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UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT (ua79sfm-il) Xfoil prediction polar at RE=50,000 Ncrit=9


Details Polar file
Airfoil: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT (ua79sfm-il)
Reynolds number: 50,000
Max Cl/Cd: 12.18 at α=17.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ua79sfm-il-50000.txt
Download as CSV file: xf-ua79sfm-il-50000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.3183   0.13237   0.12673  -0.0383  -0.0009   4.0112
 -11.500  -0.3012   0.12917   0.12353  -0.0368  -0.0009   3.9855
 -11.250  -0.3198   0.12584   0.12029  -0.0378  -0.0009   3.9603
 -11.000  -0.2978   0.12247   0.11690  -0.0360  -0.0009   3.9267
 -10.750  -0.3023   0.11894   0.11344  -0.0359  -0.0009   3.9001
 -10.500  -0.3041   0.11622   0.11076  -0.0355  -0.0009   3.8595
 -10.250  -0.2912   0.11290   0.10745  -0.0344  -0.0009   3.8308
 -10.000  -0.3001   0.10987   0.10450  -0.0344  -0.0009   3.7953
  -9.750  -0.2905   0.10696   0.10159  -0.0333  -0.0009   3.7548
  -9.500  -0.2887   0.10382   0.09850  -0.0328  -0.0009   3.7285
  -9.250  -0.3038   0.10181   0.09659  -0.0328  -0.0009   3.6826
  -9.000  -0.2853   0.09801   0.09277  -0.0316  -0.0009   3.6671
  -8.750  -0.2828   0.09522   0.09001  -0.0310  -0.0009   3.6429
  -8.500  -0.2909   0.09250   0.08737  -0.0309  -0.0009   3.6150
  -8.250  -0.2920   0.08954   0.08445  -0.0306  -0.0009   3.6134
  -8.000  -0.3842   0.07956   0.07462  -0.0446  -0.0009   4.1722
  -7.750  -0.4540   0.07478   0.06995  -0.0498  -0.0009   4.2172
  -7.500  -0.4765   0.06903   0.06411  -0.0517  -0.0009   4.2784
  -7.250  -0.4881   0.06443   0.05939  -0.0522  -0.0009   4.3126
  -7.000  -0.4994   0.05996   0.05473  -0.0523  -0.0009   4.3350
  -6.750  -0.5065   0.05576   0.05023  -0.0519  -0.0009   4.3534
  -6.500  -0.5098   0.05181   0.04588  -0.0510  -0.0009   4.3688
  -6.250  -0.5018   0.04890   0.04292  -0.0496  -0.0009   4.3743
  -6.000  -0.4996   0.04556   0.03903  -0.0481  -0.0009   4.3850
  -5.750  -0.4907   0.04302   0.03637  -0.0466  -0.0009   4.3875
  -5.500  -0.4817   0.04062   0.03375  -0.0450  -0.0009   4.3897
  -5.250  -0.4718   0.03838   0.03124  -0.0434  -0.0009   4.3911
  -5.000  -0.4606   0.03637   0.02895  -0.0417  -0.0009   4.3914
  -4.750  -0.4483   0.03458   0.02689  -0.0399  -0.0009   4.3907
  -4.500  -0.4347   0.03299   0.02501  -0.0382  -0.0009   4.3890
  -4.250  -0.4194   0.03160   0.02334  -0.0364  -0.0009   4.3867
  -4.000  -0.1472   0.04274   0.03666  -0.0325  -0.0009   2.0009
  -3.750  -0.1492   0.04149   0.03523  -0.0319  -0.0009   2.0009
  -3.500  -0.1504   0.04038   0.03395  -0.0311  -0.0009   2.0009
  -3.250  -0.1508   0.03941   0.03280  -0.0302  -0.0009   2.0009
  -3.000  -0.1505   0.03851   0.03173  -0.0292  -0.0009   2.0009
  -2.750  -0.1494   0.03773   0.03078  -0.0282  -0.0009   2.0009
  -2.500  -0.1476   0.03701   0.02989  -0.0270  -0.0009   2.0009
  -2.250  -0.1452   0.03638   0.02909  -0.0258  -0.0009   2.0009
  -2.000  -0.1424   0.03580   0.02836  -0.0246  -0.0009   2.0009
  -1.750  -0.1391   0.03527   0.02769  -0.0233  -0.0009   2.0009
  -1.500  -0.1354   0.03479   0.02707  -0.0220  -0.0009   2.0009
  -1.250  -0.1314   0.03436   0.02650  -0.0207  -0.0009   2.0009
  -1.000  -0.1271   0.03398   0.02599  -0.0194  -0.0009   2.0009
  -0.750  -0.1225   0.03363   0.02552  -0.0181  -0.0009   2.0009
  -0.500  -0.1178   0.03330   0.02508  -0.0168  -0.0009   2.0009
  -0.250  -0.1129   0.03301   0.02468  -0.0155  -0.0009   2.0009
   0.000  -0.1078   0.03275   0.02432  -0.0142  -0.0009   2.0009
   0.250  -0.1026   0.03252   0.02399  -0.0129  -0.0009   2.0009
   0.500  -0.0972   0.03233   0.02371  -0.0116  -0.0009   2.0009
   0.750  -0.0918   0.03214   0.02343  -0.0103  -0.0009   2.0009
   1.000  -0.0862   0.03199   0.02321  -0.0091  -0.0009   2.0009
   1.250  -0.0806   0.03187   0.02302  -0.0079  -0.0009   2.0009
   1.500  -0.0749   0.03177   0.02286  -0.0067  -0.0009   2.0009
   1.750  -0.0692   0.03170   0.02272  -0.0055  -0.0009   2.0009
   2.000  -0.0634   0.03164   0.02261  -0.0043  -0.0009   2.0009
   2.250  -0.0576   0.03161   0.02254  -0.0031  -0.0009   2.0009
   2.500  -0.0518   0.03162   0.02251  -0.0020  -0.0009   2.0009
   2.750  -0.0459   0.03162   0.02247  -0.0009  -0.0009   2.0009
   3.000  -0.0401   0.03167   0.02248   0.0002  -0.0009   2.0009
   3.250  -0.0343   0.03173   0.02253   0.0012  -0.0009   2.0009
   3.500  -0.0283   0.03185   0.02262   0.0022  -0.0009   2.0009
   3.750  -0.0125   0.03247   0.02322   0.0020  -0.0004   2.0009
   4.000   0.0037   0.03376   0.02444   0.0017   0.0000   2.0009
   4.250   0.0154   0.03385   0.02452   0.0020   0.0001   2.0009
   4.500   0.0343   0.03617   0.02681   0.0014  -0.0002   2.0009
   4.750   0.0403   0.03526   0.02592   0.0023  -0.0010   2.0009
   5.000   0.0575   0.03726   0.02791   0.0019  -0.0016   2.0009
   5.250   0.0625   0.03655   0.02723   0.0029  -0.0014   2.0009
   5.500   0.0773   0.03822   0.02889   0.0028  -0.0008   2.0009
   5.750   0.0829   0.03787   0.02858   0.0036  -0.0001   2.0009
   6.000   0.0951   0.03920   0.02992   0.0037   0.0000   2.0009
   6.250   0.1026   0.03930   0.03006   0.0043  -0.0004   2.0009
   6.500   0.1105   0.03997   0.03076   0.0049  -0.0004   2.0009
   6.750   0.1232   0.04107   0.03189   0.0049   0.0007   2.0009
   7.000   0.1269   0.04105   0.03192   0.0058   0.0035   2.0009
   7.250   0.1383   0.04230   0.03322   0.0060   0.0074   2.0009
   7.500   0.1457   0.04267   0.03364   0.0065   0.0142   2.0009
   7.750   0.1509   0.04314   0.03416   0.0072   0.0198   2.0009
   8.000   0.1660   0.04486   0.03593   0.0070   0.0273   2.0009
   8.250   0.1670   0.04454   0.03567   0.0080   0.0351   2.0009
   8.500   0.1750   0.04543   0.03662   0.0084   0.0427   2.0009
   8.750   0.1883   0.04690   0.03819   0.0084   0.0535   2.0009
   9.000   0.1912   0.04697   0.03833   0.0091   0.0674   2.0009
   9.250   0.1960   0.04750   0.03893   0.0097   0.0824   2.0009
   9.500   0.2044   0.04851   0.04002   0.0100   0.0990   2.0009
   9.750   0.2176   0.05012   0.04173   0.0099   0.1204   2.0009
  10.000   0.2185   0.05009   0.04177   0.0108   0.1430   2.0009
  10.250   0.2236   0.05089   0.04266   0.0112   0.1617   2.0009
  10.500   0.2376   0.05276   0.04463   0.0111   0.1836   2.0009
  10.750   0.2400   0.05296   0.04493   0.0117   0.2094   2.0009
  11.000   0.2429   0.05357   0.04563   0.0123   0.2335   2.0009
  11.250   0.2497   0.05465   0.04680   0.0125   0.2576   2.0009
  11.500   0.2614   0.05632   0.04858   0.0125   0.2871   2.0009
  11.750   0.2653   0.05688   0.04925   0.0130   0.3220   2.0009
  12.000   0.2663   0.05745   0.04992   0.0136   0.3546   2.0009
  12.250   0.2727   0.05869   0.05126   0.0138   0.3841   2.0009
  12.500   0.2882   0.06101   0.05372   0.0136   0.4233   2.0009
  12.750   0.2841   0.06079   0.05358   0.0144   0.4622   2.0009
  13.000   0.2868   0.06172   0.05462   0.0148   0.4972   2.0009
  13.250   0.2976   0.06369   0.05671   0.0148   0.5328   2.0009
  13.500   0.3045   0.06487   0.05801   0.0150   0.5790   2.0009
  13.750   0.3021   0.06530   0.05853   0.0156   0.6205   2.0009
  14.000   0.3053   0.06652   0.05986   0.0158   0.6565   2.0009
  14.250   0.3168   0.06875   0.06223   0.0158   0.6991   2.0009
  14.500   0.3179   0.06936   0.06295   0.0162   0.7482   2.0009
  14.750   0.3162   0.07021   0.06389   0.0166   0.7901   2.0009
  15.000   0.3232   0.07205   0.06585   0.0167   0.8286   2.0009
  15.250   0.3329   0.07396   0.06791   0.0169   0.8822   2.0009
  15.500   0.3270   0.07426   0.06828   0.0172   0.9288   2.0009
  15.750   0.3306   0.07588   0.07000   0.0174   0.9688   2.0009
  16.000   0.3441   0.07851   0.07279   0.0175   1.0220   2.0009
  16.250   0.3378   0.07859   0.07294   0.0179   1.0739   2.0009
  16.500   0.3378   0.07992   0.07437   0.0180   1.1164   2.0009
  16.750   0.3492   0.08242   0.07701   0.0182   1.1635   2.0009
  17.000   0.3457   0.08293   0.07761   0.0184   1.2171   2.0009
  17.250   0.3452   0.08440   0.07918   0.0186   1.2564   2.0009
  17.500   0.3582   0.08720   0.08215   0.0189   1.3087   2.0009
  17.750   0.5652   0.04642   0.04099   0.0509   3.5495   2.0009
  18.000   0.5594   0.04879   0.04361   0.0506   3.5526   2.0009
  18.250   0.5480   0.05179   0.04684   0.0495   3.5512   2.0009
  18.500   0.5341   0.05534   0.05058   0.0481   3.5451   2.0009
  18.750   0.4913   0.06389   0.05943   0.0428   3.4961   2.0009
  19.000   0.4508   0.07483   0.07037   0.0370   3.4392   2.0009
  19.250   0.4418   0.07933   0.07486   0.0355   3.4287   2.0009
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