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SD7032-099-88 (sd7032-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: SD7032-099-88 (sd7032-il)
Reynolds number: 1,000,000
Max Cl/Cd: 114.52 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sd7032-il-1000000-n5.txt
Download as CSV file: xf-sd7032-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD7032-099-88                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.3518   0.10675   0.10506  -0.0320   1.0000   0.0039
 -10.250  -0.3495   0.10317   0.10149  -0.0331   1.0000   0.0038
  -9.750  -0.5731   0.02597   0.02334  -0.0957   0.9456   0.0040
  -9.500  -0.5618   0.02260   0.01956  -0.0959   0.9366   0.0040
  -9.250  -0.5442   0.02053   0.01718  -0.0957   0.9294   0.0041
  -9.000  -0.5235   0.01891   0.01531  -0.0956   0.9231   0.0042
  -8.750  -0.5011   0.01766   0.01384  -0.0953   0.9169   0.0043
  -8.500  -0.4778   0.01655   0.01253  -0.0951   0.9114   0.0043
  -8.250  -0.4533   0.01561   0.01142  -0.0950   0.9053   0.0043
  -8.000  -0.4293   0.01454   0.01014  -0.0947   0.8995   0.0044
  -7.750  -0.4045   0.01345   0.00886  -0.0946   0.8936   0.0046
  -7.500  -0.3788   0.01272   0.00798  -0.0945   0.8873   0.0048
  -7.250  -0.3524   0.01220   0.00736  -0.0943   0.8815   0.0050
  -7.000  -0.3255   0.01179   0.00687  -0.0942   0.8749   0.0053
  -6.750  -0.2986   0.01141   0.00641  -0.0941   0.8687   0.0055
  -6.500  -0.2714   0.01101   0.00593  -0.0940   0.8615   0.0059
  -6.250  -0.2443   0.01063   0.00545  -0.0939   0.8545   0.0062
  -6.000  -0.2168   0.01026   0.00499  -0.0938   0.8468   0.0065
  -5.750  -0.1894   0.00994   0.00458  -0.0937   0.8390   0.0067
  -5.500  -0.1620   0.00949   0.00406  -0.0936   0.8303   0.0073
  -5.250  -0.1344   0.00923   0.00374  -0.0936   0.8216   0.0078
  -5.000  -0.1067   0.00902   0.00346  -0.0935   0.8120   0.0085
  -4.750  -0.0788   0.00880   0.00318  -0.0934   0.8017   0.0092
  -4.500  -0.0510   0.00859   0.00290  -0.0934   0.7909   0.0101
  -4.250  -0.0232   0.00844   0.00272  -0.0933   0.7796   0.0115
  -4.000   0.0047   0.00835   0.00255  -0.0932   0.7674   0.0129
  -3.750   0.0326   0.00819   0.00234  -0.0932   0.7544   0.0143
  -3.500   0.0605   0.00807   0.00217  -0.0931   0.7410   0.0158
  -3.250   0.0884   0.00798   0.00201  -0.0930   0.7271   0.0172
  -3.000   0.1163   0.00792   0.00188  -0.0930   0.7128   0.0181
  -2.750   0.1442   0.00779   0.00168  -0.0929   0.6980   0.0206
  -2.500   0.1721   0.00773   0.00155  -0.0928   0.6828   0.0228
  -2.250   0.2000   0.00769   0.00143  -0.0928   0.6674   0.0247
  -2.000   0.2278   0.00762   0.00132  -0.0927   0.6517   0.0303
  -1.500   0.2834   0.00743   0.00116  -0.0927   0.6204   0.0774
  -1.250   0.3112   0.00733   0.00111  -0.0927   0.6049   0.1118
  -1.000   0.3390   0.00725   0.00107  -0.0927   0.5896   0.1517
  -0.750   0.3668   0.00713   0.00105  -0.0928   0.5744   0.2074
  -0.500   0.3944   0.00700   0.00104  -0.0929   0.5592   0.2725
  -0.250   0.4222   0.00693   0.00104  -0.0929   0.5441   0.3231
   0.000   0.4498   0.00683   0.00106  -0.0930   0.5293   0.3905
   0.250   0.4771   0.00659   0.00112  -0.0931   0.5142   0.5175
   0.500   0.5046   0.00655   0.00117  -0.0930   0.4995   0.5785
   0.750   0.5321   0.00655   0.00122  -0.0930   0.4840   0.6244
   1.000   0.5593   0.00656   0.00129  -0.0929   0.4676   0.6731
   1.250   0.5863   0.00660   0.00137  -0.0927   0.4503   0.7196
   1.500   0.6130   0.00665   0.00145  -0.0924   0.4339   0.7600
   1.750   0.6397   0.00670   0.00154  -0.0921   0.4187   0.7970
   2.000   0.6658   0.00676   0.00163  -0.0917   0.4041   0.8337
   2.250   0.6909   0.00680   0.00171  -0.0911   0.3900   0.8747
   2.500   0.7132   0.00678   0.00179  -0.0897   0.3769   0.9387
   2.750   0.7451   0.00689   0.00185  -0.0906   0.3622   1.0000
   3.000   0.7725   0.00705   0.00195  -0.0905   0.3501   1.0000
   3.250   0.7997   0.00722   0.00206  -0.0904   0.3376   1.0000
   3.500   0.8268   0.00741   0.00218  -0.0903   0.3240   1.0000
   3.750   0.8538   0.00759   0.00230  -0.0903   0.3125   1.0000
   4.000   0.8808   0.00778   0.00243  -0.0901   0.3003   1.0000
   4.250   0.9076   0.00797   0.00258  -0.0900   0.2873   1.0000
   4.500   0.9344   0.00817   0.00272  -0.0899   0.2756   1.0000
   4.750   0.9608   0.00839   0.00289  -0.0897   0.2619   1.0000
   5.000   0.9871   0.00862   0.00307  -0.0895   0.2486   1.0000
   5.250   1.0134   0.00886   0.00325  -0.0893   0.2362   1.0000
   5.500   1.0393   0.00912   0.00345  -0.0891   0.2227   1.0000
   5.750   1.0650   0.00939   0.00366  -0.0888   0.2087   1.0000
   6.000   1.0903   0.00970   0.00390  -0.0885   0.1929   1.0000
   6.250   1.1152   0.01004   0.00416  -0.0881   0.1759   1.0000
   6.500   1.1406   0.01031   0.00440  -0.0878   0.1662   1.0000
   6.750   1.1658   0.01061   0.00466  -0.0875   0.1564   1.0000
   7.000   1.1904   0.01095   0.00495  -0.0870   0.1443   1.0000
   7.250   1.2150   0.01127   0.00524  -0.0866   0.1338   1.0000
   7.500   1.2394   0.01161   0.00555  -0.0862   0.1231   1.0000
   7.750   1.2631   0.01199   0.00588  -0.0857   0.1113   1.0000
   8.000   1.2865   0.01240   0.00625  -0.0851   0.0997   1.0000
   8.250   1.3091   0.01286   0.00665  -0.0844   0.0871   1.0000
   8.500   1.3312   0.01334   0.00707  -0.0837   0.0753   1.0000
   8.750   1.3526   0.01387   0.00754  -0.0828   0.0633   1.0000
   9.000   1.3737   0.01440   0.00802  -0.0819   0.0532   1.0000
   9.250   1.3945   0.01493   0.00852  -0.0810   0.0455   1.0000
   9.500   1.4153   0.01543   0.00901  -0.0801   0.0399   1.0000
   9.750   1.4358   0.01592   0.00950  -0.0791   0.0350   1.0000
  10.000   1.4545   0.01653   0.01008  -0.0779   0.0290   1.0000
  10.250   1.4739   0.01703   0.01060  -0.0768   0.0255   1.0000
  10.500   1.4916   0.01763   0.01120  -0.0754   0.0218   1.0000
  10.750   1.5091   0.01816   0.01176  -0.0740   0.0194   1.0000
  11.000   1.5226   0.01879   0.01239  -0.0719   0.0165   1.0000
  11.250   1.5360   0.01939   0.01302  -0.0698   0.0145   1.0000
  11.500   1.5477   0.02009   0.01375  -0.0676   0.0125   1.0000
  11.750   1.5596   0.02081   0.01450  -0.0655   0.0106   1.0000
  12.000   1.5695   0.02167   0.01539  -0.0632   0.0088   1.0000
  12.250   1.5796   0.02255   0.01632  -0.0612   0.0072   1.0000
  12.500   1.5878   0.02359   0.01740  -0.0590   0.0056   1.0000
  12.750   1.5946   0.02477   0.01862  -0.0568   0.0041   1.0000
  13.000   1.6012   0.02602   0.01993  -0.0548   0.0031   1.0000
  13.250   1.6079   0.02731   0.02129  -0.0530   0.0027   1.0000
  13.500   1.6142   0.02870   0.02275  -0.0513   0.0024   1.0000
  13.750   1.6195   0.03022   0.02435  -0.0497   0.0021   1.0000
  14.000   1.6231   0.03198   0.02620  -0.0482   0.0019   1.0000
  14.250   1.6266   0.03382   0.02813  -0.0469   0.0018   1.0000
  14.500   1.6298   0.03578   0.03019  -0.0458   0.0017   1.0000
  14.750   1.6325   0.03791   0.03241  -0.0449   0.0017   1.0000
  15.000   1.6336   0.04029   0.03490  -0.0442   0.0015   1.0000
  15.250   1.6340   0.04286   0.03757  -0.0437   0.0015   1.0000
  15.500   1.6328   0.04575   0.04057  -0.0435   0.0014   1.0000
  15.750   1.6308   0.04888   0.04381  -0.0435   0.0014   1.0000
  16.000   1.6265   0.05245   0.04750  -0.0439   0.0014   1.0000
  16.250   1.6222   0.05623   0.05139  -0.0445   0.0013   1.0000
  16.500   1.6165   0.06035   0.05563  -0.0455   0.0013   1.0000
  16.750   1.6086   0.06498   0.06038  -0.0468   0.0013   1.0000
  17.000   1.6000   0.06992   0.06545  -0.0485   0.0012   1.0000
  17.250   1.5889   0.07543   0.07109  -0.0505   0.0012   1.0000
  17.500   1.5768   0.08130   0.07710  -0.0529   0.0012   1.0000
  17.750   1.5636   0.08758   0.08350  -0.0556   0.0012   1.0000
  18.000   1.5487   0.09430   0.09037  -0.0586   0.0011   1.0000
  18.250   1.5330   0.10137   0.09757  -0.0620   0.0011   1.0000
  18.500   1.5172   0.10865   0.10498  -0.0656   0.0011   1.0000
  18.750   1.5004   0.11624   0.11271  -0.0695   0.0011   1.0000
  19.000   1.4832   0.12407   0.12067  -0.0737   0.0011   1.0000
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