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SD5060 (9.5%) (sd5060-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: SD5060 (9.5%) (sd5060-il)
Reynolds number: 1,000,000
Max Cl/Cd: 100.89 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sd5060-il-1000000.txt
Download as CSV file: xf-sd5060-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD5060 (9.5%)                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.7993   0.05714   0.05517  -0.0343   1.0000   0.0081
 -11.500  -0.8290   0.04539   0.04324  -0.0453   1.0000   0.0080
 -11.250  -0.8591   0.03791   0.03555  -0.0527   1.0000   0.0079
 -11.000  -0.8625   0.03440   0.03181  -0.0539   1.0000   0.0080
 -10.750  -0.8581   0.03142   0.02858  -0.0543   1.0000   0.0081
 -10.500  -0.8435   0.02973   0.02670  -0.0544   1.0000   0.0083
 -10.250  -0.8432   0.02497   0.02146  -0.0544   1.0000   0.0086
 -10.000  -0.8255   0.02325   0.01961  -0.0542   1.0000   0.0089
  -9.750  -0.8029   0.02248   0.01879  -0.0541   1.0000   0.0092
  -9.500  -0.7797   0.02173   0.01796  -0.0540   1.0000   0.0095
  -9.250  -0.7564   0.02096   0.01711  -0.0538   1.0000   0.0098
  -9.000  -0.7332   0.02008   0.01612  -0.0536   1.0000   0.0102
  -8.750  -0.7108   0.01896   0.01486  -0.0533   1.0000   0.0105
  -8.500  -0.6881   0.01811   0.01389  -0.0528   1.0000   0.0109
  -8.250  -0.6562   0.01729   0.01293  -0.0541   0.9935   0.0112
  -8.000  -0.6247   0.01585   0.01129  -0.0555   0.9852   0.0116
  -7.750  -0.5954   0.01429   0.00962  -0.0566   0.9754   0.0123
  -7.500  -0.5669   0.01370   0.00897  -0.0570   0.9644   0.0128
  -7.250  -0.5420   0.01321   0.00841  -0.0565   0.9521   0.0133
  -7.000  -0.5180   0.01282   0.00794  -0.0556   0.9405   0.0139
  -6.750  -0.4935   0.01240   0.00743  -0.0549   0.9294   0.0145
  -6.500  -0.4681   0.01200   0.00695  -0.0543   0.9193   0.0149
  -6.250  -0.4424   0.01168   0.00654  -0.0537   0.9099   0.0152
  -6.000  -0.4183   0.01062   0.00533  -0.0531   0.9001   0.0161
  -5.750  -0.3921   0.01012   0.00476  -0.0528   0.8910   0.0170
  -5.500  -0.3656   0.00980   0.00436  -0.0524   0.8824   0.0179
  -5.250  -0.3383   0.00948   0.00399  -0.0522   0.8733   0.0188
  -5.000  -0.3111   0.00920   0.00363  -0.0519   0.8649   0.0195
  -4.750  -0.2836   0.00895   0.00332  -0.0517   0.8561   0.0201
  -4.500  -0.2561   0.00858   0.00286  -0.0515   0.8476   0.0220
  -4.250  -0.2286   0.00833   0.00256  -0.0513   0.8391   0.0243
  -4.000  -0.2006   0.00808   0.00229  -0.0511   0.8302   0.0300
  -3.750  -0.1735   0.00764   0.00200  -0.0510   0.8218   0.0659
  -3.500  -0.1458   0.00735   0.00182  -0.0509   0.8127   0.0967
  -3.250  -0.1178   0.00716   0.00168  -0.0509   0.8041   0.1205
  -3.000  -0.0900   0.00699   0.00156  -0.0508   0.7951   0.1429
  -2.750  -0.0617   0.00686   0.00146  -0.0508   0.7857   0.1633
  -2.500  -0.0337   0.00671   0.00136  -0.0507   0.7766   0.1888
  -2.000   0.0227   0.00649   0.00120  -0.0506   0.7567   0.2302
  -1.750   0.0508   0.00637   0.00113  -0.0506   0.7467   0.2595
  -1.500   0.0789   0.00624   0.00107  -0.0505   0.7358   0.2949
  -1.250   0.1070   0.00610   0.00102  -0.0505   0.7245   0.3315
  -1.000   0.1350   0.00596   0.00098  -0.0505   0.7128   0.3769
  -0.750   0.1631   0.00585   0.00095  -0.0504   0.7004   0.4185
  -0.500   0.1910   0.00574   0.00093  -0.0504   0.6875   0.4657
  -0.250   0.2190   0.00563   0.00092  -0.0503   0.6743   0.5139
   0.000   0.2468   0.00552   0.00092  -0.0502   0.6609   0.5701
   0.250   0.2745   0.00541   0.00093  -0.0501   0.6470   0.6270
   0.500   0.3019   0.00528   0.00095  -0.0499   0.6325   0.6902
   0.750   0.3287   0.00517   0.00098  -0.0495   0.6171   0.7554
   1.000   0.3546   0.00505   0.00103  -0.0489   0.6006   0.8249
   1.250   0.3783   0.00494   0.00107  -0.0476   0.5839   0.8970
   1.500   0.4083   0.00490   0.00109  -0.0477   0.5649   0.9701
   1.750   0.4448   0.00501   0.00111  -0.0495   0.5439   1.0000
   2.000   0.4724   0.00514   0.00115  -0.0494   0.5226   1.0000
   2.250   0.4999   0.00529   0.00120  -0.0493   0.5003   1.0000
   2.500   0.5276   0.00545   0.00127  -0.0492   0.4784   1.0000
   2.750   0.5549   0.00564   0.00135  -0.0490   0.4521   1.0000
   3.000   0.5822   0.00585   0.00145  -0.0489   0.4249   1.0000
   3.250   0.6095   0.00606   0.00155  -0.0488   0.3983   1.0000
   3.500   0.6366   0.00631   0.00168  -0.0487   0.3686   1.0000
   3.750   0.6635   0.00659   0.00182  -0.0485   0.3369   1.0000
   4.250   0.7172   0.00714   0.00213  -0.0482   0.2818   1.0000
   4.500   0.7439   0.00744   0.00232  -0.0481   0.2546   1.0000
   4.750   0.7707   0.00773   0.00250  -0.0479   0.2318   1.0000
   5.000   0.7973   0.00802   0.00269  -0.0478   0.2109   1.0000
   5.250   0.8239   0.00832   0.00291  -0.0476   0.1917   1.0000
   5.500   0.8506   0.00858   0.00311  -0.0474   0.1763   1.0000
   5.750   0.8772   0.00886   0.00333  -0.0472   0.1613   1.0000
   6.000   0.9036   0.00915   0.00356  -0.0470   0.1479   1.0000
   6.250   0.9299   0.00945   0.00381  -0.0468   0.1356   1.0000
   6.500   0.9563   0.00973   0.00405  -0.0466   0.1253   1.0000
   6.750   0.9827   0.00999   0.00430  -0.0464   0.1170   1.0000
   7.000   1.0087   0.01030   0.00458  -0.0462   0.1081   1.0000
   7.250   1.0349   0.01058   0.00484  -0.0460   0.1010   1.0000
   7.500   1.0608   0.01088   0.00514  -0.0457   0.0937   1.0000
   7.750   1.0862   0.01123   0.00544  -0.0454   0.0848   1.0000
   8.000   1.1119   0.01153   0.00574  -0.0451   0.0775   1.0000
   8.250   1.1369   0.01191   0.00608  -0.0448   0.0691   1.0000
   8.500   1.1616   0.01232   0.00645  -0.0444   0.0609   1.0000
   8.750   1.1864   0.01269   0.00681  -0.0440   0.0542   1.0000
   9.000   1.2104   0.01315   0.00723  -0.0436   0.0468   1.0000
   9.250   1.2339   0.01365   0.00770  -0.0431   0.0402   1.0000
   9.500   1.2577   0.01409   0.00815  -0.0426   0.0353   1.0000
   9.750   1.2803   0.01465   0.00868  -0.0420   0.0298   1.0000
  10.000   1.3033   0.01514   0.00918  -0.0414   0.0260   1.0000
  10.250   1.3253   0.01571   0.00976  -0.0407   0.0219   1.0000
  10.500   1.3461   0.01639   0.01042  -0.0399   0.0174   1.0000
  10.750   1.3664   0.01709   0.01112  -0.0390   0.0137   1.0000
  11.000   1.3855   0.01788   0.01192  -0.0380   0.0106   1.0000
  11.250   1.4042   0.01864   0.01274  -0.0369   0.0088   1.0000
  11.500   1.4220   0.01945   0.01358  -0.0357   0.0077   1.0000
  11.750   1.4375   0.02040   0.01461  -0.0342   0.0068   1.0000
  12.000   1.4543   0.02114   0.01543  -0.0329   0.0064   1.0000
  12.250   1.4692   0.02197   0.01632  -0.0314   0.0061   1.0000
  12.500   1.4804   0.02283   0.01728  -0.0293   0.0059   1.0000
  12.750   1.4863   0.02386   0.01837  -0.0266   0.0055   1.0000
  13.000   1.4916   0.02497   0.01958  -0.0241   0.0054   1.0000
  13.250   1.4898   0.02667   0.02140  -0.0213   0.0051   1.0000
  13.500   1.4867   0.02864   0.02351  -0.0190   0.0049   1.0000
  13.750   1.4924   0.03009   0.02504  -0.0176   0.0049   1.0000
  14.000   1.4954   0.03185   0.02691  -0.0163   0.0048   1.0000
  14.250   1.4956   0.03400   0.02918  -0.0152   0.0047   1.0000
  14.500   1.4940   0.03648   0.03177  -0.0145   0.0047   1.0000
  14.750   1.4929   0.03908   0.03449  -0.0142   0.0046   1.0000
  15.000   1.4898   0.04209   0.03762  -0.0142   0.0045   1.0000
  15.250   1.4858   0.04541   0.04106  -0.0146   0.0045   1.0000
  15.500   1.4794   0.04924   0.04502  -0.0155   0.0044   1.0000
  15.750   1.4671   0.05414   0.05006  -0.0171   0.0044   1.0000
  16.000   1.4579   0.05891   0.05497  -0.0190   0.0044   1.0000
  16.250   1.4409   0.06520   0.06141  -0.0218   0.0044   1.0000
  16.500   1.4280   0.07123   0.06757  -0.0248   0.0043   1.0000
  16.750   1.4077   0.07889   0.07539  -0.0289   0.0043   1.0000
  17.000   1.3874   0.08694   0.08359  -0.0332   0.0043   1.0000
  17.250   1.3652   0.09565   0.09245  -0.0380   0.0044   1.0000
  17.500   1.3394   0.10538   0.10233  -0.0435   0.0044   1.0000
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