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WORTMANN FX 76-100 (fx76100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 76-100 (fx76100-il)
Reynolds number: 1,000,000
Max Cl/Cd: 75.42 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx76100-il-1000000-n5.txt
Download as CSV file: xf-fx76100-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 76-100                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.1587   0.10185   0.09907  -0.0017   1.0000   0.0066
 -17.500  -1.2067   0.08949   0.08655  -0.0084   1.0000   0.0066
 -17.250  -1.2563   0.07703   0.07391  -0.0153   1.0000   0.0064
 -17.000  -1.2908   0.06715   0.06386  -0.0210   1.0000   0.0064
 -16.750  -1.3230   0.05762   0.05414  -0.0269   1.0000   0.0064
 -16.500  -1.3492   0.04945   0.04578  -0.0323   1.0000   0.0063
 -16.250  -1.3533   0.04529   0.04149  -0.0347   1.0000   0.0065
 -16.000  -1.3617   0.04088   0.03693  -0.0369   1.0000   0.0065
 -15.750  -1.3641   0.03769   0.03361  -0.0380   1.0000   0.0066
 -15.500  -1.3669   0.03481   0.03061  -0.0385   1.0000   0.0066
 -15.250  -1.3684   0.03236   0.02804  -0.0381   1.0000   0.0066
 -15.000  -1.3664   0.03048   0.02605  -0.0372   1.0000   0.0067
 -14.750  -1.3667   0.02859   0.02404  -0.0357   1.0000   0.0069
 -14.500  -1.3620   0.02722   0.02257  -0.0340   1.0000   0.0069
 -14.250  -1.3581   0.02589   0.02114  -0.0319   1.0000   0.0072
 -14.000  -1.3501   0.02490   0.02006  -0.0297   1.0000   0.0072
 -13.750  -1.3432   0.02390   0.01899  -0.0272   1.0000   0.0074
 -13.500  -1.3334   0.02307   0.01810  -0.0248   1.0000   0.0076
 -13.250  -1.3195   0.02231   0.01726  -0.0231   1.0000   0.0078
 -13.000  -1.3047   0.02156   0.01645  -0.0215   1.0000   0.0081
 -12.750  -1.2889   0.02086   0.01567  -0.0199   1.0000   0.0083
 -12.500  -1.2720   0.02021   0.01495  -0.0184   1.0000   0.0085
 -12.250  -1.2546   0.01957   0.01424  -0.0170   1.0000   0.0088
 -12.000  -1.2365   0.01896   0.01357  -0.0157   1.0000   0.0089
 -11.750  -1.2176   0.01841   0.01296  -0.0144   1.0000   0.0093
 -11.500  -1.1996   0.01777   0.01225  -0.0130   1.0000   0.0097
 -11.250  -1.1805   0.01720   0.01165  -0.0117   1.0000   0.0101
 -11.000  -1.1607   0.01671   0.01112  -0.0104   1.0000   0.0106
 -10.750  -1.1407   0.01621   0.01058  -0.0092   1.0000   0.0111
 -10.500  -1.1201   0.01577   0.01009  -0.0080   1.0000   0.0116
 -10.250  -1.0993   0.01537   0.00964  -0.0068   1.0000   0.0120
 -10.000  -1.0789   0.01492   0.00914  -0.0055   1.0000   0.0125
  -9.750  -1.0586   0.01447   0.00867  -0.0042   1.0000   0.0132
  -9.500  -1.0379   0.01408   0.00826  -0.0030   1.0000   0.0140
  -9.250  -1.0171   0.01372   0.00787  -0.0017   1.0000   0.0148
  -9.000  -0.9961   0.01340   0.00751  -0.0004   1.0000   0.0154
  -8.750  -0.9753   0.01306   0.00714   0.0009   1.0000   0.0160
  -8.500  -0.9550   0.01270   0.00678   0.0023   1.0000   0.0173
  -8.250  -0.9344   0.01239   0.00646   0.0037   1.0000   0.0185
  -8.000  -0.9138   0.01211   0.00615   0.0051   1.0000   0.0195
  -7.750  -0.8872   0.01182   0.00583   0.0052   0.9994   0.0205
  -7.500  -0.8565   0.01147   0.00549   0.0045   0.9979   0.0223
  -7.250  -0.8262   0.01117   0.00518   0.0038   0.9956   0.0241
  -7.000  -0.7960   0.01091   0.00490   0.0032   0.9934   0.0254
  -6.750  -0.7648   0.01059   0.00459   0.0023   0.9911   0.0282
  -6.500  -0.7322   0.01030   0.00431   0.0012   0.9890   0.0310
  -6.250  -0.7020   0.01004   0.00405   0.0006   0.9857   0.0339
  -6.000  -0.6709   0.00975   0.00379  -0.0002   0.9832   0.0382
  -5.750  -0.6391   0.00949   0.00354  -0.0011   0.9814   0.0435
  -5.500  -0.6099   0.00924   0.00332  -0.0014   0.9777   0.0491
  -5.250  -0.5797   0.00897   0.00310  -0.0020   0.9738   0.0571
  -5.000  -0.5470   0.00869   0.00287  -0.0031   0.9710   0.0682
  -4.750  -0.5149   0.00842   0.00266  -0.0041   0.9652   0.0819
  -4.250  -0.4432   0.00782   0.00224  -0.0078   0.9522   0.1229
  -4.000  -0.4085   0.00759   0.00207  -0.0093   0.9457   0.1420
  -3.750  -0.3762   0.00736   0.00192  -0.0103   0.9351   0.1614
  -3.500  -0.3437   0.00719   0.00178  -0.0113   0.9202   0.1780
  -3.250  -0.3141   0.00704   0.00165  -0.0116   0.9023   0.1973
  -3.000  -0.2865   0.00693   0.00154  -0.0114   0.8823   0.2139
  -2.750  -0.2607   0.00683   0.00143  -0.0109   0.8609   0.2311
  -2.500  -0.2362   0.00673   0.00134  -0.0100   0.8339   0.2521
  -2.250  -0.2125   0.00667   0.00125  -0.0090   0.8041   0.2729
  -2.000  -0.1894   0.00663   0.00117  -0.0078   0.7702   0.2957
  -1.750  -0.1662   0.00660   0.00110  -0.0067   0.7370   0.3190
  -1.500  -0.1429   0.00658   0.00105  -0.0056   0.7027   0.3415
  -1.250  -0.1193   0.00658   0.00101  -0.0046   0.6682   0.3631
  -1.000  -0.0957   0.00655   0.00097  -0.0036   0.6367   0.3914
  -0.750  -0.0719   0.00658   0.00094  -0.0027   0.6011   0.4152
  -0.500  -0.0477   0.00657   0.00092  -0.0018   0.5695   0.4403
  -0.250  -0.0240   0.00657   0.00091  -0.0009   0.5341   0.4711
   0.000  -0.0001   0.00656   0.00090   0.0000   0.5013   0.5034
   0.250   0.0239   0.00655   0.00091   0.0009   0.4733   0.5386
   0.500   0.0478   0.00656   0.00092   0.0018   0.4438   0.5713
   0.750   0.0718   0.00657   0.00094   0.0027   0.4156   0.6023
   1.000   0.0957   0.00658   0.00097   0.0036   0.3881   0.6347
   1.250   0.1194   0.00658   0.00101   0.0046   0.3635   0.6674
   1.500   0.1430   0.00658   0.00105   0.0056   0.3419   0.7015
   1.750   0.1658   0.00660   0.00111   0.0068   0.3164   0.7392
   2.000   0.1891   0.00663   0.00117   0.0079   0.2941   0.7721
   2.250   0.2126   0.00666   0.00125   0.0090   0.2764   0.8039
   2.500   0.2362   0.00674   0.00134   0.0100   0.2518   0.8332
   2.750   0.2606   0.00683   0.00143   0.0109   0.2297   0.8604
   3.250   0.3140   0.00704   0.00165   0.0116   0.1971   0.9019
   3.500   0.3436   0.00720   0.00178   0.0113   0.1773   0.9201
   3.750   0.3763   0.00736   0.00192   0.0103   0.1613   0.9352
   4.000   0.4083   0.00759   0.00207   0.0093   0.1414   0.9456
   4.250   0.4432   0.00781   0.00223   0.0078   0.1238   0.9522
   4.500   0.4771   0.00812   0.00244   0.0064   0.1001   0.9599
   4.750   0.5150   0.00841   0.00266   0.0041   0.0824   0.9653
   5.000   0.5470   0.00871   0.00288   0.0031   0.0667   0.9710
   5.250   0.5798   0.00898   0.00310   0.0019   0.0563   0.9739
   5.500   0.6100   0.00924   0.00332   0.0014   0.0487   0.9777
   5.750   0.6391   0.00951   0.00355   0.0011   0.0425   0.9815
   6.000   0.6710   0.00976   0.00380   0.0001   0.0380   0.9833
   6.250   0.7021   0.01004   0.00405  -0.0006   0.0338   0.9857
   6.500   0.7324   0.01030   0.00432  -0.0012   0.0312   0.9890
   6.750   0.7649   0.01059   0.00459  -0.0023   0.0283   0.9911
   7.000   0.7961   0.01091   0.00490  -0.0032   0.0253   0.9935
   7.250   0.8264   0.01117   0.00519  -0.0038   0.0240   0.9956
   7.500   0.8567   0.01147   0.00549  -0.0045   0.0223   0.9980
   7.750   0.8873   0.01182   0.00583  -0.0053   0.0206   0.9994
   8.000   0.9137   0.01212   0.00616  -0.0051   0.0196   1.0000
   8.250   0.9344   0.01239   0.00646  -0.0037   0.0186   1.0000
   8.500   0.9550   0.01270   0.00678  -0.0023   0.0175   1.0000
   8.750   0.9753   0.01305   0.00714  -0.0009   0.0162   1.0000
   9.000   0.9961   0.01339   0.00751   0.0004   0.0154   1.0000
   9.250   1.0170   0.01373   0.00788   0.0017   0.0148   1.0000
   9.500   1.0380   0.01408   0.00826   0.0030   0.0140   1.0000
   9.750   1.0587   0.01447   0.00867   0.0042   0.0134   1.0000
  10.000   1.0791   0.01490   0.00912   0.0055   0.0126   1.0000
  10.250   1.0995   0.01536   0.00962   0.0068   0.0120   1.0000
  10.500   1.1201   0.01578   0.01010   0.0080   0.0116   1.0000
  10.750   1.1408   0.01621   0.01058   0.0092   0.0111   1.0000
  11.000   1.1611   0.01667   0.01108   0.0104   0.0105   1.0000
  11.250   1.1809   0.01718   0.01162   0.0116   0.0101   1.0000
  11.500   1.1999   0.01776   0.01223   0.0129   0.0096   1.0000
  11.750   1.2179   0.01841   0.01295   0.0143   0.0092   1.0000
  12.000   1.2371   0.01892   0.01353   0.0156   0.0089   1.0000
  12.250   1.2552   0.01954   0.01421   0.0169   0.0087   1.0000
  12.500   1.2727   0.02016   0.01490   0.0183   0.0085   1.0000
  12.750   1.2897   0.02081   0.01562   0.0198   0.0081   1.0000
  13.000   1.3057   0.02151   0.01638   0.0213   0.0079   1.0000
  13.250   1.3203   0.02227   0.01721   0.0230   0.0077   1.0000
  13.500   1.3345   0.02304   0.01805   0.0247   0.0075   1.0000
  13.750   1.3438   0.02391   0.01899   0.0271   0.0073   1.0000
  14.000   1.3521   0.02482   0.01998   0.0295   0.0072   1.0000
  14.250   1.3582   0.02593   0.02117   0.0318   0.0070   1.0000
  14.500   1.3632   0.02720   0.02254   0.0339   0.0069   1.0000
  14.750   1.3658   0.02873   0.02418   0.0357   0.0067   1.0000
  15.000   1.3678   0.03044   0.02601   0.0371   0.0067   1.0000
  15.250   1.3722   0.03212   0.02778   0.0379   0.0066   1.0000
  15.500   1.3747   0.03413   0.02991   0.0384   0.0065   1.0000
  15.750   1.3708   0.03706   0.03296   0.0381   0.0065   1.0000
  16.000   1.3679   0.04025   0.03629   0.0371   0.0063   1.0000
  16.250   1.3615   0.04430   0.04048   0.0351   0.0063   1.0000
  16.500   1.3509   0.04942   0.04575   0.0320   0.0063   1.0000
  16.750   1.3288   0.05691   0.05342   0.0271   0.0064   1.0000
  17.000   1.3054   0.06489   0.06157   0.0222   0.0063   1.0000
  17.250   1.2713   0.07474   0.07159   0.0164   0.0063   1.0000
  17.500   1.2168   0.08811   0.08515   0.0089   0.0065   1.0000
  17.750   1.1664   0.10087   0.09808   0.0020   0.0065   1.0000
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