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WORTMANN FX 73-170 (fx73170-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 73-170 (fx73170-il)
Reynolds number: 200,000
Max Cl/Cd: 45.58 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx73170-il-200000-n5.txt
Download as CSV file: xf-fx73170-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 73-170                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.0970   0.11361   0.10853  -0.1230   0.7918   0.0217
 -13.000  -0.0858   0.11170   0.10660  -0.1239   0.7903   0.0223
 -12.750  -0.0975   0.10250   0.09739  -0.1276   0.7893   0.0168
 -12.500  -0.0998   0.09711   0.09202  -0.1300   0.7879   0.0168
 -12.250  -0.0945   0.09400   0.08888  -0.1317   0.7864   0.0166
 -12.000  -0.0936   0.08991   0.08481  -0.1337   0.7849   0.0165
 -11.750  -0.0952   0.08541   0.08036  -0.1358   0.7831   0.0163
 -11.500  -0.0932   0.08190   0.07686  -0.1377   0.7813   0.0158
 -11.250  -0.1198   0.07018   0.06520  -0.1440   0.7797   0.0158
 -11.000  -0.1431   0.06109   0.05603  -0.1504   0.7780   0.0150
 -10.750  -0.1766   0.05375   0.04853  -0.1545   0.7759   0.0150
 -10.500  -0.2029   0.04874   0.04332  -0.1558   0.7738   0.0149
 -10.250  -0.2196   0.04529   0.03969  -0.1557   0.7720   0.0149
 -10.000  -0.2393   0.04179   0.03594  -0.1546   0.7701   0.0148
  -9.750  -0.2535   0.03937   0.03337  -0.1522   0.7674   0.0147
  -9.500  -0.2674   0.03723   0.03101  -0.1490   0.7648   0.0150
  -9.250  -0.2694   0.03512   0.02864  -0.1468   0.7624   0.0150
  -9.000  -0.2671   0.03296   0.02616  -0.1449   0.7605   0.0153
  -8.750  -0.2589   0.03095   0.02384  -0.1433   0.7588   0.0154
  -8.500  -0.2459   0.02926   0.02185  -0.1421   0.7573   0.0157
  -8.250  -0.2297   0.02767   0.01995  -0.1411   0.7560   0.0161
  -8.000  -0.2112   0.02639   0.01833  -0.1402   0.7547   0.0169
  -7.750  -0.1937   0.02561   0.01756  -0.1394   0.7527   0.0177
  -7.500  -0.1750   0.02490   0.01679  -0.1385   0.7506   0.0185
  -7.250  -0.1547   0.02404   0.01583  -0.1377   0.7486   0.0191
  -7.000  -0.1339   0.02316   0.01484  -0.1368   0.7468   0.0196
  -6.750  -0.1129   0.02238   0.01397  -0.1360   0.7452   0.0203
  -6.500  -0.0918   0.02169   0.01316  -0.1352   0.7437   0.0211
  -6.250  -0.0717   0.02097   0.01242  -0.1344   0.7423   0.0218
  -6.000  -0.0505   0.02042   0.01185  -0.1338   0.7410   0.0231
  -5.750  -0.0276   0.02000   0.01136  -0.1335   0.7398   0.0254
  -5.500  -0.0066   0.01946   0.01078  -0.1329   0.7384   0.0276
  -5.250   0.0118   0.01910   0.01043  -0.1318   0.7360   0.0293
  -5.000   0.0322   0.01876   0.01007  -0.1310   0.7339   0.0318
  -4.750   0.0535   0.01839   0.00969  -0.1304   0.7320   0.0359
  -4.500   0.0759   0.01805   0.00933  -0.1299   0.7304   0.0432
  -4.250   0.0990   0.01768   0.00898  -0.1296   0.7288   0.0545
  -4.000   0.1222   0.01724   0.00864  -0.1294   0.7274   0.0838
  -3.750   0.1441   0.01653   0.00829  -0.1293   0.7260   0.1681
  -3.500   0.1635   0.01542   0.00785  -0.1292   0.7247   0.3419
  -3.250   0.1822   0.01512   0.00846  -0.1274   0.7236   0.5556
  -3.000   0.2048   0.01555   0.00887  -0.1264   0.7215   0.6016
  -2.750   0.2272   0.01599   0.00926  -0.1254   0.7192   0.6214
  -2.500   0.2505   0.01653   0.00978  -0.1243   0.7172   0.6409
  -2.250   0.2741   0.01712   0.01035  -0.1230   0.7154   0.6589
  -2.000   0.2991   0.01742   0.01061  -0.1223   0.7137   0.6681
  -1.750   0.3256   0.01754   0.01065  -0.1221   0.7122   0.6739
  -1.500   0.3534   0.01753   0.01051  -0.1225   0.7109   0.6792
  -1.250   0.3808   0.01757   0.01049  -0.1225   0.7098   0.6813
  -1.000   0.4087   0.01760   0.01046  -0.1227   0.7089   0.6837
  -0.750   0.4357   0.01766   0.01046  -0.1228   0.7078   0.6862
  -0.500   0.4498   0.01804   0.01088  -0.1208   0.7041   0.6889
  -0.250   0.4712   0.01821   0.01100  -0.1200   0.7014   0.6914
   0.000   0.4955   0.01829   0.01103  -0.1199   0.6994   0.6938
   0.250   0.5208   0.01836   0.01106  -0.1198   0.6979   0.6955
   0.500   0.5471   0.01840   0.01108  -0.1198   0.6965   0.6968
   0.750   0.5749   0.01841   0.01105  -0.1200   0.6953   0.6980
   1.000   0.6036   0.01839   0.01100  -0.1204   0.6943   0.6993
   1.250   0.6330   0.01837   0.01095  -0.1210   0.6934   0.7008
   1.500   0.6358   0.01911   0.01178  -0.1171   0.6883   0.7027
   1.750   0.6529   0.01941   0.01210  -0.1157   0.6853   0.7042
   2.000   0.6766   0.01951   0.01219  -0.1153   0.6832   0.7056
   2.250   0.7026   0.01957   0.01224  -0.1153   0.6817   0.7071
   2.500   0.7300   0.01961   0.01226  -0.1156   0.6805   0.7088
   3.000   0.7900   0.01953   0.01218  -0.1169   0.6786   0.7115
   3.500   0.7866   0.02106   0.01386  -0.1075   0.6677   0.7141
   3.750   0.8141   0.02104   0.01386  -0.1077   0.6663   0.7153
   4.000   0.8438   0.02098   0.01384  -0.1082   0.6652   0.7165
   4.250   0.8764   0.02085   0.01374  -0.1093   0.6642   0.7177
   4.500   0.9102   0.02070   0.01362  -0.1106   0.6634   0.7194
   5.000   0.8484   0.02426   0.01728  -0.0928   0.6435   0.7238
   5.250   0.9026   0.02301   0.01608  -0.0965   0.6461   0.7250
   5.500   0.9573   0.02198   0.01509  -0.1007   0.6478   0.7262
   6.000   0.9377   0.02471   0.01795  -0.0906   0.6312   0.7291
   6.250   0.9902   0.02333   0.01666  -0.0938   0.6329   0.7302
   6.750   0.9894   0.02579   0.01926  -0.0873   0.6165   0.7337
   7.000   1.0492   0.02375   0.01731  -0.0910   0.6189   0.7354
   7.500   1.0265   0.02777   0.02145  -0.0827   0.5942   0.7398
   7.750   1.0624   0.02690   0.02066  -0.0836   0.5914   0.7417
   8.250   1.0886   0.02803   0.02196  -0.0807   0.5706   0.7449
   8.750   1.1382   0.02755   0.02160  -0.0800   0.5447   0.7487
   9.000   1.1511   0.02822   0.02230  -0.0787   0.5235   0.7508
   9.250   1.1875   0.02709   0.02109  -0.0792   0.4942   0.7532
   9.500   1.2139   0.02663   0.02038  -0.0786   0.4528   0.7554
   9.750   1.2202   0.02768   0.02120  -0.0764   0.4135   0.7577
  10.000   1.2159   0.02954   0.02282  -0.0735   0.3712   0.7599
  10.250   1.2128   0.03155   0.02466  -0.0709   0.3364   0.7622
  10.500   1.2076   0.03385   0.02678  -0.0685   0.3004   0.7651
  10.750   1.2043   0.03616   0.02892  -0.0664   0.2664   0.7677
  11.000   1.2028   0.03846   0.03106  -0.0647   0.2350   0.7706
  11.500   1.2028   0.04313   0.03546  -0.0618   0.1739   0.7756
  11.750   1.2046   0.04547   0.03766  -0.0608   0.1462   0.7785
  12.000   1.2085   0.04765   0.03977  -0.0599   0.1235   0.7817
  12.250   1.2132   0.04981   0.04185  -0.0591   0.1042   0.7852
  12.750   1.2260   0.05404   0.04604  -0.0580   0.0754   0.7929
  13.000   1.2341   0.05609   0.04812  -0.0577   0.0676   0.7977
  13.250   1.2412   0.05823   0.05029  -0.0574   0.0596   0.8029
  13.500   1.2500   0.06036   0.05253  -0.0573   0.0542   0.8092
  13.750   1.2578   0.06262   0.05484  -0.0572   0.0491   0.8167
  14.000   1.2667   0.06493   0.05726  -0.0574   0.0453   0.8273
  14.250   1.2773   0.06726   0.05975  -0.0580   0.0420   0.8433
  14.500   1.2878   0.07024   0.06289  -0.0595   0.0386   0.8796
  14.750   1.2915   0.07218   0.06494  -0.0585   0.0367   1.0000
  15.000   1.2968   0.07454   0.06741  -0.0581   0.0347   1.0000
  15.250   1.3018   0.07698   0.06991  -0.0579   0.0326   1.0000
  15.500   1.3032   0.07984   0.07281  -0.0576   0.0309   1.0000
  15.750   1.3079   0.08234   0.07542  -0.0574   0.0293   1.0000
  16.000   1.3124   0.08485   0.07805  -0.0573   0.0279   1.0000
  16.250   1.3160   0.08753   0.08081  -0.0572   0.0264   1.0000
  16.500   1.3180   0.09042   0.08377  -0.0572   0.0252   1.0000
  16.750   1.3180   0.09359   0.08698  -0.0573   0.0239   1.0000
  17.000   1.3218   0.09631   0.08984  -0.0574   0.0229   1.0000
  17.250   1.3246   0.09918   0.09283  -0.0576   0.0218   1.0000
  17.500   1.3274   0.10214   0.09590  -0.0581   0.0205   1.0000
  17.750   1.3277   0.10538   0.09923  -0.0586   0.0197   1.0000
  18.000   1.3259   0.10892   0.10281  -0.0591   0.0190   1.0000
  18.250   1.3278   0.11202   0.10607  -0.0597   0.0182   1.0000
  18.500   1.3289   0.11524   0.10943  -0.0603   0.0175   1.0000
  18.750   1.3294   0.11866   0.11297  -0.0613   0.0166   1.0000
  19.000   1.3292   0.12216   0.11658  -0.0623   0.0161   1.0000
  19.250   1.3287   0.12575   0.12027  -0.0635   0.0157   1.0000
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