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WORTMANN FX 72-MS-150B AIRFOIL (fx72150b-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 72-MS-150B AIRFOIL (fx72150b-il)
Reynolds number: 500,000
Max Cl/Cd: 117.1 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx72150b-il-500000.txt
Download as CSV file: xf-fx72150b-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 72-MS-150B AIRFOIL                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.000   0.2714   0.10180   0.09788  -0.1547   0.7294   0.0158
 -10.750   0.2732   0.09975   0.09577  -0.1566   0.7248   0.0160
 -10.500   0.2782   0.09765   0.09369  -0.1580   0.7198   0.0160
 -10.250   0.2934   0.09450   0.09051  -0.1580   0.7147   0.0162
 -10.000   0.3047   0.09240   0.08835  -0.1583   0.7100   0.0164
  -9.750   0.3137   0.09018   0.08614  -0.1592   0.7054   0.0165
  -9.500   0.3233   0.08824   0.08419  -0.1600   0.7006   0.0170
  -9.250   0.3322   0.08615   0.08207  -0.1608   0.6961   0.0175
  -9.000   0.3407   0.08407   0.07995  -0.1616   0.6921   0.0177
  -8.750   0.3491   0.08191   0.07781  -0.1625   0.6879   0.0183
  -8.500   0.3568   0.07973   0.07562  -0.1634   0.6836   0.0187
  -8.250   0.3584   0.07762   0.07350  -0.1652   0.6797   0.0191
  -8.000   0.3625   0.07553   0.07139  -0.1665   0.6759   0.0192
  -7.750   0.3690   0.07289   0.06878  -0.1673   0.6721   0.0193
  -7.500   0.3830   0.07088   0.06676  -0.1668   0.6681   0.0196
  -7.250   0.3935   0.06909   0.06494  -0.1671   0.6643   0.0198
  -7.000   0.4024   0.06733   0.06313  -0.1674   0.6606   0.0202
  -6.750   0.4100   0.06546   0.06130  -0.1679   0.6572   0.0208
  -6.500   0.4167   0.06355   0.05942  -0.1683   0.6536   0.0212
  -6.250   0.4200   0.06156   0.05744  -0.1685   0.6501   0.0222
  -6.000   0.4170   0.05889   0.05478  -0.1718   0.6468   0.0228
  -5.750   0.4266   0.05588   0.05174  -0.1751   0.6435   0.0230
  -5.500   0.4380   0.05418   0.05007  -0.1747   0.6405   0.0232
  -5.250   0.4514   0.05288   0.04878  -0.1745   0.6373   0.0237
  -5.000   0.4661   0.05098   0.04688  -0.1764   0.6342   0.0242
  -4.750   0.4833   0.04859   0.04446  -0.1798   0.6313   0.0251
  -4.500   0.5462   0.03723   0.03278  -0.2090   0.6285   0.0271
  -4.250   0.5621   0.03566   0.03130  -0.2089   0.6259   0.0274
  -4.000   0.5877   0.03385   0.02946  -0.2118   0.6232   0.0279
  -3.750   0.6212   0.03130   0.02680  -0.2171   0.6205   0.0289
  -3.500   0.6799   0.02546   0.02041  -0.2297   0.6179   0.0325
  -3.250   0.7104   0.02422   0.01909  -0.2320   0.6155   0.0335
  -3.000   0.7545   0.02170   0.01610  -0.2374   0.6130   0.0382
  -2.750   0.7854   0.02078   0.01512  -0.2391   0.6106   0.0402
  -2.500   0.8216   0.01936   0.01344  -0.2419   0.6083   0.0454
  -2.250   0.8564   0.01842   0.01223  -0.2440   0.6058   0.0521
  -2.000   0.9031   0.01465   0.00761  -0.2470   0.6037   0.0270
  -1.500   0.9658   0.01332   0.00612  -0.2491   0.5995   0.0279
  -1.250   0.9967   0.01309   0.00584  -0.2500   0.5973   0.0294
  -1.000   1.0277   0.01296   0.00565  -0.2509   0.5952   0.0313
  -0.750   1.0579   0.01274   0.00547  -0.2518   0.5933   0.0350
  -0.500   1.0881   0.01259   0.00531  -0.2526   0.5912   0.0397
  -0.250   1.1179   0.01250   0.00522  -0.2533   0.5891   0.0480
   0.000   1.1495   0.01227   0.00514  -0.2545   0.5870   0.1104
   0.250   1.1833   0.01178   0.00537  -0.2567   0.5851   0.4654
   0.500   1.2113   0.01191   0.00550  -0.2569   0.5833   0.5074
   0.750   1.2395   0.01210   0.00565  -0.2572   0.5815   0.5314
   1.000   1.2680   0.01235   0.00585  -0.2576   0.5795   0.5514
   1.250   1.2946   0.01248   0.00601  -0.2576   0.5780   0.5682
   1.500   1.3212   0.01263   0.00619  -0.2576   0.5764   0.5862
   1.750   1.3481   0.01277   0.00634  -0.2577   0.5748   0.5971
   2.000   1.3754   0.01292   0.00648  -0.2578   0.5732   0.6061
   2.250   1.4027   0.01304   0.00661  -0.2581   0.5716   0.6129
   2.500   1.4302   0.01317   0.00674  -0.2583   0.5702   0.6189
   2.750   1.4578   0.01332   0.00686  -0.2587   0.5688   0.6243
   3.000   1.4854   0.01346   0.00700  -0.2590   0.5675   0.6291
   3.250   1.5134   0.01364   0.00717  -0.2594   0.5661   0.6342
   3.500   1.5422   0.01388   0.00738  -0.2600   0.5646   0.6398
   3.750   1.5697   0.01409   0.00761  -0.2604   0.5634   0.6449
   4.000   1.5955   0.01424   0.00783  -0.2604   0.5623   0.6510
   4.250   1.6213   0.01442   0.00805  -0.2604   0.5609   0.6580
   4.500   1.6470   0.01457   0.00827  -0.2605   0.5595   0.6651
   4.750   1.6729   0.01474   0.00849  -0.2606   0.5579   0.6737
   5.000   1.6990   0.01490   0.00872  -0.2607   0.5564   0.6821
   5.250   1.7253   0.01508   0.00894  -0.2608   0.5551   0.6923
   5.500   1.7518   0.01526   0.00917  -0.2611   0.5538   0.7041
   5.750   1.7786   0.01543   0.00940  -0.2614   0.5526   0.7185
   6.000   1.8058   0.01562   0.00966  -0.2617   0.5515   0.7381
   6.250   1.8331   0.01579   0.00994  -0.2622   0.5503   0.7750
   6.500   1.8561   0.01585   0.01020  -0.2616   0.5489   1.0000
   6.750   1.8825   0.01620   0.01059  -0.2619   0.5476   1.0000
   7.000   1.9044   0.01645   0.01092  -0.2613   0.5462   1.0000
   7.250   1.9262   0.01670   0.01125  -0.2607   0.5445   1.0000
   7.500   1.9474   0.01692   0.01154  -0.2600   0.5421   1.0000
   7.750   1.9690   0.01704   0.01169  -0.2593   0.5390   1.0000
   8.000   1.9932   0.01715   0.01180  -0.2590   0.5361   1.0000
   8.250   2.0196   0.01736   0.01202  -0.2593   0.5335   1.0000
   8.500   2.0398   0.01768   0.01239  -0.2584   0.5305   1.0000
   8.750   2.0506   0.01792   0.01276  -0.2558   0.5272   1.0000
   9.000   2.0635   0.01814   0.01305  -0.2535   0.5239   1.0000
   9.250   2.0786   0.01831   0.01325  -0.2515   0.5206   1.0000
   9.500   2.1025   0.01846   0.01336  -0.2513   0.5160   1.0000
   9.750   2.0951   0.01902   0.01408  -0.2455   0.5123   1.0000
  10.000   2.0954   0.01958   0.01472  -0.2414   0.5073   1.0000
  10.250   2.1046   0.02000   0.01512  -0.2388   0.5014   1.0000
  10.500   2.1004   0.02105   0.01631  -0.2345   0.4959   1.0000
  10.750   2.1014   0.02205   0.01738  -0.2311   0.4896   1.0000
  11.000   2.1084   0.02298   0.01834  -0.2287   0.4839   1.0000
  11.250   2.1073   0.02441   0.01989  -0.2255   0.4772   1.0000
  11.500   2.1100   0.02572   0.02120  -0.2228   0.4696   1.0000
  11.750   2.1060   0.02762   0.02324  -0.2196   0.4599   1.0000
  12.000   2.1026   0.02961   0.02530  -0.2166   0.4490   1.0000
  12.250   2.0949   0.03209   0.02782  -0.2133   0.4339   1.0000
  12.500   2.0785   0.03547   0.03116  -0.2095   0.4161   1.0000
  12.750   2.0579   0.03954   0.03518  -0.2056   0.3970   1.0000
  13.000   2.0320   0.04445   0.04003  -0.2017   0.3693   1.0000
  13.250   2.0007   0.05026   0.04574  -0.1979   0.3490   1.0000
  13.500   1.9743   0.05585   0.05129  -0.1948   0.3295   1.0000
  13.750   1.9471   0.06179   0.05717  -0.1920   0.3065   1.0000
  14.000   1.9193   0.06810   0.06340  -0.1895   0.2858   1.0000
  14.250   1.8948   0.07422   0.06947  -0.1875   0.2653   1.0000
  14.500   1.8704   0.08052   0.07568  -0.1857   0.2421   1.0000
  14.750   1.8464   0.08695   0.08201  -0.1843   0.2191   1.0000
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