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NACA 63(3)-018 (naca633018-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(3)-018 (naca633018-il)
Reynolds number: 100,000
Max Cl/Cd: 36.37 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca633018-il-100000-n5.txt
Download as CSV file: xf-naca633018-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(3)-018                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.9417   0.11905   0.11331  -0.0080   1.0000   0.0509
 -17.750  -0.9801   0.10798   0.10193  -0.0148   1.0000   0.0511
 -17.500  -1.0094   0.09934   0.09298  -0.0197   1.0000   0.0514
 -17.250  -1.0072   0.09605   0.08969  -0.0211   1.0000   0.0526
 -17.000  -1.0051   0.09287   0.08649  -0.0225   1.0000   0.0538
 -16.750  -1.0111   0.08851   0.08200  -0.0246   1.0000   0.0548
 -16.500  -1.0187   0.08400   0.07734  -0.0266   1.0000   0.0558
 -16.250  -1.0261   0.07964   0.07279  -0.0284   1.0000   0.0568
 -16.000  -1.0325   0.07553   0.06847  -0.0299   1.0000   0.0579
 -15.750  -1.0375   0.07170   0.06441  -0.0311   1.0000   0.0590
 -15.500  -1.0414   0.06814   0.06060  -0.0321   1.0000   0.0601
 -15.250  -1.0414   0.06508   0.05733  -0.0327   1.0000   0.0613
 -15.000  -1.0272   0.06343   0.05571  -0.0327   1.0000   0.0628
 -14.750  -1.0176   0.06147   0.05370  -0.0328   1.0000   0.0641
 -14.500  -1.0087   0.05945   0.05160  -0.0330   1.0000   0.0656
 -14.250  -1.0001   0.05742   0.04946  -0.0331   1.0000   0.0672
 -14.000  -0.9911   0.05545   0.04735  -0.0331   1.0000   0.0690
 -13.750  -0.9803   0.05364   0.04538  -0.0331   1.0000   0.0707
 -13.500  -0.9662   0.05215   0.04381  -0.0328   1.0000   0.0725
 -13.250  -0.9517   0.05079   0.04248  -0.0325   1.0000   0.0742
 -13.000  -0.9390   0.04935   0.04102  -0.0323   1.0000   0.0762
 -12.750  -0.9266   0.04789   0.03952  -0.0321   1.0000   0.0785
 -12.500  -0.9135   0.04651   0.03805  -0.0318   1.0000   0.0811
 -12.250  -0.9000   0.04519   0.03666  -0.0314   1.0000   0.0838
 -12.000  -0.8890   0.04375   0.03527  -0.0310   1.0000   0.0865
 -11.750  -0.8783   0.04229   0.03381  -0.0307   1.0000   0.0896
 -11.500  -0.8668   0.04091   0.03240  -0.0303   1.0000   0.0931
 -11.250  -0.8559   0.03951   0.03098  -0.0299   1.0000   0.0971
 -11.000  -0.8488   0.03784   0.02937  -0.0295   1.0000   0.1016
 -10.750  -0.8395   0.03636   0.02787  -0.0290   1.0000   0.1076
 -10.500  -0.8329   0.03471   0.02627  -0.0286   1.0000   0.1139
 -10.250  -0.8250   0.03318   0.02475  -0.0281   1.0000   0.1222
 -10.000  -0.8201   0.03148   0.02314  -0.0275   1.0000   0.1318
  -9.750  -0.8147   0.02988   0.02162  -0.0269   1.0000   0.1438
  -9.500  -0.8106   0.02827   0.02011  -0.0262   1.0000   0.1593
  -9.250  -0.8082   0.02672   0.01870  -0.0252   1.0000   0.1781
  -9.000  -0.7931   0.02502   0.01711  -0.0270   0.9456   0.2081
  -8.750  -0.7843   0.02359   0.01579  -0.0267   0.9213   0.2405
  -8.500  -0.7827   0.02260   0.01490  -0.0241   0.9011   0.2698
  -8.250  -0.7800   0.02187   0.01428  -0.0210   0.8854   0.3015
  -8.000  -0.7725   0.02131   0.01383  -0.0184   0.8726   0.3350
  -7.750  -0.7609   0.02092   0.01351  -0.0161   0.8613   0.3661
  -7.500  -0.7458   0.02066   0.01325  -0.0143   0.8505   0.3928
  -7.250  -0.7297   0.02045   0.01297  -0.0125   0.8415   0.4163
  -7.000  -0.7108   0.02033   0.01283  -0.0111   0.8320   0.4368
  -6.750  -0.6910   0.02032   0.01277  -0.0097   0.8240   0.4565
  -6.500  -0.6701   0.02035   0.01272  -0.0085   0.8153   0.4752
  -6.250  -0.6483   0.02042   0.01272  -0.0073   0.8081   0.4913
  -6.000  -0.6248   0.02047   0.01270  -0.0065   0.7999   0.5041
  -5.750  -0.6030   0.02039   0.01246  -0.0055   0.7936   0.5155
  -5.500  -0.5768   0.02048   0.01252  -0.0051   0.7855   0.5253
  -5.250  -0.5520   0.02052   0.01246  -0.0043   0.7792   0.5348
  -5.000  -0.5286   0.02044   0.01225  -0.0037   0.7719   0.5450
  -4.750  -0.5013   0.02052   0.01230  -0.0033   0.7652   0.5515
  -4.500  -0.4768   0.02040   0.01206  -0.0027   0.7595   0.5591
  -4.250  -0.4508   0.02032   0.01192  -0.0026   0.7521   0.5654
  -4.000  -0.4243   0.02029   0.01182  -0.0021   0.7464   0.5711
  -3.750  -0.4007   0.02006   0.01144  -0.0018   0.7400   0.5789
  -3.500  -0.3726   0.02010   0.01147  -0.0017   0.7336   0.5832
  -3.250  -0.3464   0.02001   0.01130  -0.0013   0.7286   0.5888
  -3.000  -0.3216   0.01982   0.01101  -0.0012   0.7219   0.5957
  -2.750  -0.2939   0.01983   0.01100  -0.0011   0.7159   0.5997
  -2.500  -0.2674   0.01975   0.01084  -0.0007   0.7113   0.6050
  -2.250  -0.2422   0.01959   0.01060  -0.0008   0.7047   0.6118
  -2.000  -0.2145   0.01959   0.01061  -0.0006   0.6990   0.6155
  -1.750  -0.1875   0.01953   0.01048  -0.0004   0.6946   0.6205
  -1.500  -0.1618   0.01943   0.01032  -0.0005   0.6881   0.6271
  -1.250  -0.1344   0.01942   0.01032  -0.0004   0.6826   0.6311
  -1.000  -0.1072   0.01938   0.01024  -0.0001   0.6783   0.6356
  -0.750  -0.0809   0.01934   0.01019  -0.0002   0.6721   0.6418
  -0.500  -0.0540   0.01932   0.01016  -0.0002   0.6666   0.6466
  -0.250  -0.0266   0.01931   0.01013   0.0000   0.6624   0.6510
   0.000   0.0000   0.01932   0.01014   0.0000   0.6567   0.6567
   0.250   0.0266   0.01931   0.01013   0.0000   0.6510   0.6624
   0.500   0.0540   0.01932   0.01016   0.0002   0.6466   0.6666
   0.750   0.0809   0.01934   0.01019   0.0002   0.6417   0.6721
   1.000   0.1072   0.01938   0.01024   0.0001   0.6356   0.6783
   1.250   0.1344   0.01942   0.01032   0.0004   0.6311   0.6826
   1.500   0.1618   0.01943   0.01032   0.0005   0.6270   0.6881
   1.750   0.1875   0.01953   0.01048   0.0004   0.6205   0.6946
   2.000   0.2145   0.01959   0.01061   0.0006   0.6155   0.6990
   2.250   0.2422   0.01959   0.01060   0.0008   0.6118   0.7047
   2.500   0.2674   0.01975   0.01084   0.0007   0.6050   0.7113
   2.750   0.2939   0.01983   0.01100   0.0011   0.5997   0.7159
   3.000   0.3216   0.01982   0.01101   0.0012   0.5957   0.7219
   3.250   0.3465   0.02001   0.01130   0.0013   0.5888   0.7286
   3.500   0.3726   0.02010   0.01147   0.0017   0.5832   0.7336
   3.750   0.4007   0.02006   0.01144   0.0018   0.5789   0.7400
   4.000   0.4243   0.02030   0.01182   0.0021   0.5711   0.7464
   4.250   0.4508   0.02032   0.01191   0.0026   0.5654   0.7521
   4.500   0.4769   0.02040   0.01206   0.0027   0.5591   0.7595
   4.750   0.5013   0.02052   0.01230   0.0033   0.5515   0.7652
   5.000   0.5286   0.02044   0.01225   0.0037   0.5450   0.7719
   5.250   0.5520   0.02052   0.01246   0.0043   0.5348   0.7792
   5.500   0.5768   0.02048   0.01251   0.0051   0.5253   0.7854
   5.750   0.6030   0.02039   0.01246   0.0054   0.5155   0.7936
   6.000   0.6249   0.02047   0.01270   0.0065   0.5041   0.7999
   6.250   0.6484   0.02042   0.01272   0.0073   0.4913   0.8081
   6.500   0.6702   0.02035   0.01272   0.0085   0.4753   0.8153
   6.750   0.6910   0.02032   0.01276   0.0097   0.4566   0.8240
   7.000   0.7109   0.02033   0.01283   0.0111   0.4369   0.8320
   7.250   0.7297   0.02044   0.01297   0.0125   0.4163   0.8416
   7.500   0.7458   0.02066   0.01325   0.0143   0.3925   0.8505
   7.750   0.7609   0.02092   0.01351   0.0161   0.3657   0.8613
   8.000   0.7726   0.02130   0.01382   0.0184   0.3349   0.8726
   8.250   0.7801   0.02187   0.01428   0.0210   0.3013   0.8853
   8.500   0.7830   0.02260   0.01490   0.0241   0.2699   0.9011
   8.750   0.7845   0.02359   0.01579   0.0267   0.2403   0.9213
   9.000   0.7935   0.02501   0.01710   0.0269   0.2083   0.9456
   9.250   0.8085   0.02671   0.01869   0.0252   0.1781   1.0000
   9.500   0.8111   0.02826   0.02010   0.0261   0.1593   1.0000
   9.750   0.8154   0.02985   0.02159   0.0268   0.1440   1.0000
  10.000   0.8207   0.03147   0.02313   0.0274   0.1318   1.0000
  10.250   0.8257   0.03316   0.02473   0.0280   0.1224   1.0000
  10.500   0.8336   0.03469   0.02624   0.0285   0.1139   1.0000
  10.750   0.8402   0.03634   0.02785   0.0290   0.1076   1.0000
  11.000   0.8496   0.03782   0.02935   0.0294   0.1015   1.0000
  11.250   0.8566   0.03949   0.03095   0.0298   0.0970   1.0000
  11.500   0.8677   0.04088   0.03236   0.0302   0.0931   1.0000
  11.750   0.8792   0.04225   0.03378   0.0306   0.0895   1.0000
  12.000   0.8899   0.04371   0.03524   0.0309   0.0864   1.0000
  12.250   0.9010   0.04515   0.03662   0.0313   0.0838   1.0000
  12.500   0.9146   0.04646   0.03800   0.0317   0.0812   1.0000
  12.750   0.9274   0.04787   0.03949   0.0320   0.0785   1.0000
  13.000   0.9400   0.04931   0.04098   0.0322   0.0761   1.0000
  13.250   0.9528   0.05075   0.04244   0.0324   0.0742   1.0000
  13.500   0.9673   0.05210   0.04377   0.0327   0.0724   1.0000
  13.750   0.9819   0.05357   0.04530   0.0330   0.0707   1.0000
  14.000   0.9923   0.05540   0.04731   0.0330   0.0690   1.0000
  14.250   1.0011   0.05738   0.04943   0.0330   0.0672   1.0000
  14.500   1.0099   0.05938   0.05153   0.0329   0.0656   1.0000
  14.750   1.0188   0.06141   0.05364   0.0327   0.0641   1.0000
  15.000   1.0284   0.06337   0.05564   0.0326   0.0627   1.0000
  15.250   1.0429   0.06499   0.05722   0.0326   0.0612   1.0000
  15.500   1.0428   0.06808   0.06053   0.0320   0.0601   1.0000
  15.750   1.0387   0.07165   0.06435   0.0310   0.0590   1.0000
  16.000   1.0338   0.07546   0.06839   0.0298   0.0579   1.0000
  16.250   1.0273   0.07958   0.07272   0.0283   0.0568   1.0000
  16.500   1.0200   0.08391   0.07724   0.0265   0.0557   1.0000
  16.750   1.0126   0.08840   0.08188   0.0245   0.0547   1.0000
  17.000   1.0082   0.09249   0.08608   0.0226   0.0536   1.0000
  17.250   1.0111   0.09555   0.08916   0.0212   0.0524   1.0000
  17.500   1.0095   0.09945   0.09310   0.0195   0.0514   1.0000
  17.750   0.9806   0.10806   0.10202   0.0146   0.0510   1.0000
  18.000   0.9414   0.11930   0.11357   0.0077   0.0509   1.0000
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