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NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il)
Reynolds number: 500,000
Max Cl/Cd: 64.62 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ms317-il-500000-n5.txt
Download as CSV file: xf-ms317-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0147   0.11643   0.11243  -0.0314   1.0000   0.0186
 -19.500  -1.0319   0.10935   0.10523  -0.0353   1.0000   0.0187
 -19.250  -1.0482   0.10253   0.09828  -0.0390   1.0000   0.0188
 -19.000  -1.0634   0.09597   0.09159  -0.0426   1.0000   0.0189
 -18.750  -1.0768   0.08985   0.08535  -0.0458   1.0000   0.0190
 -18.500  -1.0886   0.08409   0.07946  -0.0488   1.0000   0.0191
 -18.250  -1.0982   0.07877   0.07401  -0.0515   1.0000   0.0193
 -18.000  -1.1060   0.07388   0.06900  -0.0540   1.0000   0.0194
 -17.750  -1.1118   0.06941   0.06442  -0.0561   1.0000   0.0196
 -17.500  -1.1157   0.06531   0.06020  -0.0579   1.0000   0.0197
 -17.250  -1.1177   0.06160   0.05637  -0.0595   1.0000   0.0199
 -17.000  -1.1180   0.05825   0.05291  -0.0608   1.0000   0.0201
 -16.750  -1.1185   0.05498   0.04955  -0.0619   1.0000   0.0203
 -16.500  -1.1187   0.05185   0.04636  -0.0629   1.0000   0.0205
 -16.250  -1.1169   0.04909   0.04353  -0.0636   1.0000   0.0207
 -16.000  -1.1132   0.04661   0.04099  -0.0642   1.0000   0.0210
 -15.750  -1.1081   0.04438   0.03869  -0.0645   1.0000   0.0212
 -15.500  -1.1020   0.04234   0.03659  -0.0647   1.0000   0.0215
 -15.250  -1.0954   0.04044   0.03462  -0.0648   1.0000   0.0218
 -15.000  -1.0879   0.03864   0.03276  -0.0647   1.0000   0.0221
 -14.750  -1.0795   0.03698   0.03103  -0.0646   1.0000   0.0224
 -14.500  -1.0704   0.03541   0.02939  -0.0644   1.0000   0.0227
 -14.250  -1.0602   0.03397   0.02788  -0.0641   1.0000   0.0230
 -14.000  -1.0491   0.03262   0.02646  -0.0638   1.0000   0.0233
 -13.750  -1.0391   0.03122   0.02502  -0.0633   1.0000   0.0237
 -13.500  -1.0290   0.02987   0.02363  -0.0629   1.0000   0.0240
 -13.250  -1.0175   0.02866   0.02241  -0.0623   1.0000   0.0244
 -13.000  -1.0049   0.02759   0.02131  -0.0617   1.0000   0.0249
 -12.750  -0.9919   0.02661   0.02029  -0.0610   1.0000   0.0254
 -12.500  -0.9793   0.02570   0.01934  -0.0601   1.0000   0.0259
 -12.250  -0.9574   0.02475   0.01834  -0.0609   0.9878   0.0265
 -12.000  -0.9330   0.02385   0.01738  -0.0621   0.9737   0.0271
 -11.750  -0.9116   0.02280   0.01630  -0.0628   0.9579   0.0278
 -11.500  -0.8917   0.02195   0.01541  -0.0629   0.9421   0.0284
 -11.250  -0.8738   0.02119   0.01459  -0.0624   0.9278   0.0291
 -11.000  -0.8568   0.02051   0.01383  -0.0615   0.9148   0.0298
 -10.750  -0.8407   0.01989   0.01313  -0.0605   0.9024   0.0305
 -10.500  -0.8215   0.01925   0.01243  -0.0601   0.8921   0.0313
 -10.250  -0.8009   0.01862   0.01175  -0.0599   0.8820   0.0323
 -10.000  -0.7785   0.01807   0.01115  -0.0599   0.8737   0.0335
  -9.750  -0.7550   0.01757   0.01059  -0.0599   0.8654   0.0348
  -9.500  -0.7314   0.01707   0.01004  -0.0599   0.8580   0.0361
  -9.250  -0.7069   0.01660   0.00956  -0.0600   0.8507   0.0376
  -9.000  -0.6818   0.01620   0.00910  -0.0601   0.8440   0.0393
  -8.750  -0.6564   0.01578   0.00866  -0.0602   0.8380   0.0413
  -8.500  -0.6302   0.01539   0.00826  -0.0604   0.8321   0.0439
  -8.250  -0.6037   0.01502   0.00787  -0.0607   0.8265   0.0469
  -8.000  -0.5768   0.01469   0.00751  -0.0609   0.8215   0.0504
  -7.750  -0.5495   0.01433   0.00716  -0.0613   0.8168   0.0543
  -7.500  -0.5217   0.01400   0.00684  -0.0617   0.8119   0.0588
  -7.250  -0.4937   0.01371   0.00654  -0.0621   0.8070   0.0640
  -7.000  -0.4656   0.01341   0.00624  -0.0625   0.8023   0.0697
  -6.750  -0.4370   0.01312   0.00596  -0.0630   0.7979   0.0755
  -6.500  -0.4081   0.01285   0.00570  -0.0635   0.7932   0.0818
  -6.250  -0.3791   0.01259   0.00545  -0.0640   0.7886   0.0891
  -6.000  -0.3499   0.01232   0.00520  -0.0646   0.7845   0.0972
  -5.750  -0.3205   0.01207   0.00496  -0.0652   0.7805   0.1065
  -5.500  -0.2907   0.01179   0.00474  -0.0659   0.7763   0.1186
  -5.250  -0.2607   0.01151   0.00453  -0.0667   0.7720   0.1339
  -4.750  -0.2002   0.01091   0.00411  -0.0683   0.7640   0.1799
  -4.500  -0.1694   0.01055   0.00388  -0.0694   0.7603   0.2160
  -4.250  -0.1380   0.01015   0.00367  -0.0706   0.7564   0.2582
  -4.000  -0.1061   0.00974   0.00345  -0.0719   0.7525   0.3061
  -3.750  -0.0734   0.00927   0.00321  -0.0735   0.7489   0.3686
  -3.500  -0.0395   0.00871   0.00298  -0.0754   0.7454   0.4538
  -3.250  -0.0067   0.00842   0.00289  -0.0768   0.7422   0.5162
  -3.000   0.0252   0.00830   0.00289  -0.0777   0.7386   0.5535
  -2.750   0.0565   0.00825   0.00292  -0.0784   0.7346   0.5763
  -2.500   0.0876   0.00825   0.00294  -0.0789   0.7304   0.5932
  -2.250   0.1186   0.00828   0.00295  -0.0795   0.7265   0.6085
  -2.000   0.1494   0.00834   0.00300  -0.0800   0.7229   0.6230
  -1.750   0.1802   0.00837   0.00305  -0.0805   0.7192   0.6314
  -1.500   0.2111   0.00840   0.00309  -0.0811   0.7148   0.6392
  -1.250   0.2417   0.00845   0.00311  -0.0815   0.7086   0.6472
  -1.000   0.2713   0.00852   0.00315  -0.0816   0.6952   0.6558
  -0.750   0.3013   0.00860   0.00312  -0.0819   0.6766   0.6634
  -0.500   0.3305   0.00865   0.00314  -0.0820   0.6621   0.6672
  -0.250   0.3604   0.00870   0.00315  -0.0824   0.6502   0.6698
   0.000   0.3904   0.00876   0.00317  -0.0827   0.6368   0.6724
   0.250   0.4201   0.00883   0.00317  -0.0830   0.6207   0.6750
   0.500   0.4497   0.00892   0.00318  -0.0833   0.6028   0.6776
   0.750   0.4792   0.00904   0.00320  -0.0837   0.5834   0.6801
   1.000   0.5085   0.00918   0.00323  -0.0840   0.5609   0.6821
   1.250   0.5362   0.00939   0.00331  -0.0839   0.5264   0.6840
   1.500   0.5618   0.00980   0.00347  -0.0836   0.4691   0.6860
   1.750   0.5860   0.01038   0.00373  -0.0831   0.4034   0.6881
   2.000   0.6109   0.01090   0.00400  -0.0828   0.3507   0.6901
   2.250   0.6366   0.01134   0.00423  -0.0826   0.3083   0.6921
   2.500   0.6626   0.01176   0.00447  -0.0825   0.2734   0.6942
   2.750   0.6888   0.01213   0.00469  -0.0824   0.2444   0.6965
   3.000   0.7151   0.01249   0.00491  -0.0823   0.2202   0.6987
   3.250   0.7416   0.01282   0.00513  -0.0822   0.2002   0.7008
   3.500   0.7679   0.01313   0.00535  -0.0820   0.1839   0.7028
   3.750   0.7940   0.01341   0.00557  -0.0819   0.1711   0.7045
   4.000   0.8202   0.01369   0.00581  -0.0817   0.1606   0.7062
   4.250   0.8466   0.01395   0.00604  -0.0815   0.1525   0.7080
   4.500   0.8723   0.01425   0.00629  -0.0813   0.1447   0.7099
   4.750   0.8985   0.01450   0.00653  -0.0811   0.1387   0.7120
   5.000   0.9241   0.01479   0.00679  -0.0808   0.1327   0.7142
   5.250   0.9496   0.01508   0.00705  -0.0805   0.1279   0.7163
   5.500   0.9750   0.01536   0.00732  -0.0802   0.1233   0.7182
   5.750   0.9995   0.01569   0.00762  -0.0798   0.1188   0.7199
   6.000   1.0243   0.01599   0.00791  -0.0794   0.1156   0.7216
   6.250   1.0486   0.01627   0.00821  -0.0789   0.1128   0.7234
   6.500   1.0721   0.01659   0.00854  -0.0783   0.1100   0.7253
   6.750   1.0947   0.01695   0.00890  -0.0775   0.1075   0.7274
   7.000   1.1168   0.01733   0.00929  -0.0767   0.1053   0.7297
   7.250   1.1393   0.01765   0.00965  -0.0759   0.1038   0.7319
   7.500   1.1609   0.01800   0.01004  -0.0750   0.1022   0.7341
   7.750   1.1812   0.01839   0.01044  -0.0738   0.1004   0.7363
   8.000   1.1981   0.01879   0.01086  -0.0721   0.0988   0.7386
   8.250   1.2151   0.01927   0.01133  -0.0705   0.0972   0.7409
   8.500   1.2325   0.01981   0.01191  -0.0690   0.0957   0.7432
   8.750   1.2507   0.02034   0.01249  -0.0677   0.0946   0.7454
   9.000   1.2697   0.02084   0.01305  -0.0666   0.0937   0.7476
   9.250   1.2883   0.02139   0.01365  -0.0655   0.0928   0.7500
   9.500   1.3066   0.02196   0.01427  -0.0644   0.0917   0.7524
   9.750   1.3244   0.02258   0.01493  -0.0634   0.0905   0.7550
  10.000   1.3418   0.02325   0.01563  -0.0623   0.0894   0.7576
  10.250   1.3586   0.02397   0.01638  -0.0612   0.0884   0.7603
  10.500   1.3744   0.02475   0.01721  -0.0600   0.0874   0.7630
  10.750   1.3890   0.02563   0.01812  -0.0588   0.0862   0.7656
  11.000   1.4034   0.02655   0.01909  -0.0576   0.0852   0.7684
  11.250   1.4208   0.02728   0.01990  -0.0567   0.0843   0.7713
  11.500   1.4375   0.02806   0.02075  -0.0558   0.0831   0.7743
  11.750   1.4537   0.02889   0.02164  -0.0550   0.0819   0.7773
  12.000   1.4690   0.02981   0.02260  -0.0541   0.0808   0.7801
  12.250   1.4834   0.03078   0.02363  -0.0531   0.0798   0.7830
  12.500   1.4967   0.03185   0.02475  -0.0522   0.0788   0.7862
  12.750   1.5090   0.03301   0.02597  -0.0511   0.0779   0.7896
  13.000   1.5197   0.03433   0.02733  -0.0501   0.0770   0.7934
  13.250   1.5320   0.03554   0.02861  -0.0492   0.0763   0.7972
  13.500   1.5455   0.03665   0.02982  -0.0484   0.0755   0.8008
  13.750   1.5582   0.03782   0.03109  -0.0475   0.0746   0.8048
  14.000   1.5702   0.03908   0.03243  -0.0467   0.0737   0.8089
  14.250   1.5817   0.04039   0.03383  -0.0460   0.0728   0.8131
  14.750   1.6019   0.04332   0.03690  -0.0445   0.0710   0.8211
  15.000   1.6104   0.04496   0.03860  -0.0438   0.0702   0.8257
  15.250   1.6174   0.04678   0.04048  -0.0431   0.0694   0.8305
  15.750   1.6337   0.05030   0.04420  -0.0419   0.0677   0.8400
  16.000   1.6428   0.05202   0.04603  -0.0415   0.0668   0.8454
  16.250   1.6506   0.05391   0.04802  -0.0411   0.0657   0.8510
  16.500   1.6575   0.05588   0.05008  -0.0408   0.0647   0.8567
  16.750   1.6631   0.05805   0.05235  -0.0405   0.0638   0.8635
  17.000   1.6676   0.06039   0.05477  -0.0403   0.0629   0.8703
  17.250   1.6703   0.06295   0.05741  -0.0402   0.0621   0.8781
  17.500   1.6724   0.06563   0.06019  -0.0401   0.0612   0.8864
  17.750   1.6763   0.06807   0.06277  -0.0401   0.0604   0.8965
  18.000   1.6788   0.07063   0.06546  -0.0400   0.0594   0.9088
  18.500   1.6756   0.07630   0.07138  -0.0396   0.0575   1.0000
  18.750   1.6748   0.07971   0.07486  -0.0403   0.0565   1.0000
  19.000   1.6717   0.08348   0.07870  -0.0413   0.0556   1.0000
  19.250   1.6677   0.08739   0.08271  -0.0423   0.0547   1.0000
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