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WORTMANN FX 72-MS-150A AIRFOIL (fx72150a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 72-MS-150A AIRFOIL (fx72150a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 160.23 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx72150a-il-1000000.txt
Download as CSV file: xf-fx72150a-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 72-MS-150A 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.500   0.2205   0.08639   0.08298  -0.1438   0.6710   0.0124
  -9.250   0.2280   0.08401   0.08058  -0.1447   0.6667   0.0127
  -9.000   0.2355   0.08166   0.07821  -0.1456   0.6624   0.0128
  -8.750   0.2397   0.07858   0.07515  -0.1473   0.6590   0.0133
  -8.000   0.2545   0.07046   0.06701  -0.1504   0.6469   0.0137
  -7.750   0.2604   0.06785   0.06442  -0.1516   0.6435   0.0136
  -7.500   0.2720   0.06641   0.06298  -0.1517   0.6397   0.0138
  -7.250   0.2796   0.06441   0.06098  -0.1523   0.6357   0.0139
  -7.000   0.2876   0.06275   0.05931  -0.1526   0.6316   0.0144
  -6.750   0.2925   0.06062   0.05718  -0.1530   0.6281   0.0146
  -6.500   0.2952   0.05844   0.05503  -0.1532   0.6248   0.0150
  -6.250   0.2975   0.05622   0.05282  -0.1539   0.6213   0.0154
  -6.000   0.2967   0.03412   0.03090  -0.1479   0.6101   0.0164
  -5.750   0.3069   0.03182   0.02861  -0.1499   0.6073   0.0165
  -5.500   0.3194   0.02930   0.02609  -0.1529   0.6045   0.0167
  -5.250   0.3345   0.02612   0.02289  -0.1580   0.6018   0.0169
  -5.000   0.3612   0.01997   0.01662  -0.1726   0.5995   0.0171
  -4.750   0.4039   0.01268   0.00871  -0.1880   0.5974   0.0192
  -4.500   0.4331   0.01001   0.00587  -0.1926   0.5950   0.0196
  -4.250   0.4620   0.00899   0.00477  -0.1949   0.5929   0.0198
  -4.000   0.5109   0.02066   0.01607  -0.2069   0.5941   0.0202
  -3.750   0.5424   0.01926   0.01450  -0.2089   0.5918   0.0210
  -3.500   0.5788   0.01692   0.01170  -0.2116   0.5893   0.0230
  -3.250   0.6085   0.01603   0.01075  -0.2127   0.5867   0.0235
  -3.000   0.6461   0.01266   0.00674  -0.2146   0.5841   0.0169
  -2.750   0.6768   0.01156   0.00548  -0.2153   0.5812   0.0150
  -2.500   0.7076   0.01079   0.00457  -0.2161   0.5785   0.0144
  -2.250   0.7381   0.01039   0.00413  -0.2169   0.5766   0.0146
  -2.000   0.7683   0.01011   0.00382  -0.2176   0.5743   0.0151
  -1.750   0.7982   0.00991   0.00358  -0.2182   0.5720   0.0158
  -1.500   0.8278   0.00977   0.00340  -0.2187   0.5697   0.0162
  -1.250   0.8577   0.00959   0.00317  -0.2194   0.5675   0.0168
  -1.000   0.8867   0.00954   0.00308  -0.2198   0.5651   0.0175
  -0.750   0.9156   0.00954   0.00304  -0.2202   0.5627   0.0185
  -0.500   0.9450   0.00947   0.00298  -0.2207   0.5613   0.0203
  -0.250   0.9743   0.00942   0.00293  -0.2211   0.5597   0.0231
   0.000   1.0045   0.00926   0.00287  -0.2219   0.5579   0.0663
   0.250   1.0362   0.00881   0.00289  -0.2233   0.5562   0.2773
   0.500   1.0661   0.00859   0.00302  -0.2242   0.5544   0.4558
   0.750   1.0942   0.00865   0.00310  -0.2245   0.5526   0.4812
   1.000   1.1220   0.00875   0.00320  -0.2246   0.5507   0.5062
   1.250   1.1495   0.00888   0.00334  -0.2248   0.5484   0.5301
   1.500   1.1773   0.00904   0.00346  -0.2249   0.5464   0.5420
   1.750   1.2053   0.00909   0.00356  -0.2252   0.5454   0.5527
   2.000   1.2333   0.00917   0.00364  -0.2254   0.5443   0.5591
   2.250   1.2612   0.00923   0.00372  -0.2256   0.5431   0.5649
   2.500   1.2890   0.00931   0.00382  -0.2258   0.5418   0.5709
   2.750   1.3166   0.00940   0.00391  -0.2260   0.5403   0.5752
   3.000   1.3442   0.00949   0.00400  -0.2262   0.5388   0.5789
   3.250   1.3716   0.00957   0.00411  -0.2264   0.5373   0.5836
   3.500   1.3988   0.00968   0.00423  -0.2265   0.5358   0.5886
   3.750   1.4259   0.00981   0.00435  -0.2267   0.5343   0.5934
   4.000   1.4531   0.00995   0.00449  -0.2268   0.5328   0.5982
   4.250   1.4805   0.01012   0.00468  -0.2271   0.5310   0.6036
   4.500   1.5078   0.01026   0.00484  -0.2273   0.5298   0.6096
   4.750   1.5345   0.01032   0.00496  -0.2273   0.5286   0.6159
   5.000   1.5601   0.01033   0.00503  -0.2272   0.5257   0.6229
   5.250   1.5857   0.01038   0.00512  -0.2271   0.5225   0.6300
   5.500   1.6116   0.01046   0.00525  -0.2270   0.5202   0.6376
   5.750   1.6369   0.01059   0.00539  -0.2268   0.5179   0.6463
   6.000   1.6619   0.01080   0.00561  -0.2267   0.5141   0.6551
   6.500   1.7116   0.01091   0.00588  -0.2262   0.5093   0.6774
   6.750   1.7361   0.01098   0.00603  -0.2259   0.5063   0.6920
   7.000   1.7583   0.01110   0.00619  -0.2252   0.5016   0.7107
   7.250   1.7798   0.01125   0.00640  -0.2243   0.4966   0.7360
   7.500   1.8010   0.01124   0.00659  -0.2234   0.4898   0.8043
   7.750   1.8104   0.01133   0.00683  -0.2201   0.4822   1.0000
   8.000   1.8269   0.01156   0.00708  -0.2183   0.4719   1.0000
   8.250   1.8393   0.01194   0.00744  -0.2159   0.4575   1.0000
   8.500   1.8378   0.01284   0.00819  -0.2112   0.4254   1.0000
   8.750   1.8245   0.01446   0.00960  -0.2050   0.3892   1.0000
   9.000   1.7964   0.01718   0.01204  -0.1974   0.3415   1.0000
   9.250   1.7687   0.02039   0.01502  -0.1907   0.2974   1.0000
   9.500   1.7453   0.02373   0.01817  -0.1852   0.2611   1.0000
   9.750   1.7197   0.02756   0.02183  -0.1801   0.2256   1.0000
  10.000   1.6956   0.03164   0.02576  -0.1757   0.1927   1.0000
  10.250   1.6765   0.03563   0.02964  -0.1722   0.1644   1.0000
  10.500   1.6523   0.04045   0.03431  -0.1688   0.1311   1.0000
  10.750   1.6300   0.04538   0.03909  -0.1659   0.0994   1.0000
  11.000   1.6045   0.05094   0.04448  -0.1633   0.0633   1.0000
  11.250   1.5788   0.05681   0.05017  -0.1609   0.0264   1.0000
  11.500   1.5735   0.06052   0.05384  -0.1597   0.0133   1.0000
  11.750   1.5793   0.06294   0.05630  -0.1590   0.0122   1.0000
  12.000   1.5844   0.06548   0.05889  -0.1583   0.0114   1.0000
  12.250   1.5903   0.06797   0.06142  -0.1577   0.0110   1.0000
  12.500   1.5973   0.07032   0.06383  -0.1572   0.0107   1.0000
  12.750   1.6028   0.07291   0.06647  -0.1567   0.0104   1.0000
  13.000   1.6089   0.07541   0.06902  -0.1562   0.0102   1.0000
  13.250   1.6141   0.07808   0.07174  -0.1558   0.0100   1.0000
  13.500   1.6190   0.08080   0.07451  -0.1554   0.0097   1.0000
  13.750   1.6242   0.08349   0.07725  -0.1550   0.0095   1.0000
  14.000   1.6274   0.08651   0.08033  -0.1547   0.0094   1.0000
  14.250   1.6307   0.08951   0.08339  -0.1544   0.0092   1.0000
  14.500   1.6333   0.09261   0.08657  -0.1541   0.0090   1.0000
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