00767  -0.1221   0.4871   0.9582
   9.500   1.5339   0.01300   0.00920  -0.1199   0.4567   1.0000
   9.750   1.5068   0.01612   0.01207  -0.1136   0.4081   1.0000
  10.000   1.4950   0.01857   0.01439  -0.1097   0.3794   1.0000
  10.250   1.4734   0.02172   0.01736  -0.1047   0.3432   1.0000
  10.500   1.4744   0.02349   0.01910  -0.1024   0.3281   1.0000
  10.750   1.4488   0.02711   0.02250  -0.0975   0.2865   1.0000
  11.000   1.4341   0.03017   0.02538  -0.0940   0.2543   1.0000
  11.250   1.4331   0.03229   0.02743  -0.0919   0.2360   1.0000
  11.500   1.4239   0.03510   0.03009  -0.0891   0.2069   1.0000
  11.750   1.4147   0.03799   0.03282  -0.0865   0.1766   1.0000
  12.250   1.4094   0.04288   0.03747  -0.0826   0.1310   1.0000
  12.500   1.4049   0.04555   0.04002  -0.0807   0.1076   1.0000
  12.750   1.4074   0.04765   0.04204  -0.0794   0.0922   1.0000
  13.000   1.4064   0.05012   0.04441  -0.0778   0.0751   1.0000
  13.250   1.4091   0.05228   0.04650  -0.0766   0.0616   1.0000
  13.500   1.4118   0.05449   0.04867  -0.0755   0.0510   1.0000
  13.750   1.4149   0.05666   0.05078  -0.0744   0.0410   1.0000
  14.000   1.4203   0.05866   0.05278  -0.0735   0.0357   1.0000
  14.250   1.4271   0.06057   0.05471  -0.0728   0.0319   1.0000
  14.500   1.4337   0.06248   0.05663  -0.0721   0.0287   1.0000
  14.750   1.4408   0.06440   0.05856  -0.0715   0.0260   1.0000
  15.000   1.4476   0.06634   0.06055  -0.0709   0.0241   1.0000
  15.250   1.4536   0.06835   0.06257  -0.0703   0.0220   1.0000
  15.500   1.4602   0.07034   0.06461  -0.0697   0.0208   1.0000
  15.750   1.4676   0.07229   0.06660  -0.0693   0.0191   1.0000
  16.000   1.4726   0.07447   0.06880  -0.0688   0.0169   1.0000
  16.250   1.4793   0.07650   0.07088  -0.0684   0.0155   1.0000
  16.500   1.4849   0.07869   0.07310  -0.0680   0.0140   1.0000
  16.750   1.4889   0.08100   0.07544  -0.0676   0.0118   1.0000
  17.000   1.4907   0.08362   0.07807  -0.0671   0.0099   1.0000
  17.250   1.4947   0.08603   0.08053  -0.0668   0.0088   1.0000
  17.500   1.4966   0.08868   0.08322  -0.0665   0.0079   1.0000
  17.750   1.4961   0.09169   0.08629  -0.0661   0.0072   1.0000
  18.000   1.5021   0.09389   0.08856  -0.0661   0.0067   1.0000
  18.250   1.5030   0.09677   0.09151  -0.0659   0.0062   1.0000
  18.500   1.5041   0.09961   0.09441  -0.0659   0.0060   1.0000
  18.750   1.5013   0.10299   0.09785  -0.0658   0.0055   1.0000
  19.000   1.5007   0.10612   0.10107  -0.0659   0.0052   1.0000
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