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WORTMANN FX 72-MS-150B AIRFOIL (fx72150b-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 72-MS-150B AIRFOIL (fx72150b-il)
Reynolds number: 1,000,000
Max Cl/Cd: 150.98 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx72150b-il-1000000-n5.txt
Download as CSV file: xf-fx72150b-il-1000000-n5.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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.750   0.3129   0.08807   0.08427  -0.1598   0.6203   0.0101
  -9.500   0.3205   0.08568   0.08188  -0.1608   0.6170   0.0102
  -9.250   0.3267   0.08308   0.07927  -0.1620   0.6137   0.0103
  -9.000   0.3350   0.08085   0.07703  -0.1629   0.6109   0.0103
  -8.750   0.3426   0.07847   0.07466  -0.1638   0.6083   0.0103
  -8.500   0.3506   0.07623   0.07242  -0.1647   0.6053   0.0103
  -8.250   0.3592   0.07411   0.07030  -0.1654   0.6023   0.0103
  -8.000   0.3701   0.07266   0.06884  -0.1658   0.5991   0.0100
  -7.750   0.3769   0.07049   0.06667  -0.1664   0.5962   0.0095
  -7.500   0.3832   0.06816   0.06435  -0.1671   0.5938   0.0091
  -7.250   0.3900   0.06591   0.06212  -0.1678   0.5914   0.0092
  -7.000   0.3959   0.06369   0.05991  -0.1684   0.5887   0.0094
  -6.750   0.4007   0.06151   0.05774  -0.1688   0.5858   0.0096
  -6.500   0.4039   0.05942   0.05567  -0.1688   0.5832   0.0095
  -6.250   0.4034   0.05747   0.05373  -0.1683   0.5805   0.0098
  -6.000   0.4097   0.05509   0.05136  -0.1697   0.5783   0.0099
  -5.750   0.4187   0.05254   0.04883  -0.1719   0.5761   0.0098
  -5.500   0.4898   0.01654   0.01166  -0.2346   0.5749   0.0101
  -5.250   0.5274   0.01446   0.00915  -0.2385   0.5722   0.0103
  -5.000   0.5615   0.01322   0.00761  -0.2409   0.5695   0.0105
  -4.750   0.5930   0.01257   0.00680  -0.2423   0.5669   0.0108
  -4.250   0.6537   0.01185   0.00589  -0.2442   0.5624   0.0111
  -4.000   0.6841   0.01154   0.00549  -0.2451   0.5605   0.0113
  -3.750   0.7144   0.01125   0.00513  -0.2460   0.5585   0.0115
  -3.500   0.7446   0.01099   0.00480  -0.2468   0.5565   0.0118
  -3.250   0.7746   0.01079   0.00452  -0.2475   0.5544   0.0121
  -3.000   0.8042   0.01063   0.00430  -0.2481   0.5524   0.0125
  -2.750   0.8336   0.01050   0.00410  -0.2487   0.5504   0.0128
  -2.250   0.8935   0.01019   0.00371  -0.2502   0.5468   0.0137
  -2.000   0.9231   0.01009   0.00360  -0.2508   0.5453   0.0142
  -1.750   0.9525   0.01003   0.00351  -0.2514   0.5437   0.0150
  -1.500   0.9817   0.00997   0.00343  -0.2519   0.5419   0.0157
  -1.250   1.0109   0.00993   0.00336  -0.2524   0.5400   0.0168
  -1.000   1.0397   0.00992   0.00333  -0.2529   0.5381   0.0182
  -0.750   1.0683   0.00992   0.00331  -0.2533   0.5362   0.0200
  -0.500   1.0964   0.00995   0.00333  -0.2536   0.5344   0.0228
  -0.250   1.1245   0.00998   0.00334  -0.2539   0.5325   0.0261
   0.000   1.1531   0.00998   0.00334  -0.2544   0.5312   0.0304
   0.250   1.1821   0.00996   0.00337  -0.2549   0.5302   0.0467
   0.500   1.2111   0.00992   0.00341  -0.2555   0.5290   0.0786
   0.750   1.2405   0.00985   0.00347  -0.2562   0.5277   0.1444
   1.000   1.2706   0.00970   0.00355  -0.2572   0.5263   0.2664
   1.250   1.3006   0.00955   0.00369  -0.2582   0.5249   0.4239
   1.500   1.3280   0.00962   0.00380  -0.2584   0.5235   0.4608
   1.750   1.3551   0.00970   0.00391  -0.2585   0.5221   0.4853
   2.250   1.4085   0.00991   0.00415  -0.2587   0.5194   0.5146
   2.500   1.4346   0.01004   0.00426  -0.2586   0.5179   0.5211
   2.750   1.4603   0.01018   0.00440  -0.2586   0.5162   0.5262
   3.000   1.4870   0.01027   0.00451  -0.2587   0.5151   0.5330
   3.250   1.5135   0.01036   0.00462  -0.2587   0.5140   0.5382
   3.500   1.5399   0.01046   0.00474  -0.2588   0.5128   0.5429
   3.750   1.5660   0.01056   0.00487  -0.2588   0.5116   0.5471
   4.000   1.5917   0.01067   0.00500  -0.2588   0.5105   0.5511
   4.250   1.6171   0.01080   0.00514  -0.2587   0.5093   0.5549
   4.500   1.6422   0.01092   0.00530  -0.2585   0.5081   0.5591
   4.750   1.6668   0.01106   0.00546  -0.2583   0.5069   0.5642
   5.000   1.6910   0.01120   0.00563  -0.2580   0.5057   0.5697
   5.250   1.7139   0.01136   0.00581  -0.2574   0.5045   0.5747
   5.500   1.7355   0.01152   0.00600  -0.2566   0.5033   0.5802
   5.750   1.7562   0.01171   0.00621  -0.2556   0.5019   0.5860
   6.000   1.7772   0.01191   0.00645  -0.2548   0.5005   0.5914
   6.250   1.7997   0.01206   0.00666  -0.2542   0.4994   0.5976
   6.500   1.8219   0.01223   0.00688  -0.2536   0.4982   0.6045
   6.750   1.8437   0.01241   0.00711  -0.2529   0.4967   0.6115
   7.000   1.8638   0.01262   0.00739  -0.2519   0.4940   0.6199
   7.250   1.8816   0.01291   0.00771  -0.2506   0.4904   0.6288
   7.500   1.8968   0.01331   0.00812  -0.2489   0.4866   0.6391
   7.750   1.9162   0.01360   0.00848  -0.2479   0.4838   0.6498
   8.000   1.9361   0.01387   0.00882  -0.2471   0.4810   0.6609
   8.250   1.9536   0.01424   0.00925  -0.2458   0.4770   0.6737
   8.500   1.9670   0.01479   0.00983  -0.2440   0.4721   0.6899
   8.750   1.9834   0.01524   0.01038  -0.2427   0.4674   0.7144
   9.000   1.9992   0.01572   0.01099  -0.2414   0.4596   0.7732
   9.250   2.0070   0.01625   0.01174  -0.2387   0.4511   1.0000
   9.500   2.0111   0.01743   0.01287  -0.2358   0.4330   1.0000
   9.750   2.0046   0.01934   0.01468  -0.2317   0.4132   1.0000
  10.000   1.9985   0.02139   0.01667  -0.2278   0.3938   1.0000
  10.250   1.9782   0.02457   0.01970  -0.2225   0.3613   1.0000
  10.500   1.9595   0.02788   0.02292  -0.2178   0.3404   1.0000
  10.750   1.9433   0.03126   0.02623  -0.2137   0.3176   1.0000
  11.000   1.9193   0.03565   0.03052  -0.2093   0.2921   1.0000
  11.250   1.9001   0.03989   0.03468  -0.2057   0.2700   1.0000
  11.500   1.8764   0.04489   0.03960  -0.2022   0.2456   1.0000
  11.750   1.8513   0.05028   0.04489  -0.1989   0.2198   1.0000
  12.000   1.8292   0.05562   0.05014  -0.1962   0.1959   1.0000
  12.250   1.8070   0.06119   0.05562  -0.1937   0.1725   1.0000
  12.500   1.7890   0.06646   0.06080  -0.1917   0.1491   1.0000
  12.750   1.7734   0.07157   0.06582  -0.1901   0.1273   1.0000
  13.000   1.7634   0.07607   0.07026  -0.1888   0.1099   1.0000
  13.250   1.7513   0.08098   0.07510  -0.1876   0.0897   1.0000
  13.500   1.7329   0.08683   0.08080  -0.1864   0.0627   1.0000
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