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WORTMANN FX 73-170 A (fx73170a-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 73-170 A (fx73170a-il)
Reynolds number: 500,000
Max Cl/Cd: 117.85 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx73170a-il-500000.txt
Download as CSV file: xf-fx73170a-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250   0.0247   0.10555   0.10171  -0.1338   0.7527   0.0183
 -12.000   0.0294   0.10191   0.09808  -0.1362   0.7506   0.0184
 -11.750   0.0328   0.09781   0.09400  -0.1389   0.7486   0.0185
 -11.500   0.0385   0.09426   0.09045  -0.1412   0.7465   0.0185
 -11.250   0.0428   0.09052   0.08671  -0.1423   0.7445   0.0188
 -11.000   0.0571   0.08928   0.08545  -0.1420   0.7425   0.0196
 -10.750   0.0628   0.08566   0.08181  -0.1448   0.7406   0.0193
 -10.500   0.0716   0.08284   0.07897  -0.1467   0.7387   0.0198
 -10.250   0.0763   0.07977   0.07594  -0.1483   0.7368   0.0202
 -10.000   0.0805   0.07654   0.07272  -0.1503   0.7346   0.0202
  -9.750   0.0811   0.07255   0.06876  -0.1527   0.7324   0.0218
  -9.500   0.0808   0.06826   0.06449  -0.1557   0.7303   0.0222
  -8.000  -0.0291   0.04185   0.03747  -0.1570   0.7163   0.0235
  -7.750  -0.0275   0.03938   0.03490  -0.1550   0.7142   0.0236
  -7.500  -0.0159   0.03778   0.03332  -0.1542   0.7124   0.0241
  -7.250  -0.0078   0.03617   0.03161  -0.1525   0.7106   0.0247
  -7.000   0.0017   0.03462   0.02994  -0.1509   0.7085   0.0252
  -6.750   0.0093   0.03273   0.02791  -0.1486   0.7066   0.0259
  -6.500  -0.0073   0.02514   0.01918  -0.1403   0.7045   0.0186
  -6.250   0.0080   0.02326   0.01702  -0.1385   0.7024   0.0186
  -6.000   0.0266   0.02099   0.01460  -0.1374   0.7005   0.0181
  -5.750   0.0475   0.01958   0.01294  -0.1363   0.6989   0.0182
  -5.500   0.0706   0.01841   0.01154  -0.1356   0.6973   0.0183
  -5.250   0.0946   0.01712   0.01005  -0.1351   0.6957   0.0188
  -5.000   0.1192   0.01607   0.00890  -0.1348   0.6941   0.0193
  -4.750   0.1414   0.01539   0.00821  -0.1339   0.6925   0.0197
  -4.500   0.1639   0.01489   0.00770  -0.1331   0.6906   0.0205
  -4.250   0.1867   0.01446   0.00725  -0.1323   0.6886   0.0216
  -4.000   0.2098   0.01405   0.00678  -0.1316   0.6867   0.0228
  -3.750   0.2311   0.01350   0.00621  -0.1306   0.6850   0.0243
  -3.500   0.2552   0.01323   0.00593  -0.1301   0.6835   0.0272
  -3.250   0.2786   0.01287   0.00551  -0.1294   0.6820   0.0300
  -3.000   0.3028   0.01260   0.00522  -0.1290   0.6805   0.0341
  -2.750   0.3269   0.01239   0.00498  -0.1285   0.6790   0.0427
  -2.500   0.3477   0.01208   0.00479  -0.1274   0.6775   0.0662
  -2.250   0.3639   0.01147   0.00466  -0.1256   0.6757   0.1891
  -2.000   0.3731   0.01055   0.00453  -0.1227   0.6739   0.4220
  -1.750   0.3789   0.00978   0.00453  -0.1184   0.6719   0.6451
  -1.500   0.3977   0.00975   0.00473  -0.1164   0.6703   0.7390
  -1.250   0.4215   0.00988   0.00485  -0.1154   0.6688   0.7735
  -1.000   0.4471   0.01000   0.00493  -0.1150   0.6675   0.7910
  -0.750   0.4730   0.01015   0.00503  -0.1145   0.6662   0.8062
  -0.500   0.4988   0.01038   0.00524  -0.1140   0.6648   0.8230
  -0.250   0.5204   0.01062   0.00552  -0.1124   0.6634   0.8412
   0.000   0.5409   0.01074   0.00565  -0.1109   0.6617   0.8526
   0.250   0.5637   0.01083   0.00576  -0.1099   0.6600   0.8612
   0.500   0.5866   0.01088   0.00580  -0.1091   0.6581   0.8681
   0.750   0.6123   0.01091   0.00582  -0.1088   0.6566   0.8724
   1.000   0.6379   0.01096   0.00583  -0.1087   0.6552   0.8765
   1.250   0.6637   0.01101   0.00584  -0.1085   0.6538   0.8804
   1.500   0.6914   0.01103   0.00583  -0.1088   0.6525   0.8833
   1.750   0.7205   0.01108   0.00585  -0.1094   0.6513   0.8863
   2.000   0.7498   0.01121   0.00593  -0.1101   0.6498   0.8894
   2.250   0.7704   0.01130   0.00605  -0.1090   0.6483   0.8934
   2.500   0.7904   0.01139   0.00617  -0.1077   0.6465   0.8972
   2.750   0.8138   0.01146   0.00628  -0.1072   0.6449   0.9005
   3.000   0.8376   0.01155   0.00639  -0.1068   0.6432   0.9041
   3.250   0.8619   0.01162   0.00647  -0.1065   0.6416   0.9080
   3.500   0.8870   0.01167   0.00652  -0.1063   0.6400   0.9116
   3.750   0.9164   0.01171   0.00657  -0.1070   0.6386   0.9145
   4.000   0.9463   0.01178   0.00664  -0.1079   0.6374   0.9176
   4.250   0.9770   0.01187   0.00673  -0.1090   0.6361   0.9207
   4.500   1.0055   0.01205   0.00690  -0.1096   0.6345   0.9242
   4.750   1.0256   0.01219   0.00714  -0.1086   0.6327   0.9286
   5.000   1.0501   0.01233   0.00736  -0.1085   0.6306   0.9329
   5.250   1.0758   0.01245   0.00754  -0.1087   0.6285   0.9373
   5.500   1.1037   0.01254   0.00768  -0.1093   0.6265   0.9416
   5.750   1.1396   0.01253   0.00771  -0.1115   0.6245   0.9450
   6.000   1.1765   0.01254   0.00773  -0.1139   0.6227   0.9486
   6.250   1.2145   0.01259   0.00778  -0.1166   0.6208   0.9520
   6.500   1.2455   0.01276   0.00806  -0.1181   0.6179   0.9573
   6.750   1.2797   0.01290   0.00830  -0.1203   0.6147   0.9626
   7.000   1.3180   0.01284   0.00831  -0.1232   0.6110   0.9676
   7.250   1.3602   0.01268   0.00815  -0.1266   0.6076   0.9718
   7.500   1.3985   0.01273   0.00826  -0.1295   0.6037   0.9784
   7.750   1.4262   0.01284   0.00848  -0.1303   0.5985   1.0000
   8.000   1.4530   0.01260   0.00822  -0.1305   0.5925   1.0000
   8.250   1.4633   0.01269   0.00839  -0.1276   0.5845   1.0000
   8.500   1.4825   0.01258   0.00823  -0.1262   0.5761   1.0000
   8.750   1.4876   0.01292   0.00869  -0.1227   0.5690   1.0000
   9.000   1.5064   0.01308   0.00887  -0.1216   0.5627   1.0000
   9.250   1.5167   0.01356   0.00946  -0.1193   0.5556   1.0000
   9.500   1.5307   0.01396   0.00987  -0.1177   0.5468   1.0000
   9.750   1.5367   0.01476   0.01075  -0.1151   0.5353   1.0000
  10.000   1.5432   0.01570   0.01173  -0.1128   0.5222   1.0000
  10.250   1.5474   0.01686   0.01291  -0.1104   0.5063   1.0000
  10.500   1.5451   0.01849   0.01449  -0.1073   0.4834   1.0000
  10.750   1.5351   0.02070   0.01659  -0.1036   0.4552   1.0000
  11.000   1.5082   0.02408   0.01974  -0.0981   0.4165   1.0000
  11.250   1.4984   0.02654   0.02213  -0.0948   0.3937   1.0000
  11.500   1.4784   0.02989   0.02532  -0.0907   0.3629   1.0000
  11.750   1.4586   0.03340   0.02867  -0.0869   0.3308   1.0000
  12.000   1.4406   0.03697   0.03207  -0.0836   0.2995   1.0000
  12.250   1.4321   0.03986   0.03486  -0.0812   0.2745   1.0000
  12.500   1.4110   0.04394   0.03869  -0.0780   0.2361   1.0000
  12.750   1.4080   0.04652   0.04119  -0.0763   0.2145   1.0000
  13.000   1.3960   0.04996   0.04442  -0.0740   0.1820   1.0000
  13.250   1.3892   0.05299   0.04729  -0.0722   0.1543   1.0000
  13.500   1.3858   0.05576   0.04994  -0.0708   0.1314   1.0000
  13.750   1.3812   0.05868   0.05272  -0.0693   0.1077   1.0000
  14.000   1.3770   0.06162   0.05552  -0.0680   0.0855   1.0000
  14.250   1.3759   0.06433   0.05813  -0.0669   0.0684   1.0000
  14.500   1.3767   0.06687   0.06063  -0.0659   0.0569   1.0000
  14.750   1.3787   0.06932   0.06306  -0.0651   0.0484   1.0000
  15.000   1.3795   0.07197   0.06569  -0.0643   0.0416   1.0000
  15.250   1.3847   0.07419   0.06795  -0.0638   0.0382   1.0000
  15.500   1.3846   0.07699   0.07075  -0.0631   0.0341   1.0000
  15.750   1.3910   0.07913   0.07298  -0.0627   0.0320   1.0000
  16.000   1.3954   0.08146   0.07534  -0.0624   0.0293   1.0000
  16.250   1.3936   0.08457   0.07848  -0.0618   0.0268   1.0000
  16.500   1.4006   0.08667   0.08068  -0.0616   0.0251   1.0000
  16.750   1.4031   0.08932   0.08337  -0.0614   0.0229   1.0000
  17.000   1.4013   0.09253   0.08662  -0.0611   0.0208   1.0000
  17.250   1.4079   0.09474   0.08891  -0.0610   0.0185   1.0000
  17.500   1.4036   0.09830   0.09250  -0.0608   0.0167   1.0000
  17.750   1.4035   0.10139   0.09569  -0.0608   0.0154   1.0000
  18.000   1.4094   0.10372   0.09807  -0.0609   0.0140   1.0000
  18.250   1.4031   0.10768   0.10208  -0.0610   0.0128   1.0000
  18.500   1.4010   0.11115   0.10566  -0.0612   0.0121   1.0000
  18.750   1.4048   0.11385   0.10843  -0.0616   0.0111   1.0000
  19.000   1.4051   0.11702   0.11168  -0.0620   0.0105   1.0000
  19.250   1.4010   0.12082   0.11555  -0.0626   0.0101   1.0000
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