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LA2573A (la2573a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: LA2573A (la2573a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 110.9 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-la2573a-il-1000000-n5.txt
Download as CSV file: xf-la2573a-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: LA2573A                                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -1.1785   0.04691   0.04308  -0.0278   0.5242   0.0208
 -14.500  -1.2119   0.04181   0.03775  -0.0273   0.5213   0.0208
 -14.250  -1.2288   0.03877   0.03453  -0.0250   0.5161   0.0209
 -14.000  -1.2374   0.03662   0.03221  -0.0222   0.5092   0.0210
 -13.750  -1.2449   0.03468   0.03010  -0.0187   0.5038   0.0210
 -13.500  -1.2453   0.03318   0.02845  -0.0155   0.4987   0.0211
 -13.250  -1.2389   0.03163   0.02674  -0.0133   0.4929   0.0212
 -12.750  -1.2161   0.02901   0.02381  -0.0097   0.4827   0.0215
 -12.500  -1.2017   0.02782   0.02248  -0.0081   0.4786   0.0216
 -12.250  -1.1857   0.02673   0.02124  -0.0067   0.4743   0.0217
 -12.000  -1.1681   0.02574   0.02011  -0.0054   0.4701   0.0218
 -11.500  -1.1290   0.02404   0.01815  -0.0031   0.4632   0.0221
 -11.250  -1.1080   0.02328   0.01728  -0.0020   0.4605   0.0222
 -11.000  -1.0862   0.02261   0.01650  -0.0011   0.4575   0.0223
 -10.750  -1.0649   0.02182   0.01560  -0.0001   0.4542   0.0224
 -10.500  -1.0439   0.02096   0.01463   0.0010   0.4510   0.0225
 -10.250  -1.0214   0.02028   0.01387   0.0019   0.4477   0.0227
 -10.000  -0.9979   0.01972   0.01324   0.0027   0.4452   0.0228
  -9.750  -0.9738   0.01921   0.01268   0.0034   0.4437   0.0230
  -9.500  -0.9494   0.01872   0.01213   0.0041   0.4419   0.0231
  -9.250  -0.9245   0.01827   0.01163   0.0048   0.4400   0.0232
  -9.000  -0.8994   0.01785   0.01115   0.0054   0.4380   0.0234
  -8.750  -0.8740   0.01744   0.01068   0.0060   0.4360   0.0236
  -8.500  -0.8485   0.01703   0.01022   0.0066   0.4340   0.0237
  -8.250  -0.8228   0.01664   0.00976   0.0072   0.4319   0.0239
  -8.000  -0.7970   0.01625   0.00931   0.0077   0.4298   0.0241
  -7.750  -0.7710   0.01587   0.00887   0.0083   0.4273   0.0243
  -7.500  -0.7448   0.01550   0.00845   0.0088   0.4258   0.0245
  -7.250  -0.7185   0.01513   0.00803   0.0093   0.4246   0.0247
  -7.000  -0.6920   0.01479   0.00764   0.0098   0.4234   0.0249
  -6.750  -0.6653   0.01446   0.00726   0.0102   0.4221   0.0252
  -6.500  -0.6384   0.01417   0.00693   0.0107   0.4207   0.0254
  -6.250  -0.6113   0.01390   0.00662   0.0111   0.4192   0.0255
  -6.000  -0.5848   0.01354   0.00621   0.0116   0.4177   0.0258
  -5.750  -0.5580   0.01320   0.00585   0.0120   0.4163   0.0261
  -5.500  -0.5309   0.01293   0.00556   0.0124   0.4146   0.0263
  -5.250  -0.5036   0.01270   0.00531   0.0128   0.4129   0.0266
  -5.000  -0.4762   0.01248   0.00507   0.0131   0.4110   0.0269
  -4.750  -0.4487   0.01228   0.00484   0.0135   0.4091   0.0272
  -4.500  -0.4211   0.01208   0.00462   0.0138   0.4079   0.0275
  -4.250  -0.3935   0.01187   0.00440   0.0142   0.4071   0.0278
  -4.000  -0.3657   0.01167   0.00419   0.0145   0.4063   0.0282
  -3.750  -0.3380   0.01148   0.00398   0.0148   0.4053   0.0286
  -3.500  -0.3101   0.01130   0.00379   0.0151   0.4041   0.0289
  -3.250  -0.2821   0.01114   0.00361   0.0154   0.4027   0.0291
  -3.000  -0.2545   0.01092   0.00339   0.0157   0.4012   0.0296
  -2.750  -0.2266   0.01075   0.00323   0.0160   0.3999   0.0301
  -2.500  -0.1985   0.01062   0.00310   0.0162   0.3986   0.0307
  -2.250  -0.1703   0.01050   0.00297   0.0164   0.3973   0.0314
  -2.000  -0.1422   0.01038   0.00284   0.0167   0.3959   0.0320
  -1.750  -0.1139   0.01027   0.00272   0.0169   0.3944   0.0326
  -1.500  -0.0857   0.01018   0.00261   0.0171   0.3926   0.0330
  -1.250  -0.0577   0.01006   0.00249   0.0173   0.3908   0.0339
  -1.000  -0.0294   0.00994   0.00240   0.0175   0.3902   0.0348
  -0.750  -0.0009   0.00985   0.00232   0.0177   0.3893   0.0357
  -0.500   0.0275   0.00976   0.00225   0.0179   0.3883   0.0366
  -0.250   0.0560   0.00967   0.00217   0.0180   0.3871   0.0378
   0.000   0.0844   0.00958   0.00211   0.0182   0.3857   0.0395
   0.250   0.1130   0.00951   0.00206   0.0183   0.3843   0.0412
   0.500   0.1414   0.00944   0.00200   0.0185   0.3830   0.0433
   0.750   0.1700   0.00938   0.00197   0.0186   0.3816   0.0460
   1.000   0.1985   0.00932   0.00193   0.0187   0.3802   0.0499
   1.250   0.2270   0.00927   0.00190   0.0188   0.3786   0.0559
   1.750   0.2836   0.00915   0.00188   0.0191   0.3750   0.0852
   2.000   0.3116   0.00903   0.00189   0.0192   0.3739   0.1202
   2.250   0.3389   0.00880   0.00189   0.0194   0.3728   0.1965
   2.500   0.3452   0.00675   0.00184   0.0233   0.3718   0.8295
   2.750   0.3716   0.00673   0.00194   0.0240   0.3702   0.8726
   3.000   0.3992   0.00677   0.00201   0.0244   0.3687   0.8900
   3.250   0.4266   0.00682   0.00208   0.0249   0.3671   0.9048
   3.500   0.4530   0.00687   0.00216   0.0257   0.3651   0.9197
   3.750   0.4787   0.00693   0.00225   0.0266   0.3633   0.9330
   4.000   0.5072   0.00700   0.00229   0.0267   0.3614   0.9360
   4.250   0.5362   0.00707   0.00234   0.0266   0.3591   0.9374
   4.500   0.5653   0.00712   0.00239   0.0265   0.3576   0.9388
   4.750   0.5944   0.00717   0.00244   0.0264   0.3558   0.9401
   5.000   0.6236   0.00721   0.00250   0.0263   0.3535   0.9414
   5.250   0.6528   0.00726   0.00255   0.0262   0.3510   0.9428
   5.500   0.6818   0.00732   0.00261   0.0261   0.3484   0.9443
   5.750   0.7106   0.00740   0.00268   0.0261   0.3456   0.9460
   6.000   0.7394   0.00748   0.00276   0.0260   0.3429   0.9477
   6.250   0.7683   0.00754   0.00284   0.0259   0.3404   0.9496
   6.500   0.7970   0.00761   0.00293   0.0258   0.3369   0.9516
   6.750   0.8254   0.00770   0.00301   0.0258   0.3329   0.9538
   7.250   0.8822   0.00796   0.00321   0.0256   0.3133   0.9582
   7.500   0.9101   0.00821   0.00338   0.0254   0.2928   0.9604
   7.750   0.9382   0.00846   0.00359   0.0252   0.2795   0.9629
   8.000   0.9659   0.00874   0.00382   0.0251   0.2663   0.9657
   8.250   0.9932   0.00906   0.00409   0.0250   0.2523   0.9689
   8.500   1.0213   0.00947   0.00443   0.0245   0.2340   0.9715
   8.750   1.0495   0.01004   0.00490   0.0239   0.2111   0.9741
   9.000   1.0773   0.01071   0.00544   0.0232   0.1868   0.9773
   9.250   1.1044   0.01142   0.00604   0.0225   0.1627   0.9808
   9.500   1.1322   0.01226   0.00675   0.0214   0.1374   0.9838
   9.750   1.1600   0.01325   0.00760   0.0201   0.1115   0.9865
  10.000   1.1876   0.01420   0.00844   0.0187   0.0912   0.9897
  10.250   1.2148   0.01506   0.00923   0.0176   0.0770   0.9932
  10.750   1.2580   0.01668   0.01078   0.0173   0.0602   1.0000
  11.000   1.2732   0.01747   0.01156   0.0184   0.0547   1.0000
  11.250   1.2875   0.01834   0.01244   0.0193   0.0503   1.0000
  11.500   1.2990   0.01942   0.01353   0.0202   0.0465   1.0000
  11.750   1.3065   0.02086   0.01502   0.0208   0.0439   1.0000
  12.250   1.2917   0.02814   0.02249   0.0181   0.0411   1.0000
  12.500   1.2880   0.03125   0.02565   0.0175   0.0398   1.0000
  12.750   1.2823   0.03446   0.02892   0.0169   0.0385   1.0000
  13.000   1.2769   0.03760   0.03209   0.0164   0.0374   1.0000
  13.250   1.2735   0.04051   0.03506   0.0159   0.0365   1.0000
  13.500   1.2705   0.04336   0.03796   0.0155   0.0355   1.0000
  13.750   1.2675   0.04621   0.04085   0.0151   0.0346   1.0000
  14.000   1.2640   0.04913   0.04381   0.0146   0.0338   1.0000
  14.250   1.2632   0.05188   0.04660   0.0142   0.0328   1.0000
  14.500   1.2649   0.05444   0.04920   0.0137   0.0322   1.0000
  14.750   1.2657   0.05716   0.05196   0.0132   0.0316   1.0000
  15.000   1.2674   0.05977   0.05460   0.0127   0.0306   1.0000
  15.250   1.2680   0.06257   0.05745   0.0121   0.0301   1.0000
  15.500   1.2685   0.06540   0.06031   0.0115   0.0294   1.0000
  15.750   1.2710   0.06796   0.06290   0.0110   0.0287   1.0000
  16.000   1.2722   0.07079   0.06577   0.0104   0.0283   1.0000
  16.250   1.2743   0.07347   0.06850   0.0098   0.0278   1.0000
  16.500   1.2768   0.07608   0.07115   0.0092   0.0273   1.0000
  16.750   1.2765   0.07912   0.07424   0.0085   0.0269   1.0000
  17.000   1.2775   0.08199   0.07714   0.0078   0.0264   1.0000
  17.250   1.2783   0.08491   0.08009   0.0071   0.0260   1.0000
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