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NASA LRN 1015 (NASA TM 102840) (lrn1015-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NASA LRN 1015 (NASA TM 102840) (lrn1015-il)
Reynolds number: 200,000
Max Cl/Cd: 72.58 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-lrn1015-il-200000-n5.txt
Download as CSV file: xf-lrn1015-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA LRN 1015 (NASA TM 102840)                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.0739   0.09361   0.08869  -0.1050   0.7765   0.0291
 -10.500  -0.0749   0.08971   0.08484  -0.1072   0.7747   0.0296
 -10.250  -0.0852   0.08413   0.07933  -0.1114   0.7727   0.0300
  -9.750  -0.0833   0.07532   0.07056  -0.1130   0.7693   0.0205
  -9.500  -0.0912   0.06976   0.06503  -0.1165   0.7674   0.0206
  -9.250  -0.0954   0.06539   0.06069  -0.1193   0.7654   0.0204
  -9.000  -0.1013   0.06149   0.05677  -0.1218   0.7635   0.0199
  -8.750  -0.1181   0.05709   0.05230  -0.1234   0.7615   0.0197
  -8.500  -0.1361   0.05407   0.04922  -0.1222   0.7590   0.0196
  -8.250  -0.1468   0.05068   0.04572  -0.1212   0.7566   0.0196
  -8.000  -0.1524   0.04738   0.04225  -0.1199   0.7543   0.0196
  -7.750  -0.1537   0.04413   0.03878  -0.1184   0.7522   0.0196
  -7.500  -0.1511   0.04095   0.03534  -0.1168   0.7503   0.0192
  -7.250  -0.1456   0.03766   0.03171  -0.1151   0.7484   0.0187
  -7.000  -0.1374   0.03430   0.02792  -0.1132   0.7468   0.0183
  -6.750  -0.1241   0.03157   0.02477  -0.1117   0.7453   0.0182
  -6.500  -0.1076   0.02944   0.02230  -0.1103   0.7437   0.0182
  -6.250  -0.0893   0.02776   0.02036  -0.1091   0.7416   0.0184
  -6.000  -0.0689   0.02632   0.01868  -0.1082   0.7396   0.0186
  -5.750  -0.0470   0.02500   0.01710  -0.1073   0.7375   0.0190
  -5.500  -0.0237   0.02392   0.01577  -0.1065   0.7356   0.0199
  -5.250   0.0008   0.02295   0.01448  -0.1058   0.7338   0.0208
  -5.000   0.0255   0.02199   0.01346  -0.1054   0.7323   0.0214
  -4.750   0.0507   0.02119   0.01258  -0.1050   0.7310   0.0218
  -4.500   0.0762   0.02047   0.01180  -0.1045   0.7298   0.0224
  -4.250   0.1018   0.01982   0.01109  -0.1041   0.7287   0.0231
  -4.000   0.1244   0.01935   0.01060  -0.1033   0.7263   0.0239
  -3.750   0.1470   0.01894   0.01017  -0.1024   0.7236   0.0247
  -3.500   0.1700   0.01853   0.00980  -0.1018   0.7214   0.0262
  -3.250   0.1940   0.01822   0.00950  -0.1012   0.7195   0.0282
  -3.000   0.2186   0.01789   0.00912  -0.1007   0.7177   0.0299
  -2.750   0.2435   0.01751   0.00872  -0.1003   0.7161   0.0318
  -2.500   0.2697   0.01723   0.00838  -0.1000   0.7147   0.0349
  -2.250   0.2961   0.01695   0.00808  -0.0998   0.7135   0.0407
  -2.000   0.3222   0.01670   0.00783  -0.0995   0.7122   0.0518
  -1.750   0.3390   0.01612   0.00790  -0.0983   0.7086   0.1961
  -1.500   0.3509   0.01484   0.00798  -0.0963   0.7056   0.5507
  -1.250   0.3647   0.01469   0.00854  -0.0926   0.7034   0.7500
  -1.000   0.3848   0.01491   0.00881  -0.0902   0.7015   0.8061
  -0.750   0.4048   0.01506   0.00896  -0.0878   0.6999   0.8390
  -0.500   0.4300   0.01508   0.00891  -0.0869   0.6985   0.8521
  -0.250   0.4571   0.01508   0.00881  -0.0866   0.6973   0.8604
   0.000   0.4756   0.01536   0.00912  -0.0850   0.6934   0.8686
   0.250   0.4967   0.01553   0.00928  -0.0838   0.6900   0.8765
   0.500   0.5210   0.01559   0.00929  -0.0832   0.6875   0.8835
   0.750   0.5470   0.01556   0.00922  -0.0827   0.6855   0.8898
   1.000   0.5748   0.01551   0.00912  -0.0827   0.6838   0.8964
   1.250   0.6033   0.01541   0.00897  -0.0827   0.6824   0.9013
   1.500   0.6231   0.01562   0.00921  -0.0814   0.6785   0.9082
   1.750   0.6432   0.01580   0.00941  -0.0802   0.6741   0.9149
   2.000   0.6702   0.01572   0.00932  -0.0800   0.6712   0.9206
   2.250   0.7004   0.01552   0.00909  -0.0804   0.6688   0.9264
   2.500   0.7345   0.01522   0.00873  -0.0813   0.6666   0.9308
   2.750   0.7521   0.01546   0.00906  -0.0799   0.6594   0.9392
   3.000   0.7829   0.01524   0.00882  -0.0804   0.6551   0.9452
   3.250   0.8192   0.01490   0.00844  -0.0818   0.6520   0.9498
   3.500   0.8437   0.01508   0.00870  -0.0817   0.6453   0.9587
   3.750   0.8776   0.01496   0.00859  -0.0831   0.6399   0.9651
   4.000   0.9156   0.01461   0.00820  -0.0849   0.6359   0.9705
   4.250   0.9433   0.01487   0.00856  -0.0857   0.6269   0.9851
   4.500   0.9788   0.01462   0.00829  -0.0873   0.6214   1.0000
   4.750   0.9911   0.01489   0.00861  -0.0850   0.6125   1.0000
   5.000   1.0195   0.01468   0.00838  -0.0850   0.6058   1.0000
   5.250   1.0341   0.01494   0.00869  -0.0831   0.5952   1.0000
   5.500   1.0542   0.01502   0.00877  -0.0819   0.5848   1.0000
   5.750   1.0753   0.01504   0.00877  -0.0809   0.5726   1.0000
   6.000   1.0932   0.01513   0.00884  -0.0793   0.5585   1.0000
   6.250   1.1097   0.01529   0.00896  -0.0774   0.5424   1.0000
   6.500   1.1250   0.01550   0.00910  -0.0754   0.5222   1.0000
   6.750   1.1392   0.01580   0.00926  -0.0733   0.4987   1.0000
   7.000   1.1475   0.01636   0.00969  -0.0704   0.4715   1.0000
   7.250   1.1509   0.01723   0.01038  -0.0672   0.4425   1.0000
   7.500   1.1523   0.01833   0.01131  -0.0641   0.4147   1.0000
   7.750   1.1522   0.01962   0.01242  -0.0610   0.3872   1.0000
   8.000   1.1533   0.02095   0.01361  -0.0582   0.3611   1.0000
   8.250   1.1555   0.02229   0.01482  -0.0557   0.3385   1.0000
   8.500   1.1597   0.02357   0.01600  -0.0535   0.3177   1.0000
   8.750   1.1647   0.02486   0.01719  -0.0514   0.2987   1.0000
   9.000   1.1709   0.02611   0.01838  -0.0496   0.2822   1.0000
   9.250   1.1781   0.02734   0.01955  -0.0479   0.2670   1.0000
   9.500   1.1855   0.02858   0.02075  -0.0464   0.2527   1.0000
   9.750   1.1935   0.02982   0.02194  -0.0449   0.2393   1.0000
  10.000   1.2013   0.03110   0.02319  -0.0435   0.2269   1.0000
  10.250   1.2090   0.03241   0.02446  -0.0421   0.2150   1.0000
  10.500   1.2189   0.03361   0.02566  -0.0410   0.2042   1.0000
  10.750   1.2284   0.03487   0.02692  -0.0399   0.1949   1.0000
  11.000   1.2371   0.03624   0.02827  -0.0388   0.1858   1.0000
  11.250   1.2476   0.03750   0.02957  -0.0379   0.1770   1.0000
  11.500   1.2558   0.03897   0.03101  -0.0369   0.1690   1.0000
  11.750   1.2662   0.04029   0.03237  -0.0361   0.1608   1.0000
  12.000   1.2744   0.04182   0.03390  -0.0352   0.1540   1.0000
  12.250   1.2851   0.04317   0.03530  -0.0345   0.1472   1.0000
  12.500   1.2925   0.04484   0.03697  -0.0337   0.1415   1.0000
  12.750   1.3035   0.04621   0.03841  -0.0331   0.1359   1.0000
  13.000   1.3121   0.04782   0.04006  -0.0325   0.1309   1.0000
  13.250   1.3195   0.04957   0.04183  -0.0318   0.1264   1.0000
  13.500   1.3298   0.05108   0.04344  -0.0313   0.1216   1.0000
  13.750   1.3374   0.05287   0.04528  -0.0308   0.1173   1.0000
  14.000   1.3434   0.05483   0.04725  -0.0303   0.1134   1.0000
  14.250   1.3533   0.05645   0.04898  -0.0299   0.1099   1.0000
  14.500   1.3613   0.05828   0.05089  -0.0295   0.1066   1.0000
  14.750   1.3674   0.06033   0.05299  -0.0292   0.1035   1.0000
  15.000   1.3723   0.06252   0.05520  -0.0289   0.1011   1.0000
  15.250   1.3817   0.06428   0.05710  -0.0286   0.0987   1.0000
  15.500   1.3894   0.06623   0.05916  -0.0285   0.0961   1.0000
  15.750   1.3955   0.06839   0.06142  -0.0284   0.0935   1.0000
  16.000   1.4002   0.07073   0.06381  -0.0283   0.0912   1.0000
  16.250   1.4039   0.07321   0.06632  -0.0283   0.0889   1.0000
  16.500   1.4108   0.07540   0.06867  -0.0284   0.0866   1.0000
  16.750   1.4158   0.07783   0.07124  -0.0286   0.0839   1.0000
  17.000   1.4190   0.08053   0.07403  -0.0290   0.0814   1.0000
  17.250   1.4206   0.08344   0.07699  -0.0294   0.0792   1.0000
  17.500   1.4224   0.08639   0.08001  -0.0299   0.0769   1.0000
  17.750   1.4262   0.08912   0.08292  -0.0304   0.0748   1.0000
  18.000   1.4277   0.09224   0.08618  -0.0311   0.0723   1.0000
  18.250   1.4273   0.09562   0.08966  -0.0320   0.0700   1.0000
  18.500   1.4258   0.09917   0.09327  -0.0330   0.0681   1.0000
  18.750   1.4254   0.10263   0.09685  -0.0341   0.0661   1.0000
  19.000   1.4254   0.10613   0.10053  -0.0353   0.0640   1.0000
  19.250   1.4242   0.10983   0.10437  -0.0366   0.0620   1.0000
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