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NACA 1410 (naca1410-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NACA 1410 (naca1410-il)
Reynolds number: 500,000
Max Cl/Cd: 70.81 at α=4°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca1410-il-500000.txt
Download as CSV file: xf-naca1410-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 1410                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.7901   0.10688   0.10456  -0.0001   1.0000   0.0169
 -13.250  -1.0099   0.05267   0.04964  -0.0381   1.0000   0.0142
 -13.000  -1.0303   0.04578   0.04250  -0.0436   1.0000   0.0142
 -12.750  -1.0410   0.04173   0.03825  -0.0455   1.0000   0.0144
 -12.500  -1.0487   0.03877   0.03510  -0.0452   1.0000   0.0146
 -12.250  -1.0527   0.03656   0.03270  -0.0434   1.0000   0.0149
 -12.000  -1.0513   0.03445   0.03038  -0.0418   1.0000   0.0153
 -11.750  -1.0451   0.03245   0.02815  -0.0404   1.0000   0.0157
 -11.500  -1.0352   0.03067   0.02614  -0.0390   1.0000   0.0161
 -11.250  -1.0266   0.02847   0.02365  -0.0375   1.0000   0.0165
 -11.000  -1.0175   0.02617   0.02116  -0.0359   1.0000   0.0173
 -10.750  -0.9984   0.02542   0.02036  -0.0351   1.0000   0.0179
 -10.500  -0.9783   0.02475   0.01962  -0.0343   1.0000   0.0186
 -10.250  -0.9585   0.02397   0.01872  -0.0334   1.0000   0.0196
 -10.000  -0.9380   0.02325   0.01786  -0.0325   1.0000   0.0206
  -9.750  -0.9159   0.02285   0.01732  -0.0317   1.0000   0.0214
  -9.500  -0.9014   0.02090   0.01526  -0.0302   1.0000   0.0228
  -9.250  -0.8800   0.02043   0.01477  -0.0293   1.0000   0.0239
  -9.000  -0.8587   0.01990   0.01417  -0.0283   1.0000   0.0252
  -8.750  -0.8371   0.01943   0.01358  -0.0273   1.0000   0.0267
  -8.500  -0.8156   0.01895   0.01298  -0.0262   1.0000   0.0279
  -8.250  -0.7983   0.01758   0.01157  -0.0247   1.0000   0.0300
  -8.000  -0.7768   0.01715   0.01112  -0.0237   1.0000   0.0316
  -7.750  -0.7553   0.01670   0.01061  -0.0226   1.0000   0.0334
  -7.500  -0.7331   0.01644   0.01027  -0.0215   1.0000   0.0348
  -7.250  -0.7147   0.01527   0.00901  -0.0200   1.0000   0.0369
  -7.000  -0.6942   0.01469   0.00842  -0.0188   1.0000   0.0388
  -6.750  -0.6726   0.01431   0.00802  -0.0177   1.0000   0.0406
  -6.500  -0.6509   0.01395   0.00761  -0.0165   1.0000   0.0425
  -6.250  -0.6290   0.01363   0.00722  -0.0154   1.0000   0.0438
  -6.000  -0.6080   0.01305   0.00659  -0.0142   1.0000   0.0453
  -5.750  -0.5870   0.01242   0.00595  -0.0131   1.0000   0.0478
  -5.500  -0.5648   0.01208   0.00559  -0.0121   1.0000   0.0499
  -5.250  -0.5421   0.01179   0.00528  -0.0113   1.0000   0.0521
  -5.000  -0.5072   0.01147   0.00491  -0.0129   0.9980   0.0544
  -4.750  -0.4705   0.01098   0.00441  -0.0149   0.9956   0.0590
  -4.500  -0.4335   0.01065   0.00410  -0.0170   0.9931   0.0654
  -4.250  -0.3978   0.01020   0.00372  -0.0188   0.9897   0.0816
  -4.000  -0.3612   0.00970   0.00342  -0.0209   0.9868   0.1198
  -3.750  -0.3232   0.00930   0.00320  -0.0233   0.9847   0.1604
  -3.500  -0.2893   0.00895   0.00300  -0.0247   0.9799   0.1997
  -3.250  -0.2523   0.00859   0.00284  -0.0268   0.9766   0.2466
  -3.000  -0.2139   0.00826   0.00267  -0.0293   0.9742   0.2922
  -2.750  -0.1816   0.00793   0.00249  -0.0303   0.9682   0.3331
  -2.500  -0.1487   0.00739   0.00235  -0.0315   0.9630   0.4281
  -2.250  -0.1188   0.00711   0.00226  -0.0319   0.9554   0.4956
  -2.000  -0.0879   0.00687   0.00214  -0.0324   0.9480   0.5351
  -1.750  -0.0609   0.00664   0.00204  -0.0320   0.9372   0.5724
  -1.500  -0.0341   0.00638   0.00196  -0.0315   0.9265   0.6201
  -1.250  -0.0078   0.00616   0.00189  -0.0308   0.9147   0.6674
  -1.000   0.0176   0.00597   0.00183  -0.0299   0.9011   0.7144
  -0.750   0.0419   0.00577   0.00180  -0.0287   0.8856   0.7688
  -0.500   0.0662   0.00564   0.00179  -0.0274   0.8683   0.8175
  -0.250   0.0907   0.00556   0.00179  -0.0262   0.8500   0.8583
   0.000   0.1156   0.00555   0.00181  -0.0249   0.8311   0.8953
   0.250   0.1420   0.00560   0.00183  -0.0241   0.8116   0.9249
   0.500   0.1710   0.00568   0.00186  -0.0238   0.7905   0.9475
   0.750   0.2042   0.00580   0.00189  -0.0246   0.7676   0.9641
   1.000   0.2395   0.00593   0.00192  -0.0259   0.7419   0.9761
   1.250   0.2771   0.00608   0.00195  -0.0279   0.7134   0.9847
   1.500   0.3177   0.00623   0.00198  -0.0305   0.6847   0.9901
   1.750   0.3560   0.00639   0.00201  -0.0328   0.6547   0.9955
   2.000   0.3945   0.00659   0.00203  -0.0351   0.6126   1.0000
   2.250   0.4188   0.00676   0.00205  -0.0344   0.5771   1.0000
   2.500   0.4433   0.00692   0.00209  -0.0338   0.5464   1.0000
   2.750   0.4675   0.00710   0.00214  -0.0331   0.5138   1.0000
   3.000   0.4916   0.00729   0.00222  -0.0324   0.4831   1.0000
   3.250   0.5157   0.00750   0.00231  -0.0316   0.4510   1.0000
   3.500   0.5395   0.00775   0.00241  -0.0309   0.4161   1.0000
   3.750   0.5633   0.00801   0.00254  -0.0301   0.3822   1.0000
   4.000   0.5870   0.00829   0.00269  -0.0293   0.3450   1.0000
   4.250   0.6102   0.00865   0.00287  -0.0285   0.3021   1.0000
   4.500   0.6329   0.00907   0.00309  -0.0277   0.2558   1.0000
   4.750   0.6556   0.00953   0.00334  -0.0268   0.2101   1.0000
   5.000   0.6781   0.01002   0.00363  -0.0259   0.1662   1.0000
   5.250   0.7005   0.01058   0.00397  -0.0251   0.1229   1.0000
   5.500   0.7224   0.01124   0.00440  -0.0241   0.0822   1.0000
   5.750   0.7451   0.01183   0.00486  -0.0232   0.0632   1.0000
   6.000   0.7694   0.01223   0.00528  -0.0226   0.0574   1.0000
   6.250   0.7932   0.01268   0.00571  -0.0219   0.0530   1.0000
   6.500   0.8160   0.01329   0.00635  -0.0210   0.0498   1.0000
   6.750   0.8405   0.01367   0.00679  -0.0204   0.0482   1.0000
   7.000   0.8646   0.01409   0.00725  -0.0197   0.0462   1.0000
   7.250   0.8883   0.01456   0.00776  -0.0191   0.0442   1.0000
   7.500   0.9107   0.01520   0.00840  -0.0182   0.0420   1.0000
   7.750   0.9300   0.01625   0.00952  -0.0170   0.0399   1.0000
   8.000   0.9543   0.01662   0.00995  -0.0164   0.0388   1.0000
   8.250   0.9778   0.01710   0.01049  -0.0158   0.0371   1.0000
   8.500   1.0008   0.01763   0.01108  -0.0151   0.0354   1.0000
   8.750   1.0228   0.01824   0.01171  -0.0143   0.0336   1.0000
   9.000   1.0387   0.01984   0.01337  -0.0128   0.0313   1.0000
   9.250   1.0624   0.02017   0.01379  -0.0122   0.0303   1.0000
   9.500   1.0846   0.02071   0.01441  -0.0114   0.0287   1.0000
   9.750   1.1064   0.02122   0.01497  -0.0107   0.0270   1.0000
  10.000   1.1258   0.02202   0.01578  -0.0097   0.0255   1.0000
  10.250   1.1414   0.02350   0.01738  -0.0083   0.0240   1.0000
  10.500   1.1621   0.02404   0.01803  -0.0074   0.0228   1.0000
  10.750   1.1812   0.02473   0.01882  -0.0063   0.0216   1.0000
  11.000   1.2001   0.02532   0.01946  -0.0053   0.0205   1.0000
  11.250   1.2169   0.02607   0.02024  -0.0041   0.0196   1.0000
  11.500   1.2253   0.02797   0.02227  -0.0020   0.0185   1.0000
  11.750   1.2404   0.02867   0.02310  -0.0005   0.0179   1.0000
  12.000   1.2512   0.02963   0.02420   0.0015   0.0171   1.0000
  12.250   1.2605   0.03073   0.02541   0.0035   0.0165   1.0000
  12.500   1.2694   0.03182   0.02659   0.0052   0.0159   1.0000
  12.750   1.2777   0.03297   0.02781   0.0068   0.0155   1.0000
  13.000   1.2838   0.03439   0.02932   0.0082   0.0150   1.0000
  13.250   1.2835   0.03660   0.03163   0.0097   0.0146   1.0000
  13.500   1.2713   0.04039   0.03564   0.0112   0.0142   1.0000
  13.750   1.2688   0.04320   0.03865   0.0116   0.0140   1.0000
  14.000   1.2663   0.04623   0.04187   0.0114   0.0138   1.0000
  14.250   1.2610   0.04981   0.04564   0.0107   0.0136   1.0000
  14.500   1.2533   0.05400   0.05001   0.0093   0.0134   1.0000
  14.750   1.2432   0.05879   0.05500   0.0072   0.0133   1.0000
  15.000   1.2307   0.06428   0.06066   0.0045   0.0131   1.0000
  15.250   1.2147   0.07059   0.06716   0.0011   0.0130   1.0000
  15.500   1.1940   0.07804   0.07479  -0.0031   0.0130   1.0000
  15.750   1.1693   0.08658   0.08352  -0.0081   0.0130   1.0000
  16.000   1.1366   0.09723   0.09438  -0.0143   0.0132   1.0000
  16.250   1.0979   0.10978   0.10712  -0.0217   0.0135   1.0000
  16.500   1.0416   0.12731   0.12485  -0.0318   0.0139   1.0000
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