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UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL (ua79sf18-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL (ua79sf18-il)
Reynolds number: 1,000,000
Max Cl/Cd: 114.11 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ua79sf18-il-1000000-n5.txt
Download as CSV file: xf-ua79sf18-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.2453   0.05951   0.05632  -0.1515   0.7580   0.0014
 -13.000  -0.2554   0.05471   0.05145  -0.1544   0.7576   0.0014
 -12.750  -0.2814   0.04892   0.04552  -0.1565   0.7570   0.0013
 -12.500  -0.3079   0.04398   0.04042  -0.1569   0.7562   0.0013
 -12.250  -0.3165   0.04128   0.03763  -0.1566   0.7556   0.0012
 -12.000  -0.3417   0.03709   0.03321  -0.1551   0.7547   0.0013
 -11.750  -0.3522   0.03445   0.03041  -0.1536   0.7540   0.0013
 -11.500  -0.3589   0.03221   0.02802  -0.1519   0.7532   0.0013
 -11.250  -0.3642   0.03004   0.02568  -0.1500   0.7526   0.0013
 -11.000  -0.3641   0.02833   0.02382  -0.1482   0.7520   0.0013
 -10.750  -0.3646   0.02644   0.02173  -0.1460   0.7513   0.0014
 -10.500  -0.3565   0.02534   0.02051  -0.1445   0.7508   0.0014
 -10.250  -0.3423   0.02491   0.02003  -0.1436   0.7503   0.0015
 -10.000  -0.3416   0.02267   0.01754  -0.1410   0.7497   0.0014
  -9.750  -0.3291   0.02176   0.01652  -0.1396   0.7492   0.0015
  -9.500  -0.3155   0.02091   0.01557  -0.1383   0.7487   0.0015
  -9.250  -0.3053   0.01910   0.01352  -0.1365   0.7482   0.0018
  -9.000  -0.2917   0.01807   0.01238  -0.1350   0.7476   0.0019
  -8.750  -0.2743   0.01750   0.01172  -0.1340   0.7471   0.0018
  -8.500  -0.2607   0.01666   0.01082  -0.1324   0.7466   0.0020
  -8.250  -0.2441   0.01615   0.01027  -0.1313   0.7463   0.0021
  -8.000  -0.2283   0.01561   0.00969  -0.1299   0.7458   0.0022
  -7.750  -0.2158   0.01498   0.00899  -0.1278   0.7453   0.0022
  -7.500  -0.2000   0.01470   0.00870  -0.1263   0.7447   0.0024
  -7.250  -0.1874   0.01424   0.00819  -0.1240   0.7441   0.0024
  -7.000  -0.1708   0.01382   0.00772  -0.1225   0.7436   0.0025
  -6.750  -0.1539   0.01337   0.00723  -0.1211   0.7431   0.0026
  -6.500  -0.1352   0.01299   0.00680  -0.1199   0.7425   0.0026
  -6.250  -0.1157   0.01263   0.00640  -0.1189   0.7420   0.0027
  -6.000  -0.0936   0.01239   0.00614  -0.1184   0.7415   0.0031
  -5.750  -0.0724   0.01207   0.00579  -0.1176   0.7410   0.0032
  -5.500  -0.0503   0.01178   0.00546  -0.1170   0.7404   0.0034
  -5.250  -0.0281   0.01147   0.00511  -0.1164   0.7398   0.0035
  -5.000  -0.0048   0.01120   0.00479  -0.1160   0.7391   0.0035
  -4.750   0.0193   0.01097   0.00452  -0.1157   0.7386   0.0036
  -4.500   0.0440   0.01077   0.00428  -0.1155   0.7381   0.0037
  -4.250   0.0695   0.01060   0.00406  -0.1155   0.7377   0.0038
  -4.000   0.0953   0.01044   0.00386  -0.1155   0.7373   0.0047
  -3.750   0.1213   0.01029   0.00371  -0.1155   0.7368   0.0079
  -3.500   0.1446   0.00994   0.00351  -0.1152   0.7363   0.0461
  -3.250   0.1627   0.00921   0.00323  -0.1142   0.7359   0.1695
  -3.000   0.1812   0.00844   0.00295  -0.1135   0.7354   0.3114
  -2.750   0.1940   0.00721   0.00277  -0.1118   0.7349   0.6169
  -2.500   0.2238   0.00737   0.00285  -0.1125   0.7345   0.6318
  -2.250   0.2528   0.00745   0.00294  -0.1130   0.7341   0.6379
  -2.000   0.2817   0.00758   0.00301  -0.1135   0.7336   0.6447
  -1.750   0.3103   0.00762   0.00305  -0.1140   0.7330   0.6484
  -1.500   0.3389   0.00766   0.00309  -0.1145   0.7322   0.6512
  -1.250   0.3676   0.00769   0.00311  -0.1151   0.7314   0.6535
  -1.000   0.3964   0.00772   0.00313  -0.1156   0.7305   0.6556
  -0.750   0.4253   0.00777   0.00315  -0.1162   0.7298   0.6576
  -0.500   0.4541   0.00781   0.00318  -0.1168   0.7291   0.6590
  -0.250   0.4830   0.00782   0.00317  -0.1174   0.7284   0.6601
   0.000   0.5118   0.00780   0.00315  -0.1180   0.7275   0.6611
   0.250   0.5408   0.00777   0.00312  -0.1186   0.7265   0.6618
   0.500   0.5699   0.00773   0.00308  -0.1193   0.7254   0.6623
   0.750   0.5991   0.00770   0.00304  -0.1200   0.7244   0.6627
   1.000   0.6283   0.00767   0.00301  -0.1206   0.7234   0.6628
   1.250   0.6578   0.00765   0.00298  -0.1214   0.7224   0.6630
   1.500   0.6859   0.00765   0.00300  -0.1218   0.7211   0.6632
   1.750   0.7129   0.00765   0.00303  -0.1221   0.7189   0.6637
   2.000   0.7404   0.00762   0.00302  -0.1224   0.7164   0.6641
   2.250   0.7684   0.00756   0.00297  -0.1228   0.7135   0.6645
   2.500   0.7971   0.00748   0.00290  -0.1233   0.7105   0.6649
   2.750   0.8208   0.00734   0.00274  -0.1227   0.6971   0.6653
   3.000   0.8353   0.00732   0.00257  -0.1201   0.6519   0.6654
   3.250   0.8358   0.00776   0.00279  -0.1148   0.6103   0.6656
   3.500   0.8091   0.00848   0.00328  -0.1040   0.5624   0.6658
   3.750   0.7846   0.00955   0.00420  -0.0944   0.5282   0.6660
   4.000   0.7697   0.01083   0.00536  -0.0875   0.4973   0.6662
   4.250   0.7652   0.01200   0.00643  -0.0828   0.4719   0.6663
   4.500   0.7314   0.01423   0.00832  -0.0735   0.4087   0.6665
   4.750   0.7157   0.01584   0.00964  -0.0672   0.3513   0.6667
   5.000   0.6982   0.01758   0.01097  -0.0608   0.2758   0.6669
   5.250   0.7118   0.01816   0.01150  -0.0592   0.2584   0.6670
   5.500   0.6585   0.02172   0.01394  -0.0481   0.0240   0.6671
   5.750   0.6755   0.02226   0.01443  -0.0472   0.0067   0.6672
   6.000   0.6946   0.02271   0.01488  -0.0465   0.0052   0.6673
   6.250   0.7139   0.02316   0.01533  -0.0459   0.0045   0.6674
   6.500   0.7331   0.02362   0.01582  -0.0453   0.0034   0.6675
   6.750   0.7524   0.02409   0.01630  -0.0446   0.0033   0.6676
   7.000   0.7714   0.02458   0.01683  -0.0440   0.0031   0.6677
   7.250   0.7899   0.02510   0.01740  -0.0433   0.0029   0.6678
   7.500   0.8074   0.02568   0.01802  -0.0424   0.0027   0.6679
   7.750   0.8249   0.02627   0.01864  -0.0417   0.0025   0.6680
   8.000   0.8425   0.02686   0.01926  -0.0409   0.0023   0.6682
   8.250   0.8595   0.02750   0.01994  -0.0401   0.0021   0.6683
   8.500   0.8765   0.02815   0.02061  -0.0393   0.0018   0.6684
   8.750   0.8919   0.02891   0.02141  -0.0384   0.0018   0.6685
   9.000   0.9069   0.02970   0.02224  -0.0374   0.0015   0.6687
   9.250   0.9215   0.03054   0.02312  -0.0364   0.0016   0.6688
   9.500   0.9357   0.03141   0.02404  -0.0354   0.0013   0.6689
   9.750   0.9496   0.03232   0.02501  -0.0343   0.0014   0.6690
  10.000   0.9613   0.03340   0.02613  -0.0331   0.0012   0.6691
  10.250   0.9733   0.03449   0.02727  -0.0320   0.0012   0.6693
  10.500   0.9680   0.03688   0.02977  -0.0289   0.0010   0.6694
  10.750   0.9761   0.03833   0.03128  -0.0276   0.0010   0.6695
  11.000   0.9850   0.03976   0.03276  -0.0263   0.0010   0.6697
  11.250   0.9943   0.04118   0.03424  -0.0251   0.0010   0.6698
  11.500   1.0013   0.04281   0.03592  -0.0238   0.0010   0.6700
  11.750   1.0088   0.04445   0.03763  -0.0226   0.0009   0.6701
  12.000   1.0169   0.04606   0.03929  -0.0215   0.0009   0.6702
  12.250   1.0252   0.04771   0.04101  -0.0204   0.0009   0.6704
  12.500   1.0339   0.04933   0.04270  -0.0195   0.0009   0.6705
  12.750   1.0437   0.05089   0.04432  -0.0186   0.0009   0.6706
  13.000   1.0539   0.05245   0.04594  -0.0178   0.0009   0.6708
  13.250   1.0654   0.05397   0.04752  -0.0171   0.0009   0.6710
  13.500   1.0778   0.05543   0.04905  -0.0164   0.0009   0.6711
  13.750   1.0915   0.05686   0.05055  -0.0159   0.0009   0.6713
  14.000   1.1055   0.05833   0.05210  -0.0154   0.0009   0.6715
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