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RAE(NPL) 5212 AIRFOIL (rae5212-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: RAE(NPL) 5212 AIRFOIL (rae5212-il)
Reynolds number: 500,000
Max Cl/Cd: 63.29 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae5212-il-500000-n5.txt
Download as CSV file: xf-rae5212-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAE(NPL) 5212 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.8564   0.06619   0.06280  -0.0628   1.0000   0.0104
 -14.500  -0.8812   0.05884   0.05526  -0.0673   1.0000   0.0104
 -14.250  -0.8947   0.05397   0.05027  -0.0697   1.0000   0.0105
 -14.000  -0.9123   0.04902   0.04514  -0.0717   1.0000   0.0105
 -13.750  -0.9196   0.04576   0.04178  -0.0725   1.0000   0.0106
 -13.500  -0.9255   0.04287   0.03879  -0.0729   1.0000   0.0107
 -13.250  -0.9318   0.04015   0.03597  -0.0728   1.0000   0.0107
 -13.000  -0.9371   0.03777   0.03347  -0.0722   1.0000   0.0108
 -12.750  -0.9401   0.03582   0.03143  -0.0712   1.0000   0.0109
 -12.500  -0.9423   0.03422   0.02976  -0.0697   1.0000   0.0110
 -12.250  -0.9489   0.03259   0.02802  -0.0674   1.0000   0.0111
 -12.000  -0.9599   0.03131   0.02664  -0.0637   1.0000   0.0112
 -11.750  -0.9667   0.03033   0.02558  -0.0595   1.0000   0.0113
 -11.500  -0.9662   0.02910   0.02422  -0.0565   1.0000   0.0114
 -11.250  -0.9506   0.02769   0.02267  -0.0562   0.9988   0.0116
 -11.000  -0.9265   0.02622   0.02103  -0.0575   0.9964   0.0119
 -10.750  -0.9011   0.02486   0.01948  -0.0587   0.9943   0.0122
 -10.500  -0.8775   0.02360   0.01806  -0.0593   0.9919   0.0125
 -10.250  -0.8524   0.02248   0.01678  -0.0600   0.9892   0.0127
 -10.000  -0.8255   0.02145   0.01561  -0.0609   0.9870   0.0130
  -9.750  -0.7974   0.02049   0.01460  -0.0621   0.9851   0.0134
  -9.500  -0.7673   0.01973   0.01379  -0.0635   0.9838   0.0137
  -9.250  -0.7438   0.01907   0.01306  -0.0633   0.9798   0.0140
  -9.000  -0.7160   0.01845   0.01239  -0.0639   0.9771   0.0145
  -8.750  -0.6867   0.01778   0.01164  -0.0648   0.9749   0.0150
  -8.500  -0.6559   0.01715   0.01092  -0.0660   0.9733   0.0156
  -8.250  -0.6268   0.01649   0.01019  -0.0668   0.9711   0.0162
  -8.000  -0.6040   0.01589   0.00958  -0.0663   0.9658   0.0167
  -7.750  -0.5748   0.01536   0.00902  -0.0670   0.9630   0.0172
  -7.500  -0.5438   0.01483   0.00846  -0.0681   0.9610   0.0179
  -7.250  -0.5116   0.01430   0.00788  -0.0693   0.9593   0.0187
  -7.000  -0.4893   0.01391   0.00743  -0.0684   0.9526   0.0194
  -6.750  -0.4605   0.01338   0.00690  -0.0689   0.9489   0.0205
  -6.500  -0.4295   0.01296   0.00647  -0.0699   0.9462   0.0216
  -6.250  -0.4036   0.01259   0.00606  -0.0697   0.9406   0.0226
  -6.000  -0.3757   0.01221   0.00564  -0.0698   0.9352   0.0237
  -5.750  -0.3447   0.01177   0.00521  -0.0707   0.9315   0.0252
  -5.500  -0.3177   0.01146   0.00488  -0.0707   0.9248   0.0268
  -5.250  -0.2880   0.01114   0.00453  -0.0711   0.9192   0.0288
  -5.000  -0.2573   0.01082   0.00421  -0.0719   0.9143   0.0316
  -4.750  -0.2289   0.01055   0.00392  -0.0720   0.9073   0.0343
  -4.500  -0.1982   0.01026   0.00363  -0.0727   0.9015   0.0390
  -4.250  -0.1699   0.01000   0.00338  -0.0729   0.8943   0.0447
  -4.000  -0.1407   0.00975   0.00314  -0.0732   0.8875   0.0530
  -3.750  -0.1126   0.00952   0.00292  -0.0733   0.8803   0.0657
  -3.500  -0.0852   0.00924   0.00271  -0.0733   0.8726   0.0880
  -3.250  -0.0584   0.00888   0.00250  -0.0733   0.8655   0.1334
  -3.000  -0.0333   0.00839   0.00226  -0.0730   0.8574   0.2098
  -2.750  -0.0095   0.00765   0.00197  -0.0727   0.8502   0.3431
  -2.500   0.0146   0.00714   0.00183  -0.0723   0.8424   0.4531
  -2.000   0.0686   0.00694   0.00186  -0.0717   0.8285   0.5532
  -1.750   0.0962   0.00695   0.00190  -0.0715   0.8218   0.5767
  -1.500   0.1238   0.00698   0.00194  -0.0713   0.8151   0.5947
  -1.250   0.1516   0.00702   0.00196  -0.0711   0.8080   0.6058
  -1.000   0.1795   0.00705   0.00196  -0.0709   0.8003   0.6117
  -0.750   0.2072   0.00707   0.00193  -0.0708   0.7903   0.6155
  -0.500   0.2342   0.00711   0.00188  -0.0704   0.7756   0.6189
   0.000   0.2860   0.00721   0.00182  -0.0691   0.7316   0.6250
   0.250   0.3122   0.00729   0.00181  -0.0686   0.7115   0.6284
   0.500   0.3376   0.00740   0.00180  -0.0679   0.6850   0.6318
   0.750   0.3622   0.00755   0.00180  -0.0671   0.6515   0.6349
   1.000   0.3869   0.00768   0.00183  -0.0663   0.6192   0.6377
   1.250   0.4101   0.00789   0.00188  -0.0652   0.5748   0.6407
   1.500   0.4314   0.00825   0.00197  -0.0639   0.5146   0.6439
   1.750   0.4513   0.00874   0.00214  -0.0624   0.4387   0.6473
   2.000   0.4717   0.00929   0.00233  -0.0610   0.3639   0.6505
   2.250   0.4933   0.00974   0.00253  -0.0599   0.3024   0.6534
   2.500   0.5159   0.01013   0.00272  -0.0590   0.2529   0.6566
   2.750   0.5390   0.01049   0.00291  -0.0581   0.2113   0.6601
   3.000   0.5623   0.01086   0.00311  -0.0573   0.1741   0.6637
   3.250   0.5859   0.01121   0.00330  -0.0566   0.1433   0.6672
   3.500   0.6099   0.01148   0.00350  -0.0559   0.1219   0.6703
   3.750   0.6341   0.01175   0.00370  -0.0552   0.1060   0.6736
   4.000   0.6585   0.01200   0.00391  -0.0546   0.0950   0.6770
   4.250   0.6829   0.01225   0.00411  -0.0539   0.0874   0.6808
   4.500   0.7079   0.01246   0.00432  -0.0534   0.0834   0.6844
   4.750   0.7322   0.01269   0.00455  -0.0527   0.0794   0.6878
   5.000   0.7561   0.01296   0.00481  -0.0520   0.0756   0.6914
   5.250   0.7807   0.01316   0.00505  -0.0514   0.0740   0.6953
   5.500   0.8050   0.01339   0.00530  -0.0508   0.0723   0.6992
   5.750   0.8289   0.01362   0.00557  -0.0500   0.0706   0.7031
   6.000   0.8523   0.01388   0.00586  -0.0493   0.0687   0.7079
   6.250   0.8753   0.01418   0.00617  -0.0484   0.0668   0.7128
   6.500   0.8973   0.01454   0.00655  -0.0474   0.0647   0.7177
   6.750   0.9199   0.01482   0.00689  -0.0465   0.0637   0.7229
   7.000   0.9427   0.01509   0.00721  -0.0456   0.0629   0.7287
   7.250   0.9651   0.01537   0.00757  -0.0447   0.0619   0.7348
   7.500   0.9870   0.01566   0.00793  -0.0437   0.0608   0.7419
   7.750   1.0086   0.01596   0.00829  -0.0426   0.0597   0.7498
   8.000   1.0296   0.01627   0.00868  -0.0415   0.0586   0.7593
   8.250   1.0499   0.01659   0.00906  -0.0402   0.0573   0.7706
   8.500   1.0683   0.01694   0.00948  -0.0386   0.0561   0.7859
   8.750   1.0840   0.01736   0.01001  -0.0365   0.0548   0.8097
   9.000   1.0984   0.01761   0.01051  -0.0340   0.0541   0.8734
   9.250   1.1313   0.01796   0.01104  -0.0355   0.0533   1.0000
   9.500   1.1502   0.01839   0.01151  -0.0341   0.0525   1.0000
   9.750   1.1686   0.01884   0.01201  -0.0326   0.0517   1.0000
  10.000   1.1873   0.01926   0.01248  -0.0313   0.0506   1.0000
  10.250   1.2060   0.01967   0.01292  -0.0299   0.0495   1.0000
  10.500   1.2244   0.02009   0.01337  -0.0286   0.0484   1.0000
  10.750   1.2416   0.02058   0.01387  -0.0272   0.0472   1.0000
  11.000   1.2565   0.02126   0.01457  -0.0254   0.0461   1.0000
  11.250   1.2741   0.02174   0.01513  -0.0241   0.0453   1.0000
  11.500   1.2915   0.02223   0.01569  -0.0228   0.0443   1.0000
  11.750   1.3085   0.02275   0.01628  -0.0214   0.0432   1.0000
  12.000   1.3247   0.02331   0.01690  -0.0200   0.0423   1.0000
  12.250   1.3407   0.02388   0.01752  -0.0187   0.0412   1.0000
  12.500   1.3559   0.02450   0.01816  -0.0173   0.0402   1.0000
  12.750   1.3691   0.02528   0.01897  -0.0157   0.0393   1.0000
  13.000   1.3824   0.02608   0.01986  -0.0143   0.0385   1.0000
  13.250   1.3962   0.02687   0.02075  -0.0129   0.0377   1.0000
  13.500   1.4093   0.02771   0.02168  -0.0115   0.0369   1.0000
  13.750   1.4221   0.02858   0.02262  -0.0102   0.0359   1.0000
  14.000   1.4346   0.02947   0.02356  -0.0090   0.0348   1.0000
  14.250   1.4456   0.03049   0.02464  -0.0077   0.0339   1.0000
  14.500   1.4555   0.03164   0.02584  -0.0064   0.0327   1.0000
  14.750   1.4655   0.03282   0.02714  -0.0053   0.0319   1.0000
  15.000   1.4749   0.03406   0.02848  -0.0041   0.0309   1.0000
  15.250   1.4838   0.03538   0.02988  -0.0031   0.0298   1.0000
  15.500   1.4911   0.03687   0.03144  -0.0021   0.0288   1.0000
  15.750   1.4964   0.03860   0.03322  -0.0012   0.0278   1.0000
  16.000   1.5026   0.04029   0.03506  -0.0004   0.0268   1.0000
  16.250   1.5071   0.04220   0.03708   0.0002   0.0258   1.0000
  16.500   1.5105   0.04429   0.03925   0.0007   0.0247   1.0000
  16.750   1.5117   0.04666   0.04170   0.0011   0.0237   1.0000
  17.000   1.5112   0.04933   0.04448   0.0012   0.0231   1.0000
  17.250   1.5105   0.05216   0.04743   0.0012   0.0222   1.0000
  17.500   1.5075   0.05537   0.05077   0.0008   0.0215   1.0000
  17.750   1.5026   0.05899   0.05450   0.0000   0.0208   1.0000
  18.000   1.4950   0.06317   0.05880  -0.0012   0.0203   1.0000
  18.250   1.4839   0.06813   0.06388  -0.0030   0.0197   1.0000
  18.500   1.4707   0.07367   0.06957  -0.0054   0.0194   1.0000
  18.750   1.4557   0.07983   0.07590  -0.0084   0.0190   1.0000
  19.000   1.4359   0.08717   0.08341  -0.0123   0.0188   1.0000
  19.250   1.4100   0.09597   0.09240  -0.0173   0.0188   1.0000
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