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NACA/LANGLEY SYMMETRICAL (n0011sc-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA/LANGLEY SYMMETRICAL (n0011sc-il)
Reynolds number: 1,000,000
Max Cl/Cd: 58.98 at α=8°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n0011sc-il-1000000.txt
Download as CSV file: xf-n0011sc-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA/LANGLEY SYMMETRICAL                        
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.0275   0.09411   0.09149  -0.0447   1.0000   0.0178
 -17.500  -1.0870   0.07856   0.07559  -0.0545   1.0000   0.0175
 -17.250  -1.1184   0.06942   0.06626  -0.0600   1.0000   0.0175
 -17.000  -1.1415   0.06237   0.05904  -0.0639   1.0000   0.0175
 -16.750  -1.1565   0.05711   0.05363  -0.0663   1.0000   0.0174
 -16.500  -1.1769   0.05179   0.04816  -0.0680   1.0000   0.0175
 -16.250  -1.1907   0.04779   0.04405  -0.0684   1.0000   0.0177
 -16.000  -1.2019   0.04449   0.04063  -0.0679   1.0000   0.0178
 -15.750  -1.2068   0.04214   0.03821  -0.0669   1.0000   0.0179
 -15.500  -1.2176   0.03938   0.03530  -0.0652   1.0000   0.0178
 -15.250  -1.2216   0.03750   0.03334  -0.0631   1.0000   0.0180
 -15.000  -1.2270   0.03559   0.03132  -0.0606   1.0000   0.0180
 -14.750  -1.2319   0.03385   0.02946  -0.0576   1.0000   0.0180
 -14.500  -1.2302   0.03281   0.02838  -0.0549   1.0000   0.0183
 -14.250  -1.2306   0.03163   0.02712  -0.0518   1.0000   0.0183
 -14.000  -1.2295   0.03065   0.02607  -0.0486   1.0000   0.0186
 -13.750  -1.2291   0.02964   0.02498  -0.0450   1.0000   0.0187
 -13.500  -1.2293   0.02861   0.02386  -0.0413   1.0000   0.0187
 -13.250  -1.2293   0.02764   0.02279  -0.0372   1.0000   0.0189
 -13.000  -1.2274   0.02687   0.02194  -0.0333   1.0000   0.0190
 -12.750  -1.2255   0.02616   0.02115  -0.0292   1.0000   0.0192
 -12.500  -1.2248   0.02536   0.02025  -0.0248   1.0000   0.0193
 -12.250  -1.2236   0.02467   0.01949  -0.0203   1.0000   0.0194
 -12.000  -1.2227   0.02404   0.01877  -0.0156   1.0000   0.0195
 -11.750  -1.2225   0.02348   0.01814  -0.0106   1.0000   0.0196
 -11.500  -1.2218   0.02300   0.01758  -0.0057   1.0000   0.0198
 -11.250  -1.2029   0.02230   0.01679  -0.0045   0.9991   0.0199
 -11.000  -1.1809   0.02164   0.01605  -0.0039   0.9979   0.0201
 -10.750  -1.1570   0.02111   0.01545  -0.0037   0.9967   0.0203
 -10.500  -1.1337   0.02034   0.01459  -0.0034   0.9955   0.0205
 -10.250  -1.1121   0.01933   0.01351  -0.0029   0.9944   0.0210
 -10.000  -1.0924   0.01869   0.01284  -0.0017   0.9928   0.0213
  -9.750  -1.0709   0.01822   0.01234  -0.0007   0.9911   0.0217
  -9.500  -1.0474   0.01773   0.01181  -0.0002   0.9895   0.0219
  -9.250  -1.0215   0.01733   0.01139  -0.0001   0.9882   0.0225
  -9.000  -0.9949   0.01693   0.01094  -0.0002   0.9871   0.0230
  -8.750  -0.9677   0.01655   0.01052  -0.0003   0.9862   0.0234
  -8.500  -0.9393   0.01626   0.01019  -0.0007   0.9855   0.0239
  -8.250  -0.9122   0.01570   0.00959  -0.0009   0.9848   0.0244
  -8.000  -0.8969   0.01516   0.00903   0.0015   0.9815   0.0251
  -7.750  -0.8736   0.01484   0.00870   0.0023   0.9794   0.0258
  -7.500  -0.8476   0.01451   0.00836   0.0025   0.9779   0.0264
  -7.250  -0.8194   0.01423   0.00805   0.0023   0.9767   0.0274
  -7.000  -0.7900   0.01397   0.00777   0.0018   0.9758   0.0281
  -6.750  -0.7623   0.01350   0.00730   0.0016   0.9749   0.0296
  -6.500  -0.7320   0.01325   0.00705   0.0009   0.9743   0.0309
  -6.250  -0.7007   0.01304   0.00683   0.0000   0.9737   0.0323
  -6.000  -0.6889   0.01271   0.00650   0.0035   0.9690   0.0338
  -5.750  -0.6631   0.01246   0.00627   0.0039   0.9669   0.0357
  -5.500  -0.6344   0.01226   0.00606   0.0036   0.9655   0.0375
  -5.250  -0.6054   0.01195   0.00578   0.0033   0.9643   0.0407
  -5.000  -0.5745   0.01175   0.00558   0.0026   0.9634   0.0434
  -4.750  -0.5438   0.01146   0.00534   0.0019   0.9626   0.0482
  -4.500  -0.5122   0.01121   0.00513   0.0010   0.9619   0.0535
  -4.250  -0.4800   0.01097   0.00494  -0.0001   0.9613   0.0609
  -4.000  -0.4680   0.01081   0.00480   0.0035   0.9557   0.0663
  -3.750  -0.4406   0.01056   0.00462   0.0036   0.9536   0.0777
  -3.500  -0.4113   0.01028   0.00444   0.0032   0.9520   0.0936
  -3.250  -0.3803   0.00999   0.00425   0.0025   0.9508   0.1133
  -3.000  -0.3487   0.00967   0.00407   0.0016   0.9499   0.1411
  -2.750  -0.3162   0.00932   0.00388   0.0005   0.9490   0.1768
  -2.500  -0.2836   0.00892   0.00369  -0.0007   0.9483   0.2231
  -2.250  -0.2510   0.00845   0.00348  -0.0019   0.9477   0.2851
  -2.000  -0.2456   0.00816   0.00339   0.0032   0.9400   0.3398
  -1.750  -0.2199   0.00753   0.00315   0.0035   0.9379   0.4390
  -1.500  -0.1945   0.00666   0.00280   0.0040   0.9360   0.5746
  -1.250  -0.1657   0.00564   0.00233   0.0041   0.9336   0.7149
  -1.000  -0.1631   0.00520   0.00216   0.0103   0.9236   0.7847
  -0.750  -0.1194   0.00485   0.00204   0.0071   0.9205   0.8467
  -0.500  -0.0646   0.00473   0.00200   0.0013   0.9183   0.8744
  -0.250  -0.0449   0.00472   0.00202   0.0036   0.9088   0.8898
   0.000   0.0018   0.00465   0.00194  -0.0004   0.9022   0.9026
   0.250   0.0438   0.00473   0.00204  -0.0033   0.8905   0.9092
   0.500   0.0662   0.00473   0.00199  -0.0017   0.8734   0.9183
   0.750   0.1204   0.00486   0.00204  -0.0073   0.8436   0.9206
   1.000   0.1627   0.00520   0.00215  -0.0102   0.7844   0.9235
   1.250   0.1654   0.00565   0.00233  -0.0040   0.7116   0.9336
   1.500   0.1954   0.00661   0.00279  -0.0042   0.5832   0.9359
   1.750   0.2200   0.00755   0.00316  -0.0036   0.4370   0.9379
   2.000   0.2451   0.00817   0.00339  -0.0031   0.3370   0.9400
   2.250   0.2512   0.00843   0.00347   0.0018   0.2887   0.9477
   2.500   0.2839   0.00890   0.00369   0.0006   0.2265   0.9483
   2.750   0.3163   0.00932   0.00388  -0.0005   0.1767   0.9491
   3.000   0.3486   0.00967   0.00407  -0.0016   0.1410   0.9499
   3.250   0.3803   0.00999   0.00425  -0.0025   0.1137   0.9508
   3.500   0.4111   0.01029   0.00443  -0.0032   0.0923   0.9520
   3.750   0.4405   0.01057   0.00462  -0.0036   0.0770   0.9536
   4.000   0.4680   0.01081   0.00480  -0.0035   0.0664   0.9557
   4.250   0.4799   0.01098   0.00494   0.0001   0.0599   0.9613
   4.500   0.5122   0.01122   0.00513  -0.0010   0.0532   0.9619
   4.750   0.5438   0.01146   0.00534  -0.0019   0.0476   0.9626
   5.000   0.5745   0.01175   0.00558  -0.0026   0.0434   0.9634
   5.250   0.6056   0.01194   0.00577  -0.0033   0.0407   0.9644
   5.500   0.6344   0.01226   0.00606  -0.0036   0.0375   0.9655
   5.750   0.6631   0.01247   0.00627  -0.0039   0.0357   0.9670
   6.000   0.6886   0.01273   0.00651  -0.0035   0.0337   0.9691
   6.250   0.7009   0.01303   0.00682  -0.0001   0.0322   0.9737
   6.500   0.7322   0.01323   0.00703  -0.0010   0.0308   0.9743
   6.750   0.7623   0.01351   0.00730  -0.0016   0.0293   0.9749
   7.000   0.7903   0.01396   0.00775  -0.0019   0.0279   0.9758
   7.250   0.8198   0.01420   0.00802  -0.0024   0.0270   0.9767
   7.500   0.8477   0.01452   0.00836  -0.0025   0.0262   0.9780
   7.750   0.8739   0.01482   0.00868  -0.0024   0.0256   0.9795
   8.000   0.8965   0.01520   0.00906  -0.0015   0.0249   0.9815
   8.250   0.9116   0.01580   0.00968   0.0010   0.0242   0.9848
   8.500   0.9394   0.01627   0.01021   0.0007   0.0238   0.9855
   8.750   0.9678   0.01657   0.01055   0.0003   0.0233   0.9862
   9.000   0.9945   0.01699   0.01101   0.0002   0.0230   0.9871
   9.250   1.0213   0.01736   0.01142   0.0001   0.0225   0.9882
   9.500   1.0474   0.01777   0.01185   0.0002   0.0220   0.9896
   9.750   1.0711   0.01823   0.01235   0.0007   0.0217   0.9912
  10.000   1.0924   0.01872   0.01287   0.0016   0.0213   0.9929
  10.250   1.1126   0.01932   0.01351   0.0027   0.0210   0.9945
  10.500   1.1354   0.02022   0.01447   0.0031   0.0207   0.9955
  10.750   1.1570   0.02121   0.01556   0.0036   0.0203   0.9967
  11.000   1.1807   0.02175   0.01617   0.0039   0.0201   0.9980
  11.250   1.2025   0.02244   0.01694   0.0045   0.0200   0.9992
  11.500   1.2217   0.02302   0.01760   0.0057   0.0198   1.0000
  11.750   1.2223   0.02353   0.01819   0.0107   0.0196   1.0000
  12.000   1.2222   0.02413   0.01887   0.0157   0.0196   1.0000
  12.250   1.2227   0.02479   0.01961   0.0204   0.0195   1.0000
  12.500   1.2252   0.02532   0.02022   0.0247   0.0192   1.0000
  12.750   1.2258   0.02614   0.02113   0.0292   0.0192   1.0000
  13.000   1.2284   0.02680   0.02186   0.0332   0.0190   1.0000
  13.250   1.2281   0.02777   0.02293   0.0374   0.0189   1.0000
  13.500   1.2286   0.02871   0.02397   0.0413   0.0188   1.0000
  13.750   1.2304   0.02954   0.02487   0.0449   0.0186   1.0000
  14.000   1.2311   0.03052   0.02593   0.0484   0.0185   1.0000
  14.250   1.2284   0.03187   0.02738   0.0520   0.0185   1.0000
  14.500   1.2316   0.03271   0.02828   0.0548   0.0182   1.0000
  14.750   1.2228   0.03473   0.03045   0.0584   0.0183   1.0000
  15.000   1.2242   0.03590   0.03167   0.0607   0.0181   1.0000
  15.250   1.2225   0.03746   0.03330   0.0630   0.0180   1.0000
  15.500   1.2175   0.03945   0.03538   0.0651   0.0179   1.0000
  15.750   1.2095   0.04191   0.03795   0.0668   0.0178   1.0000
  16.000   1.1980   0.04499   0.04119   0.0679   0.0179   1.0000
  16.250   1.1882   0.04818   0.04446   0.0682   0.0177   1.0000
  16.500   1.1752   0.05214   0.04856   0.0677   0.0177   1.0000
  16.750   1.1595   0.05693   0.05350   0.0662   0.0177   1.0000
  17.000   1.1434   0.06227   0.05896   0.0637   0.0176   1.0000
  17.250   1.1208   0.06932   0.06618   0.0598   0.0176   1.0000
  17.500   1.0857   0.07929   0.07638   0.0536   0.0177   1.0000
  17.750   1.0520   0.08936   0.08661   0.0476   0.0176   1.0000
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