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UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL (ua79sf18-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL (ua79sf18-il)
Reynolds number: 100,000
Max Cl/Cd: 23.11 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ua79sf18-il-100000-n5.txt
Download as CSV file: xf-ua79sf18-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.0705   0.11386   0.10795  -0.1383   0.8506   0.0183
 -13.000  -0.0707   0.10971   0.10383  -0.1400   0.8500   0.0177
 -12.750  -0.0727   0.10526   0.09943  -0.1419   0.8494   0.0172
 -12.500  -0.0781   0.09994   0.09418  -0.1440   0.8488   0.0166
 -12.250  -0.0904   0.09228   0.08662  -0.1474   0.8482   0.0156
 -12.000  -0.1139   0.08144   0.07574  -0.1533   0.8474   0.0147
 -11.750  -0.1277   0.07653   0.07070  -0.1563   0.8466   0.0144
 -11.500  -0.1421   0.07242   0.06655  -0.1581   0.8457   0.0143
 -11.250  -0.1589   0.06867   0.06272  -0.1591   0.8448   0.0142
 -11.000  -0.1750   0.06548   0.05945  -0.1592   0.8436   0.0141
 -10.750  -0.1941   0.06245   0.05628  -0.1586   0.8420   0.0141
 -10.500  -0.2107   0.05990   0.05361  -0.1573   0.8408   0.0140
 -10.250  -0.2270   0.05764   0.05120  -0.1553   0.8396   0.0140
 -10.000  -0.2400   0.05587   0.04928  -0.1530   0.8385   0.0139
  -9.750  -0.2561   0.05414   0.04737  -0.1496   0.8367   0.0139
  -9.500  -0.2774   0.05371   0.04688  -0.1442   0.8331   0.0139
  -9.250  -0.2998   0.05324   0.04631  -0.1382   0.8300   0.0138
  -9.000  -0.3175   0.05249   0.04541  -0.1325   0.8276   0.0138
  -8.750  -0.3280   0.05141   0.04413  -0.1279   0.8258   0.0138
  -8.500  -0.3343   0.04988   0.04234  -0.1238   0.8245   0.0138
  -8.250  -0.3746   0.05145   0.04401  -0.1133   0.8198   0.0138
  -8.000  -0.3948   0.05111   0.04355  -0.1062   0.8162   0.0138
  -7.750  -0.3980   0.04978   0.04197  -0.1019   0.8139   0.0138
  -7.500  -0.3929   0.04813   0.04003  -0.0990   0.8124   0.0138
  -7.250  -0.3804   0.04635   0.03792  -0.0970   0.8114   0.0139
  -7.000  -0.4261   0.04755   0.03921  -0.0853   0.8058   0.0138
  -6.500  -0.4086   0.04504   0.03617  -0.0798   0.8020   0.0140
  -6.250  -0.3885   0.04369   0.03459  -0.0787   0.8006   0.0142
  -6.000  -0.3661   0.04245   0.03315  -0.0779   0.7995   0.0144
  -5.500  -0.3587   0.04104   0.03163  -0.0708   0.7951   0.0151
  -5.250  -0.3560   0.04049   0.03103  -0.0672   0.7924   0.0158
  -5.000  -0.3437   0.03987   0.03034  -0.0651   0.7901   0.0165
  -4.750  -0.3279   0.03928   0.02966  -0.0635   0.7884   0.0180
  -4.500  -0.3068   0.03884   0.02905  -0.0628   0.7869   0.0218
  -4.250  -0.2849   0.03793   0.02804  -0.0622   0.7856   0.0264
  -4.000  -0.2906   0.03785   0.02791  -0.0573   0.7799   0.0292
  -3.750  -0.2748   0.03733   0.02729  -0.0555   0.7773   0.0375
  -3.500  -0.2580   0.03636   0.02670  -0.0542   0.7754   0.0962
  -3.250  -0.2600   0.03375   0.02676  -0.0503   0.7737   0.5219
  -3.000  -0.2474   0.03484   0.02782  -0.0470   0.7706   0.6620
  -2.750  -0.2418   0.03561   0.02854  -0.0426   0.7664   0.6908
  -2.500  -0.2296   0.03656   0.02950  -0.0381   0.7638   0.7211
  -2.250  -0.2128   0.03732   0.03019  -0.0345   0.7617   0.7448
  -2.000  -0.1891   0.03778   0.03043  -0.0328   0.7602   0.7582
  -1.750  -0.1856   0.03811   0.03066  -0.0294   0.7549   0.7677
  -1.500  -0.1680   0.03838   0.03080  -0.0277   0.7517   0.7732
  -1.250  -0.1412   0.03845   0.03067  -0.0282   0.7495   0.7779
  -1.000  -0.1112   0.03851   0.03054  -0.0292   0.7478   0.7807
  -0.750  -0.1007   0.03878   0.03073  -0.0271   0.7431   0.7833
  -0.500  -0.0810   0.03893   0.03076  -0.0266   0.7392   0.7858
  -0.250  -0.0531   0.03902   0.03070  -0.0273   0.7368   0.7881
   0.000  -0.0218   0.03910   0.03063  -0.0287   0.7351   0.7899
   0.250  -0.0118   0.03939   0.03085  -0.0269   0.7291   0.7919
   0.500   0.0125   0.03953   0.03086  -0.0271   0.7257   0.7934
   0.750   0.0423   0.03962   0.03085  -0.0280   0.7236   0.7945
   1.000   0.0751   0.03968   0.03080  -0.0294   0.7220   0.7957
   1.500   0.1113   0.04010   0.03109  -0.0282   0.7113   0.7991
   1.750   0.1441   0.04014   0.03105  -0.0296   0.7095   0.8004
   2.000   0.1527   0.04059   0.03147  -0.0279   0.7016   0.8026
   2.250   0.1801   0.04070   0.03155  -0.0284   0.6985   0.8043
   2.500   0.2111   0.04074   0.03155  -0.0295   0.6965   0.8056
   3.000   0.2478   0.04137   0.03215  -0.0285   0.6855   0.8084
   3.250   0.2788   0.04139   0.03216  -0.0296   0.6833   0.8093
   3.500   0.2905   0.04191   0.03269  -0.0284   0.6756   0.8106
   3.750   0.3183   0.04199   0.03276  -0.0291   0.6722   0.8117
   4.000   0.3505   0.04193   0.03270  -0.0304   0.6700   0.8130
   4.250   0.3628   0.04242   0.03321  -0.0292   0.6613   0.8148
   4.500   0.3941   0.04227   0.03307  -0.0302   0.6583   0.8163
   5.000   0.4382   0.04260   0.03348  -0.0300   0.6465   0.8188
   5.250   0.4708   0.04237   0.03333  -0.0311   0.6441   0.8201
   5.500   0.4828   0.04302   0.03404  -0.0299   0.6348   0.8217
   5.750   0.5136   0.04284   0.03391  -0.0308   0.6315   0.8234
   6.000   0.5482   0.04243   0.03357  -0.0321   0.6294   0.8251
   6.250   0.5582   0.04318   0.03439  -0.0307   0.6183   0.8272
   6.500   0.5927   0.04268   0.03402  -0.0319   0.6157   0.8293
   6.750   0.6033   0.04339   0.03483  -0.0305   0.6048   0.8313
   7.000   0.6361   0.04290   0.03445  -0.0314   0.6021   0.8335
   7.500   0.6814   0.04305   0.03484  -0.0311   0.5888   0.8390
   7.750   0.6965   0.04366   0.03556  -0.0303   0.5787   0.8423
   8.000   0.7354   0.04075   0.03272  -0.0298   0.5617   0.8457
   8.750   0.8027   0.03998   0.03234  -0.0279   0.5111   0.8602
   9.000   0.8387   0.03811   0.03023  -0.0276   0.4575   0.8669
   9.250   0.8662   0.03756   0.02953  -0.0272   0.4186   0.8746
   9.500   0.8798   0.03807   0.02971  -0.0257   0.3594   0.8843
   9.750   0.8842   0.03944   0.03074  -0.0237   0.3012   0.8968
  10.250   0.8714   0.04458   0.03455  -0.0194   0.1025   0.9357
  10.750   0.8766   0.04843   0.03780  -0.0166   0.0132   1.0000
  11.000   0.8895   0.04989   0.03933  -0.0162   0.0119   1.0000
  11.250   0.9024   0.05135   0.04092  -0.0158   0.0114   1.0000
  11.500   0.9143   0.05290   0.04262  -0.0154   0.0110   1.0000
  11.750   0.9247   0.05462   0.04450  -0.0148   0.0106   1.0000
  12.000   0.9351   0.05635   0.04638  -0.0143   0.0104   1.0000
  12.250   0.9430   0.05835   0.04856  -0.0137   0.0101   1.0000
  12.500   0.9502   0.06045   0.05082  -0.0132   0.0100   1.0000
  12.750   0.9563   0.06269   0.05323  -0.0126   0.0098   1.0000
  13.000   0.9613   0.06508   0.05579  -0.0122   0.0097   1.0000
  13.250   0.9642   0.06779   0.05874  -0.0117   0.0096   1.0000
  13.500   0.9666   0.07056   0.06167  -0.0113   0.0095   1.0000
  13.750   0.9683   0.07347   0.06475  -0.0110   0.0094   1.0000
  14.000   0.9701   0.07641   0.06784  -0.0108   0.0093   1.0000
  14.250   0.9726   0.07930   0.07087  -0.0107   0.0092   1.0000
  14.500   0.9737   0.08237   0.07406  -0.0106   0.0087   1.0000
  14.750   0.9768   0.08521   0.07701  -0.0106   0.0085   1.0000
  15.000   0.9835   0.08761   0.07954  -0.0106   0.0086   1.0000
  15.250   0.9864   0.09037   0.08235  -0.0104   0.0078   1.0000
  15.500   0.9965   0.09228   0.08433  -0.0100   0.0075   1.0000
  15.750   1.0097   0.09398   0.08614  -0.0094   0.0073   1.0000
  16.000   1.0186   0.09640   0.08870  -0.0094   0.0072   1.0000
  16.250   1.0252   0.09913   0.09162  -0.0096   0.0071   1.0000
  16.500   1.0297   0.10221   0.09490  -0.0099   0.0071   1.0000
  16.750   1.0327   0.10551   0.09839  -0.0105   0.0072   1.0000
  17.000   1.0321   0.10936   0.10245  -0.0113   0.0072   1.0000
  17.250   1.0303   0.11339   0.10668  -0.0124   0.0072   1.0000
  17.500   1.0257   0.11790   0.11141  -0.0139   0.0072   1.0000
  18.500   0.9967   0.13849   0.13291  -0.0234   0.0073   1.0000
  18.750   0.9891   0.14406   0.13866  -0.0266   0.0074   1.0000
  19.000   0.9801   0.15016   0.14493  -0.0302   0.0074   1.0000
  19.250   0.9715   0.15643   0.15138  -0.0341   0.0075   1.0000
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