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NASA/LANGLEY MS(1)-0313 AIRFOIL (ms313-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NASA/LANGLEY MS(1)-0313 AIRFOIL (ms313-il)
Reynolds number: 1,000,000
Max Cl/Cd: 85.33 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ms313-il-1000000.txt
Download as CSV file: xf-ms313-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.9908   0.07431   0.07164  -0.0457   1.0000   0.0116
 -16.000  -1.0236   0.06412   0.06122  -0.0526   1.0000   0.0116
 -15.750  -1.0427   0.05737   0.05428  -0.0568   1.0000   0.0116
 -15.500  -1.0554   0.05213   0.04890  -0.0597   1.0000   0.0116
 -15.250  -1.0635   0.04786   0.04450  -0.0618   1.0000   0.0116
 -15.000  -1.0687   0.04423   0.04075  -0.0633   1.0000   0.0117
 -14.750  -1.0703   0.04117   0.03757  -0.0643   1.0000   0.0118
 -14.500  -1.0702   0.03846   0.03475  -0.0649   1.0000   0.0119
 -14.250  -1.0677   0.03609   0.03228  -0.0653   1.0000   0.0120
 -14.000  -1.0638   0.03395   0.03003  -0.0654   1.0000   0.0121
 -13.750  -1.0584   0.03203   0.02801  -0.0653   1.0000   0.0122
 -13.500  -1.0520   0.03028   0.02615  -0.0650   1.0000   0.0123
 -13.250  -1.0449   0.02871   0.02447  -0.0644   1.0000   0.0125
 -13.000  -1.0386   0.02730   0.02297  -0.0633   1.0000   0.0126
 -12.750  -1.0300   0.02603   0.02160  -0.0624   1.0000   0.0128
 -12.500  -1.0175   0.02491   0.02039  -0.0616   1.0000   0.0130
 -12.250  -1.0072   0.02401   0.01941  -0.0598   1.0000   0.0131
 -12.000  -0.9872   0.02310   0.01841  -0.0598   0.9983   0.0133
 -11.750  -0.9569   0.02231   0.01752  -0.0615   0.9957   0.0136
 -11.500  -0.9310   0.02059   0.01566  -0.0631   0.9928   0.0140
 -11.250  -0.9040   0.01946   0.01447  -0.0644   0.9878   0.0144
 -11.000  -0.8737   0.01870   0.01367  -0.0659   0.9838   0.0147
 -10.750  -0.8456   0.01805   0.01297  -0.0667   0.9772   0.0150
 -10.500  -0.8177   0.01742   0.01229  -0.0674   0.9706   0.0154
 -10.250  -0.7929   0.01686   0.01166  -0.0674   0.9620   0.0158
 -10.000  -0.7682   0.01633   0.01106  -0.0673   0.9544   0.0162
  -9.750  -0.7434   0.01586   0.01052  -0.0671   0.9465   0.0166
  -9.500  -0.7190   0.01534   0.00991  -0.0668   0.9395   0.0169
  -9.250  -0.6951   0.01445   0.00898  -0.0668   0.9324   0.0176
  -9.000  -0.6693   0.01405   0.00853  -0.0667   0.9259   0.0182
  -8.750  -0.6426   0.01368   0.00813  -0.0668   0.9202   0.0188
  -8.500  -0.6154   0.01332   0.00773  -0.0669   0.9144   0.0195
  -8.250  -0.5883   0.01299   0.00734  -0.0670   0.9091   0.0201
  -8.000  -0.5610   0.01250   0.00679  -0.0673   0.9041   0.0209
  -7.750  -0.5332   0.01209   0.00638  -0.0676   0.8989   0.0220
  -7.500  -0.5052   0.01182   0.00608  -0.0678   0.8939   0.0230
  -7.250  -0.4769   0.01156   0.00578  -0.0681   0.8892   0.0240
  -7.000  -0.4481   0.01119   0.00536  -0.0685   0.8849   0.0250
  -6.750  -0.4194   0.01082   0.00500  -0.0689   0.8804   0.0266
  -6.500  -0.3905   0.01061   0.00476  -0.0693   0.8761   0.0282
  -6.250  -0.3614   0.01034   0.00445  -0.0697   0.8719   0.0301
  -6.000  -0.3319   0.01005   0.00418  -0.0702   0.8677   0.0326
  -5.750  -0.3024   0.00987   0.00398  -0.0706   0.8636   0.0346
  -5.500  -0.2729   0.00958   0.00369  -0.0712   0.8598   0.0387
  -5.250  -0.2433   0.00939   0.00348  -0.0716   0.8560   0.0428
  -5.000  -0.2133   0.00917   0.00330  -0.0722   0.8523   0.0483
  -4.750  -0.1832   0.00892   0.00310  -0.0728   0.8483   0.0570
  -4.500  -0.1531   0.00869   0.00291  -0.0734   0.8447   0.0710
  -4.250  -0.1229   0.00844   0.00274  -0.0741   0.8411   0.0946
  -4.000  -0.0922   0.00809   0.00257  -0.0750   0.8376   0.1369
  -3.750  -0.0607   0.00759   0.00237  -0.0762   0.8340   0.2121
  -3.500  -0.0287   0.00703   0.00217  -0.0777   0.8305   0.3118
  -3.250   0.0044   0.00633   0.00196  -0.0795   0.8272   0.4518
  -3.000   0.0362   0.00601   0.00189  -0.0806   0.8236   0.5389
  -2.750   0.0672   0.00587   0.00188  -0.0813   0.8203   0.5813
  -2.500   0.0978   0.00582   0.00188  -0.0818   0.8166   0.6058
  -2.250   0.1279   0.00580   0.00186  -0.0822   0.8115   0.6251
  -2.000   0.1575   0.00579   0.00184  -0.0824   0.8023   0.6397
  -1.750   0.1868   0.00579   0.00179  -0.0825   0.7890   0.6508
  -1.500   0.2164   0.00579   0.00177  -0.0827   0.7773   0.6636
  -1.250   0.2463   0.00585   0.00180  -0.0830   0.7695   0.6757
  -1.000   0.2760   0.00585   0.00181  -0.0832   0.7617   0.6819
  -0.750   0.3058   0.00588   0.00181  -0.0835   0.7533   0.6873
  -0.500   0.3356   0.00593   0.00181  -0.0838   0.7440   0.6932
  -0.250   0.3651   0.00595   0.00186  -0.0841   0.7359   0.7000
   0.000   0.3948   0.00601   0.00188  -0.0843   0.7266   0.7057
   0.250   0.4247   0.00606   0.00189  -0.0847   0.7149   0.7091
   0.500   0.4539   0.00608   0.00189  -0.0849   0.6994   0.7125
   0.750   0.4831   0.00615   0.00191  -0.0851   0.6808   0.7156
   1.000   0.5120   0.00627   0.00194  -0.0852   0.6556   0.7187
   1.250   0.5400   0.00650   0.00199  -0.0853   0.6103   0.7218
   1.500   0.5658   0.00704   0.00215  -0.0850   0.5226   0.7248
   1.750   0.5908   0.00768   0.00238  -0.0847   0.4304   0.7278
   2.000   0.6163   0.00823   0.00261  -0.0845   0.3551   0.7307
   2.250   0.6425   0.00869   0.00282  -0.0844   0.2977   0.7336
   2.750   0.6961   0.00944   0.00320  -0.0843   0.2201   0.7397
   3.000   0.7235   0.00973   0.00337  -0.0844   0.1952   0.7423
   3.250   0.7507   0.00999   0.00354  -0.0843   0.1753   0.7455
   3.500   0.7779   0.01024   0.00372  -0.0843   0.1593   0.7485
   3.750   0.8053   0.01048   0.00390  -0.0843   0.1465   0.7514
   4.000   0.8327   0.01071   0.00409  -0.0843   0.1364   0.7545
   4.250   0.8599   0.01097   0.00429  -0.0843   0.1274   0.7575
   4.500   0.8875   0.01117   0.00447  -0.0843   0.1219   0.7604
   4.750   0.9141   0.01143   0.00470  -0.0842   0.1149   0.7636
   5.000   0.9415   0.01160   0.00491  -0.0841   0.1119   0.7666
   5.250   0.9686   0.01182   0.00512  -0.0840   0.1084   0.7699
   5.500   0.9952   0.01208   0.00535  -0.0839   0.1046   0.7731
   5.750   1.0213   0.01242   0.00567  -0.0837   0.1005   0.7760
   6.000   1.0483   0.01257   0.00587  -0.0836   0.0990   0.7795
   6.250   1.0749   0.01277   0.00611  -0.0834   0.0971   0.7828
   6.500   1.1011   0.01302   0.00637  -0.0832   0.0950   0.7861
   6.750   1.1269   0.01330   0.00665  -0.0830   0.0928   0.7895
   7.000   1.1520   0.01366   0.00700  -0.0826   0.0902   0.7928
   7.250   1.1759   0.01406   0.00745  -0.0820   0.0879   0.7965
   7.500   1.2020   0.01425   0.00769  -0.0818   0.0871   0.8001
   7.750   1.2279   0.01446   0.00792  -0.0816   0.0856   0.8038
   8.000   1.2534   0.01471   0.00820  -0.0813   0.0839   0.8074
   8.250   1.2782   0.01498   0.00849  -0.0808   0.0822   0.8112
   8.500   1.3022   0.01530   0.00883  -0.0803   0.0805   0.8153
   8.750   1.3248   0.01574   0.00930  -0.0795   0.0783   0.8195
   9.000   1.3464   0.01625   0.00985  -0.0786   0.0764   0.8237
   9.250   1.3708   0.01647   0.01012  -0.0782   0.0757   0.8279
   9.500   1.3948   0.01671   0.01042  -0.0776   0.0746   0.8324
   9.750   1.4182   0.01700   0.01075  -0.0770   0.0733   0.8373
  10.000   1.4411   0.01729   0.01108  -0.0763   0.0719   0.8423
  10.250   1.4630   0.01762   0.01144  -0.0755   0.0703   0.8475
  10.500   1.4833   0.01805   0.01190  -0.0744   0.0685   0.8532
  10.750   1.4989   0.01874   0.01264  -0.0725   0.0662   0.8590
  11.000   1.5205   0.01896   0.01293  -0.0716   0.0655   0.8654
  11.500   1.5578   0.01955   0.01366  -0.0688   0.0630   0.8813
  11.750   1.5761   0.01993   0.01410  -0.0674   0.0614   0.8909
  12.250   1.6057   0.02103   0.01530  -0.0637   0.0569   0.9218
  12.500   1.6189   0.02122   0.01563  -0.0613   0.0558   1.0000
  12.750   1.6379   0.02172   0.01616  -0.0604   0.0538   1.0000
  13.000   1.6551   0.02235   0.01678  -0.0592   0.0512   1.0000
  13.250   1.6702   0.02312   0.01756  -0.0579   0.0485   1.0000
  13.500   1.6869   0.02377   0.01826  -0.0568   0.0462   1.0000
  13.750   1.7009   0.02464   0.01911  -0.0554   0.0433   1.0000
  14.000   1.7140   0.02558   0.02008  -0.0540   0.0409   1.0000
  14.250   1.7268   0.02655   0.02109  -0.0526   0.0387   1.0000
  14.500   1.7369   0.02774   0.02229  -0.0510   0.0363   1.0000
  14.750   1.7479   0.02889   0.02349  -0.0496   0.0346   1.0000
  15.000   1.7577   0.03013   0.02478  -0.0482   0.0330   1.0000
  15.250   1.7651   0.03159   0.02628  -0.0466   0.0314   1.0000
  15.500   1.7715   0.03318   0.02792  -0.0451   0.0299   1.0000
  15.750   1.7802   0.03458   0.02940  -0.0439   0.0290   1.0000
  16.000   1.7864   0.03622   0.03111  -0.0426   0.0279   1.0000
  16.250   1.7903   0.03811   0.03307  -0.0413   0.0269   1.0000
  16.500   1.7913   0.04033   0.03535  -0.0399   0.0258   1.0000
  16.750   1.7940   0.04242   0.03753  -0.0388   0.0250   1.0000
  17.000   1.7980   0.04443   0.03963  -0.0380   0.0243   1.0000
  17.250   1.7995   0.04677   0.04206  -0.0372   0.0236   1.0000
  17.500   1.7985   0.04946   0.04483  -0.0365   0.0228   1.0000
  17.750   1.7944   0.05259   0.04804  -0.0360   0.0221   1.0000
  18.000   1.7869   0.05629   0.05185  -0.0358   0.0213   1.0000
  18.250   1.7825   0.05978   0.05545  -0.0359   0.0209   1.0000
  18.500   1.7792   0.06325   0.05903  -0.0362   0.0204   1.0000
  18.750   1.7720   0.06736   0.06327  -0.0369   0.0199   1.0000
  19.000   1.7615   0.07214   0.06816  -0.0381   0.0195   1.0000
  19.250   1.7470   0.07770   0.07386  -0.0398   0.0191   1.0000
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