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NASA/LANGLEY MS(1)-0313 AIRFOIL (ms313-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NASA/LANGLEY MS(1)-0313 AIRFOIL (ms313-il)
Reynolds number: 200,000
Max Cl/Cd: 50.52 at α=2.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ms313-il-200000-n5.txt
Download as CSV file: xf-ms313-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA/LANGLEY MS(1)-0313 AIRFOIL                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.6087   0.09535   0.09140  -0.0372   1.0000   0.0200
 -12.500  -0.7152   0.06510   0.06075  -0.0588   1.0000   0.0192
 -12.250  -0.7479   0.05714   0.05252  -0.0638   1.0000   0.0192
 -12.000  -0.7733   0.05136   0.04646  -0.0661   1.0000   0.0192
 -11.750  -0.7934   0.04693   0.04177  -0.0665   1.0000   0.0193
 -11.500  -0.8110   0.04356   0.03814  -0.0652   1.0000   0.0194
 -11.250  -0.8247   0.04070   0.03501  -0.0630   1.0000   0.0197
 -11.000  -0.8346   0.03816   0.03213  -0.0600   1.0000   0.0200
 -10.750  -0.8417   0.03610   0.02975  -0.0565   1.0000   0.0204
 -10.500  -0.8222   0.03465   0.02824  -0.0572   0.9965   0.0208
 -10.250  -0.7962   0.03325   0.02673  -0.0589   0.9924   0.0214
 -10.000  -0.7707   0.03162   0.02491  -0.0603   0.9877   0.0220
  -9.750  -0.7434   0.02978   0.02282  -0.0619   0.9841   0.0227
  -9.500  -0.7163   0.02801   0.02078  -0.0631   0.9800   0.0235
  -9.250  -0.6892   0.02643   0.01892  -0.0640   0.9754   0.0243
  -9.000  -0.6603   0.02514   0.01754  -0.0653   0.9719   0.0250
  -8.750  -0.6307   0.02427   0.01664  -0.0666   0.9682   0.0260
  -8.500  -0.6030   0.02343   0.01570  -0.0673   0.9629   0.0273
  -8.250  -0.5733   0.02246   0.01458  -0.0682   0.9587   0.0286
  -8.000  -0.5432   0.02143   0.01348  -0.0693   0.9555   0.0297
  -7.750  -0.5169   0.02068   0.01272  -0.0697   0.9499   0.0308
  -7.500  -0.4887   0.01998   0.01199  -0.0703   0.9452   0.0324
  -7.250  -0.4590   0.01933   0.01122  -0.0710   0.9415   0.0345
  -7.000  -0.4317   0.01861   0.01052  -0.0716   0.9368   0.0364
  -6.750  -0.4048   0.01803   0.00992  -0.0718   0.9312   0.0385
  -6.500  -0.3763   0.01748   0.00929  -0.0723   0.9269   0.0410
  -6.250  -0.3474   0.01687   0.00870  -0.0730   0.9235   0.0442
  -6.000  -0.3207   0.01645   0.00824  -0.0731   0.9181   0.0480
  -5.750  -0.2930   0.01593   0.00773  -0.0736   0.9133   0.0522
  -5.500  -0.2641   0.01553   0.00728  -0.0740   0.9093   0.0581
  -5.250  -0.2355   0.01507   0.00686  -0.0745   0.9055   0.0661
  -5.000  -0.2076   0.01467   0.00650  -0.0749   0.9006   0.0773
  -4.750  -0.1789   0.01426   0.00614  -0.0755   0.8964   0.0947
  -4.500  -0.1498   0.01375   0.00579  -0.0762   0.8927   0.1278
  -4.250  -0.1205   0.01310   0.00544  -0.0771   0.8893   0.1951
  -4.000  -0.0911   0.01233   0.00512  -0.0784   0.8847   0.3014
  -3.750  -0.0608   0.01142   0.00491  -0.0799   0.8809   0.4576
  -3.500  -0.0322   0.01118   0.00503  -0.0800   0.8772   0.5569
  -3.250  -0.0036   0.01119   0.00514  -0.0799   0.8741   0.6026
  -3.000   0.0250   0.01129   0.00525  -0.0799   0.8698   0.6307
  -2.750   0.0535   0.01141   0.00537  -0.0798   0.8655   0.6538
  -2.500   0.0817   0.01157   0.00553  -0.0795   0.8615   0.6773
  -2.250   0.1103   0.01171   0.00563  -0.0793   0.8582   0.6930
  -2.000   0.1381   0.01181   0.00573  -0.0790   0.8545   0.7002
  -1.750   0.1670   0.01191   0.00580  -0.0792   0.8498   0.7105
  -1.500   0.1943   0.01203   0.00593  -0.0787   0.8456   0.7188
  -1.250   0.2246   0.01205   0.00588  -0.0792   0.8421   0.7262
  -1.000   0.2528   0.01208   0.00592  -0.0791   0.8381   0.7295
  -0.750   0.2810   0.01212   0.00595  -0.0791   0.8322   0.7333
  -0.500   0.3098   0.01202   0.00580  -0.0789   0.8243   0.7377
  -0.250   0.3378   0.01185   0.00553  -0.0785   0.8083   0.7423
   0.000   0.3642   0.01170   0.00531  -0.0776   0.7902   0.7453
   0.250   0.3914   0.01164   0.00522  -0.0771   0.7752   0.7486
   0.500   0.4196   0.01161   0.00518  -0.0770   0.7621   0.7523
   0.750   0.4485   0.01159   0.00513  -0.0771   0.7487   0.7564
   1.000   0.4774   0.01157   0.00507  -0.0772   0.7339   0.7603
   1.250   0.5047   0.01156   0.00505  -0.0768   0.7166   0.7631
   1.500   0.5321   0.01157   0.00502  -0.0765   0.6949   0.7664
   1.750   0.5596   0.01161   0.00499  -0.0762   0.6657   0.7702
   2.000   0.5868   0.01172   0.00492  -0.0759   0.6192   0.7742
   2.250   0.6103   0.01208   0.00489  -0.0749   0.5412   0.7775
   2.500   0.6300   0.01279   0.00510  -0.0733   0.4506   0.7807
   2.750   0.6507   0.01351   0.00544  -0.0722   0.3745   0.7842
   3.000   0.6732   0.01415   0.00577  -0.0716   0.3151   0.7881
   3.250   0.6973   0.01472   0.00608  -0.0713   0.2692   0.7923
   3.500   0.7206   0.01518   0.00639  -0.0706   0.2370   0.7953
   3.750   0.7446   0.01559   0.00670  -0.0701   0.2129   0.7987
   4.000   0.7692   0.01600   0.00702  -0.0697   0.1940   0.8024
   4.250   0.7943   0.01640   0.00734  -0.0694   0.1786   0.8066
   4.500   0.8189   0.01678   0.00768  -0.0690   0.1663   0.8103
   4.750   0.8424   0.01717   0.00803  -0.0684   0.1565   0.8136
   5.000   0.8668   0.01752   0.00839  -0.0679   0.1485   0.8174
   5.250   0.8908   0.01796   0.00879  -0.0675   0.1421   0.8218
   5.500   0.9154   0.01831   0.00919  -0.0671   0.1366   0.8260
   5.750   0.9382   0.01872   0.00960  -0.0663   0.1317   0.8296
   6.000   0.9607   0.01920   0.01007  -0.0656   0.1274   0.8336
   6.250   0.9849   0.01958   0.01051  -0.0651   0.1234   0.8383
   6.500   1.0079   0.02000   0.01097  -0.0644   0.1197   0.8427
   6.750   1.0293   0.02048   0.01147  -0.0635   0.1166   0.8471
   7.000   1.0504   0.02107   0.01205  -0.0626   0.1139   0.8519
   7.250   1.0737   0.02153   0.01259  -0.0620   0.1117   0.8569
   7.500   1.0948   0.02198   0.01314  -0.0609   0.1093   0.8616
   7.750   1.1162   0.02247   0.01370  -0.0600   0.1069   0.8673
   8.000   1.1373   0.02299   0.01427  -0.0592   0.1045   0.8732
   8.250   1.1563   0.02357   0.01487  -0.0579   0.1023   0.8790
   8.500   1.1759   0.02431   0.01562  -0.0568   0.1004   0.8855
   8.750   1.1958   0.02482   0.01626  -0.0557   0.0990   0.8923
   9.000   1.2153   0.02537   0.01693  -0.0545   0.0971   0.9008
   9.250   1.2328   0.02589   0.01756  -0.0529   0.0952   0.9107
   9.500   1.2482   0.02640   0.01817  -0.0510   0.0933   0.9236
   9.750   1.2621   0.02688   0.01874  -0.0489   0.0915   0.9450
  10.000   1.2774   0.02751   0.01940  -0.0473   0.0896   1.0000
  10.250   1.2971   0.02843   0.02034  -0.0467   0.0876   1.0000
  10.500   1.3167   0.02916   0.02123  -0.0460   0.0857   1.0000
  10.750   1.3352   0.02996   0.02214  -0.0452   0.0837   1.0000
  11.000   1.3525   0.03078   0.02306  -0.0443   0.0818   1.0000
  11.250   1.3686   0.03162   0.02397  -0.0433   0.0800   1.0000
  11.500   1.3836   0.03255   0.02496  -0.0422   0.0783   1.0000
  11.750   1.3980   0.03371   0.02610  -0.0412   0.0765   1.0000
  12.000   1.4124   0.03469   0.02729  -0.0401   0.0749   1.0000
  12.250   1.4259   0.03576   0.02852  -0.0389   0.0730   1.0000
  12.500   1.4382   0.03688   0.02977  -0.0378   0.0711   1.0000
  12.750   1.4495   0.03803   0.03103  -0.0367   0.0693   1.0000
  13.000   1.4595   0.03928   0.03235  -0.0355   0.0678   1.0000
  13.250   1.4678   0.04076   0.03384  -0.0344   0.0662   1.0000
  13.500   1.4770   0.04226   0.03557  -0.0333   0.0646   1.0000
  13.750   1.4851   0.04386   0.03736  -0.0323   0.0627   1.0000
  14.000   1.4920   0.04553   0.03917  -0.0314   0.0609   1.0000
  14.250   1.4978   0.04730   0.04105  -0.0306   0.0593   1.0000
  14.500   1.5020   0.04925   0.04309  -0.0298   0.0579   1.0000
  14.750   1.5044   0.05150   0.04543  -0.0291   0.0566   1.0000
  15.000   1.5065   0.05394   0.04811  -0.0286   0.0549   1.0000
  15.250   1.5072   0.05656   0.05090  -0.0282   0.0533   1.0000
  15.500   1.5068   0.05935   0.05384  -0.0281   0.0518   1.0000
  15.750   1.5051   0.06237   0.05698  -0.0282   0.0505   1.0000
  16.000   1.5013   0.06577   0.06047  -0.0287   0.0494   1.0000
  16.250   1.4952   0.06971   0.06455  -0.0294   0.0484   1.0000
  16.500   1.4870   0.07421   0.06928  -0.0305   0.0472   1.0000
  16.750   1.4768   0.07921   0.07450  -0.0321   0.0461   1.0000
  17.000   1.4643   0.08482   0.08030  -0.0344   0.0451   1.0000
  17.250   1.4496   0.09111   0.08677  -0.0374   0.0442   1.0000
  17.500   1.4319   0.09822   0.09404  -0.0410   0.0435   1.0000
  17.750   1.4107   0.10622   0.10220  -0.0454   0.0430   1.0000
  18.000   1.3856   0.11527   0.11142  -0.0506   0.0425   1.0000
  18.250   1.3564   0.12543   0.12173  -0.0567   0.0421   1.0000
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