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NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il)
Reynolds number: 200,000
Max Cl/Cd: 47.7 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ms317-il-200000-n5.txt
Download as CSV file: xf-ms317-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA/LANGLEY MS(1)-0317 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.8667   0.10357   0.09843  -0.0443   1.0000   0.0279
 -17.250  -0.8970   0.09361   0.08822  -0.0504   1.0000   0.0280
 -17.000  -0.9154   0.08637   0.08079  -0.0547   1.0000   0.0281
 -16.750  -0.9287   0.08034   0.07460  -0.0581   1.0000   0.0283
 -16.500  -0.9389   0.07508   0.06918  -0.0609   1.0000   0.0285
 -16.250  -0.9470   0.07038   0.06433  -0.0633   1.0000   0.0288
 -16.000  -0.9534   0.06615   0.05996  -0.0652   1.0000   0.0291
 -15.750  -0.9583   0.06230   0.05595  -0.0667   1.0000   0.0294
 -15.500  -0.9619   0.05879   0.05227  -0.0678   1.0000   0.0298
 -15.250  -0.9644   0.05558   0.04889  -0.0686   1.0000   0.0303
 -15.000  -0.9657   0.05263   0.04574  -0.0692   1.0000   0.0307
 -14.750  -0.9639   0.05012   0.04309  -0.0694   1.0000   0.0311
 -14.500  -0.9580   0.04812   0.04108  -0.0694   1.0000   0.0315
 -14.250  -0.9520   0.04619   0.03910  -0.0694   1.0000   0.0319
 -14.000  -0.9455   0.04434   0.03720  -0.0693   1.0000   0.0324
 -13.750  -0.9382   0.04257   0.03536  -0.0690   1.0000   0.0329
 -13.500  -0.9304   0.04088   0.03358  -0.0687   1.0000   0.0334
 -13.250  -0.9216   0.03929   0.03189  -0.0682   1.0000   0.0340
 -13.000  -0.9122   0.03779   0.03028  -0.0676   1.0000   0.0347
 -12.750  -0.9023   0.03639   0.02879  -0.0669   1.0000   0.0354
 -12.500  -0.8927   0.03510   0.02751  -0.0662   1.0000   0.0360
 -12.250  -0.8826   0.03392   0.02631  -0.0654   1.0000   0.0368
 -12.000  -0.8728   0.03282   0.02517  -0.0643   1.0000   0.0376
 -11.750  -0.8639   0.03180   0.02411  -0.0629   1.0000   0.0385
 -11.500  -0.8575   0.03089   0.02315  -0.0609   1.0000   0.0394
 -11.250  -0.8538   0.03007   0.02230  -0.0584   0.9988   0.0401
 -11.000  -0.8290   0.02888   0.02111  -0.0601   0.9912   0.0412
 -10.750  -0.8039   0.02782   0.02001  -0.0615   0.9824   0.0426
 -10.500  -0.7789   0.02683   0.01895  -0.0627   0.9732   0.0443
 -10.250  -0.7539   0.02582   0.01791  -0.0639   0.9646   0.0460
 -10.000  -0.7308   0.02494   0.01700  -0.0646   0.9547   0.0478
  -9.750  -0.7074   0.02412   0.01612  -0.0651   0.9458   0.0500
  -9.500  -0.6839   0.02327   0.01525  -0.0657   0.9371   0.0520
  -9.250  -0.6610   0.02255   0.01449  -0.0659   0.9282   0.0546
  -9.000  -0.6379   0.02185   0.01374  -0.0661   0.9198   0.0576
  -8.750  -0.6152   0.02120   0.01308  -0.0661   0.9119   0.0609
  -8.500  -0.5926   0.02061   0.01245  -0.0660   0.9038   0.0646
  -8.250  -0.5689   0.02004   0.01185  -0.0660   0.8973   0.0690
  -8.000  -0.5462   0.01952   0.01133  -0.0658   0.8892   0.0738
  -7.750  -0.5218   0.01905   0.01081  -0.0657   0.8827   0.0795
  -7.500  -0.4976   0.01853   0.01030  -0.0657   0.8769   0.0855
  -7.250  -0.4731   0.01808   0.00985  -0.0657   0.8699   0.0923
  -7.000  -0.4476   0.01766   0.00941  -0.0657   0.8641   0.1002
  -6.750  -0.4218   0.01721   0.00897  -0.0659   0.8595   0.1094
  -6.500  -0.3958   0.01678   0.00859  -0.0661   0.8538   0.1203
  -6.250  -0.3693   0.01636   0.00821  -0.0664   0.8484   0.1338
  -6.000  -0.3424   0.01594   0.00784  -0.0668   0.8436   0.1514
  -5.750  -0.3151   0.01546   0.00745  -0.0673   0.8394   0.1749
  -5.500  -0.2876   0.01499   0.00712  -0.0679   0.8337   0.2050
  -5.250  -0.2595   0.01444   0.00677  -0.0687   0.8286   0.2437
  -5.000  -0.2306   0.01387   0.00639  -0.0697   0.8243   0.2932
  -4.750  -0.2008   0.01319   0.00600  -0.0710   0.8206   0.3605
  -4.500  -0.1708   0.01255   0.00583  -0.0722   0.8157   0.4533
  -4.250  -0.1418   0.01237   0.00596  -0.0725   0.8108   0.5229
  -4.000  -0.1127   0.01242   0.00612  -0.0725   0.8065   0.5625
  -3.750  -0.0829   0.01250   0.00618  -0.0727   0.8027   0.5879
  -3.500  -0.0527   0.01259   0.00623  -0.0730   0.7987   0.6063
  -3.250  -0.0232   0.01272   0.00636  -0.0731   0.7938   0.6202
  -3.000   0.0063   0.01286   0.00649  -0.0733   0.7895   0.6332
  -2.750   0.0367   0.01300   0.00656  -0.0736   0.7857   0.6465
  -2.500   0.0656   0.01319   0.00672  -0.0734   0.7823   0.6556
  -2.250   0.0965   0.01327   0.00674  -0.0741   0.7783   0.6644
  -2.000   0.1239   0.01348   0.00699  -0.0736   0.7734   0.6708
  -1.750   0.1549   0.01363   0.00708  -0.0742   0.7689   0.6823
  -1.500   0.1808   0.01389   0.00739  -0.0731   0.7649   0.6882
  -1.250   0.2100   0.01401   0.00745  -0.0731   0.7615   0.6934
  -1.000   0.2407   0.01401   0.00745  -0.0738   0.7567   0.6976
  -0.750   0.2728   0.01397   0.00736  -0.0750   0.7518   0.7018
  -0.500   0.3012   0.01400   0.00739  -0.0749   0.7470   0.7039
  -0.250   0.3302   0.01400   0.00734  -0.0748   0.7413   0.7062
   0.000   0.3579   0.01391   0.00725  -0.0746   0.7276   0.7087
   0.250   0.3862   0.01380   0.00708  -0.0743   0.7112   0.7115
   0.500   0.4154   0.01373   0.00694  -0.0744   0.6970   0.7147
   0.750   0.4458   0.01367   0.00682  -0.0750   0.6864   0.7178
   1.000   0.4769   0.01362   0.00673  -0.0758   0.6743   0.7212
   1.250   0.5048   0.01362   0.00671  -0.0755   0.6622   0.7231
   1.500   0.5325   0.01363   0.00670  -0.0753   0.6481   0.7251
   1.750   0.5605   0.01365   0.00671  -0.0752   0.6316   0.7271
   2.000   0.5884   0.01369   0.00670  -0.0752   0.6126   0.7294
   2.250   0.6162   0.01376   0.00670  -0.0751   0.5900   0.7320
   2.500   0.6437   0.01387   0.00670  -0.0750   0.5599   0.7349
   2.750   0.6700   0.01409   0.00671  -0.0748   0.5172   0.7378
   3.000   0.6936   0.01454   0.00679  -0.0742   0.4530   0.7408
   3.250   0.7120   0.01521   0.00711  -0.0727   0.3895   0.7428
   3.500   0.7311   0.01587   0.00750  -0.0713   0.3364   0.7447
   3.750   0.7513   0.01648   0.00789  -0.0703   0.2945   0.7467
   4.000   0.7727   0.01702   0.00826  -0.0694   0.2619   0.7488
   4.250   0.7950   0.01751   0.00862  -0.0687   0.2370   0.7512
   4.500   0.8177   0.01798   0.00898  -0.0681   0.2169   0.7540
   4.750   0.8407   0.01844   0.00934  -0.0676   0.2007   0.7569
   5.000   0.8640   0.01890   0.00971  -0.0673   0.1872   0.7596
   5.250   0.8860   0.01933   0.01010  -0.0665   0.1760   0.7616
   5.500   0.9073   0.01975   0.01050  -0.0656   0.1672   0.7634
   5.750   0.9275   0.02022   0.01095  -0.0645   0.1597   0.7654
   6.000   0.9486   0.02064   0.01139  -0.0636   0.1538   0.7678
   6.250   0.9688   0.02111   0.01185  -0.0626   0.1483   0.7705
   6.500   0.9873   0.02167   0.01238  -0.0613   0.1438   0.7734
   6.750   1.0071   0.02210   0.01285  -0.0603   0.1400   0.7763
   7.000   1.0251   0.02259   0.01335  -0.0590   0.1362   0.7791
   7.250   1.0414   0.02315   0.01391  -0.0574   0.1328   0.7812
   7.500   1.0571   0.02384   0.01459  -0.0558   0.1298   0.7835
   7.750   1.0761   0.02438   0.01521  -0.0548   0.1272   0.7862
   8.000   1.0947   0.02499   0.01587  -0.0537   0.1246   0.7892
   8.250   1.1130   0.02565   0.01658  -0.0528   0.1223   0.7921
   8.500   1.1309   0.02638   0.01731  -0.0518   0.1202   0.7950
   8.750   1.1481   0.02721   0.01812  -0.0509   0.1183   0.7980
   9.000   1.1648   0.02799   0.01894  -0.0498   0.1166   0.8003
   9.250   1.1826   0.02869   0.01973  -0.0488   0.1149   0.8029
   9.500   1.1999   0.02943   0.02055  -0.0478   0.1130   0.8060
   9.750   1.2171   0.03022   0.02140  -0.0469   0.1113   0.8094
  10.000   1.2343   0.03105   0.02228  -0.0461   0.1098   0.8130
  10.250   1.2513   0.03195   0.02320  -0.0453   0.1084   0.8163
  10.500   1.2666   0.03287   0.02415  -0.0443   0.1070   0.8190
  10.750   1.2818   0.03387   0.02515  -0.0432   0.1057   0.8220
  11.000   1.2984   0.03474   0.02614  -0.0423   0.1044   0.8253
  11.250   1.3148   0.03566   0.02717  -0.0415   0.1031   0.8290
  11.500   1.3310   0.03664   0.02824  -0.0408   0.1017   0.8328
  11.750   1.3460   0.03764   0.02933  -0.0399   0.1004   0.8364
  12.000   1.3598   0.03868   0.03044  -0.0389   0.0991   0.8402
  12.250   1.3733   0.03977   0.03160  -0.0381   0.0978   0.8447
  12.500   1.3868   0.04093   0.03281  -0.0373   0.0966   0.8494
  12.750   1.4004   0.04211   0.03399  -0.0364   0.0954   0.8536
  13.000   1.4123   0.04333   0.03534  -0.0354   0.0942   0.8579
  13.250   1.4233   0.04466   0.03682  -0.0346   0.0929   0.8628
  13.500   1.4344   0.04606   0.03835  -0.0338   0.0916   0.8681
  13.750   1.4436   0.04745   0.03987  -0.0329   0.0903   0.8730
  14.000   1.4528   0.04891   0.04143  -0.0320   0.0890   0.8788
  14.500   1.4692   0.05198   0.04465  -0.0304   0.0869   0.8917
  14.750   1.4776   0.05355   0.04625  -0.0296   0.0859   0.8998
  15.000   1.4833   0.05526   0.04809  -0.0286   0.0849   0.9093
  15.250   1.4860   0.05724   0.05029  -0.0277   0.0838   0.9219
  15.500   1.4871   0.05918   0.05241  -0.0265   0.0828   0.9450
  15.750   1.4884   0.06130   0.05469  -0.0259   0.0817   1.0000
  16.000   1.4931   0.06373   0.05724  -0.0261   0.0806   1.0000
  16.250   1.4975   0.06621   0.05981  -0.0264   0.0796   1.0000
  16.500   1.5015   0.06875   0.06243  -0.0267   0.0786   1.0000
  16.750   1.5053   0.07136   0.06509  -0.0271   0.0777   1.0000
  17.000   1.5104   0.07377   0.06751  -0.0274   0.0768   1.0000
  17.250   1.5065   0.07750   0.07145  -0.0282   0.0758   1.0000
  17.500   1.5009   0.08157   0.07574  -0.0293   0.0748   1.0000
  17.750   1.4951   0.08577   0.08013  -0.0305   0.0737   1.0000
  18.000   1.4893   0.09007   0.08459  -0.0320   0.0727   1.0000
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