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AUGUST 160 (august160-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: AUGUST 160 (august160-il)
Reynolds number: 500,000
Max Cl/Cd: 82.08 at α=10°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-august160-il-500000.txt
Download as CSV file: xf-august160-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AUGUST 160                                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.1619   0.08963   0.08545  -0.0564   0.5063   0.0232
  -9.750  -0.1642   0.08495   0.08079  -0.0592   0.5016   0.0232
  -9.500  -0.1610   0.08184   0.07767  -0.0597   0.4944   0.0234
  -9.250  -0.1533   0.07994   0.07573  -0.0596   0.4876   0.0236
  -9.000  -0.1489   0.07725   0.07306  -0.0604   0.4822   0.0237
  -8.750  -0.1465   0.07436   0.07017  -0.0615   0.4769   0.0240
  -8.500  -0.1445   0.07165   0.06745  -0.0625   0.4712   0.0245
  -8.250  -0.1520   0.06738   0.06321  -0.0654   0.4683   0.0245
  -8.000  -0.1685   0.06276   0.05860  -0.0681   0.4657   0.0247
  -7.750  -0.1828   0.05928   0.05510  -0.0676   0.4629   0.0251
  -7.500  -0.1904   0.05533   0.05107  -0.0676   0.4594   0.0251
  -7.250  -0.2269   0.04526   0.04056  -0.0662   0.4610   0.0273
  -7.000  -0.2162   0.04360   0.03884  -0.0649   0.4553   0.0275
  -6.750  -0.2038   0.04234   0.03749  -0.0637   0.4496   0.0279
  -6.500  -0.2152   0.03753   0.03197  -0.0592   0.4478   0.0313
  -6.250  -0.1962   0.03550   0.03002  -0.0587   0.4423   0.0316
  -6.000  -0.1787   0.03416   0.02864  -0.0577   0.4368   0.0320
  -5.750  -0.1615   0.03297   0.02733  -0.0565   0.4312   0.0328
  -5.500  -0.1527   0.03012   0.02399  -0.0534   0.4280   0.0363
  -5.250  -0.1316   0.02887   0.02275  -0.0526   0.4231   0.0370
  -5.000  -0.1177   0.02754   0.02088  -0.0498   0.4189   0.0411
  -4.750  -0.0957   0.02590   0.01924  -0.0492   0.4140   0.0418
  -4.500  -0.0795   0.01941   0.01145  -0.0440   0.4116   0.0233
  -4.250  -0.0536   0.01797   0.01000  -0.0434   0.4078   0.0227
  -4.000  -0.0280   0.01691   0.00883  -0.0427   0.4034   0.0222
  -3.750  -0.0026   0.01614   0.00793  -0.0418   0.3993   0.0220
  -3.500   0.0224   0.01555   0.00720  -0.0410   0.3949   0.0220
  -3.250   0.0479   0.01500   0.00661  -0.0402   0.3917   0.0222
  -3.000   0.0732   0.01454   0.00611  -0.0394   0.3885   0.0226
  -2.750   0.0985   0.01420   0.00571  -0.0386   0.3849   0.0231
  -2.500   0.1232   0.01388   0.00534  -0.0377   0.3815   0.0233
  -2.250   0.1466   0.01352   0.00494  -0.0367   0.3779   0.0240
  -2.000   0.1716   0.01331   0.00472  -0.0359   0.3749   0.0247
  -1.750   0.1975   0.01311   0.00452  -0.0353   0.3724   0.0259
  -1.500   0.2233   0.01294   0.00433  -0.0346   0.3698   0.0272
  -1.250   0.2489   0.01277   0.00416  -0.0340   0.3671   0.0290
  -1.000   0.2747   0.01266   0.00401  -0.0333   0.3645   0.0315
  -0.750   0.3002   0.01257   0.00390  -0.0327   0.3618   0.0381
  -0.500   0.3213   0.01212   0.00383  -0.0314   0.3590   0.1533
  -0.250   0.3409   0.01151   0.00382  -0.0300   0.3572   0.3278
   0.000   0.3516   0.01054   0.00379  -0.0267   0.3557   0.6031
   0.250   0.3690   0.00985   0.00404  -0.0238   0.3539   0.8797
   0.500   0.4052   0.01006   0.00427  -0.0248   0.3516   0.9323
   0.750   0.4537   0.01040   0.00454  -0.0284   0.3490   0.9578
   1.000   0.5263   0.01084   0.00483  -0.0371   0.3462   0.9697
   1.250   0.5670   0.01110   0.00497  -0.0396   0.3437   0.9766
   1.500   0.6171   0.01139   0.00515  -0.0442   0.3409   0.9799
   1.750   0.6619   0.01152   0.00525  -0.0476   0.3394   0.9857
   2.000   0.7061   0.01161   0.00529  -0.0509   0.3378   0.9885
   2.250   0.7523   0.01171   0.00535  -0.0548   0.3359   0.9931
   2.500   0.7986   0.01177   0.00536  -0.0587   0.3339   0.9973
   2.750   0.8378   0.01183   0.00538  -0.0611   0.3321   1.0000
   3.000   0.8604   0.01194   0.00545  -0.0602   0.3305   1.0000
   3.250   0.8830   0.01207   0.00555  -0.0593   0.3292   1.0000
   3.500   0.9056   0.01223   0.00568  -0.0584   0.3279   1.0000
   3.750   0.9280   0.01246   0.00587  -0.0575   0.3263   1.0000
   4.000   0.9505   0.01281   0.00618  -0.0566   0.3244   1.0000
   4.250   0.9728   0.01292   0.00631  -0.0557   0.3237   1.0000
   4.500   0.9950   0.01304   0.00645  -0.0547   0.3227   1.0000
   4.750   1.0170   0.01317   0.00660  -0.0537   0.3215   1.0000
   5.000   1.0388   0.01332   0.00677  -0.0526   0.3203   1.0000
   5.250   1.0605   0.01348   0.00696  -0.0516   0.3190   1.0000
   5.500   1.0822   0.01366   0.00715  -0.0505   0.3179   1.0000
   5.750   1.1037   0.01386   0.00735  -0.0495   0.3169   1.0000
   6.000   1.1250   0.01406   0.00757  -0.0484   0.3159   1.0000
   6.250   1.1462   0.01426   0.00778  -0.0473   0.3148   1.0000
   6.500   1.1672   0.01442   0.00794  -0.0462   0.3133   1.0000
   6.750   1.1880   0.01464   0.00815  -0.0450   0.3122   1.0000
   7.000   1.2087   0.01489   0.00840  -0.0439   0.3107   1.0000
   7.250   1.2296   0.01543   0.00890  -0.0430   0.3080   1.0000
   7.500   1.2491   0.01557   0.00909  -0.0415   0.3073   1.0000
   7.750   1.2683   0.01573   0.00931  -0.0401   0.3063   1.0000
   8.000   1.2874   0.01589   0.00953  -0.0387   0.3052   1.0000
   8.250   1.3069   0.01612   0.00981  -0.0374   0.3042   1.0000
   8.500   1.3266   0.01638   0.01012  -0.0361   0.3033   1.0000
   8.750   1.3466   0.01663   0.01042  -0.0350   0.3022   1.0000
   9.000   1.3669   0.01688   0.01071  -0.0339   0.3011   1.0000
   9.250   1.3877   0.01715   0.01102  -0.0329   0.3001   1.0000
   9.500   1.4086   0.01732   0.01121  -0.0319   0.2986   1.0000
   9.750   1.4299   0.01749   0.01140  -0.0310   0.2971   1.0000
  10.000   1.4512   0.01768   0.01159  -0.0302   0.2954   1.0000
  10.250   1.4730   0.01803   0.01193  -0.0295   0.2936   1.0000
  10.500   1.4946   0.01855   0.01248  -0.0289   0.2919   1.0000
  10.750   1.5130   0.01876   0.01279  -0.0277   0.2910   1.0000
  11.000   1.5317   0.01904   0.01316  -0.0265   0.2900   1.0000
  11.250   1.5493   0.01927   0.01348  -0.0252   0.2885   1.0000
  11.500   1.5671   0.01950   0.01378  -0.0239   0.2868   1.0000
  11.750   1.5845   0.01966   0.01401  -0.0226   0.2848   1.0000
  12.000   1.6024   0.01987   0.01426  -0.0214   0.2830   1.0000
  12.250   1.6182   0.02006   0.01448  -0.0198   0.2812   1.0000
  12.500   1.6337   0.02030   0.01472  -0.0182   0.2791   1.0000
  12.750   1.6502   0.02075   0.01519  -0.0170   0.2768   1.0000
  13.000   1.6598   0.02114   0.01571  -0.0148   0.2753   1.0000
  13.250   1.6707   0.02160   0.01628  -0.0131   0.2736   1.0000
  13.500   1.6827   0.02211   0.01690  -0.0117   0.2716   1.0000
  13.750   1.6949   0.02266   0.01752  -0.0105   0.2694   1.0000
  14.000   1.7070   0.02326   0.01819  -0.0095   0.2673   1.0000
  14.250   1.7192   0.02394   0.01888  -0.0087   0.2647   1.0000
  14.500   1.7334   0.02471   0.01968  -0.0081   0.2625   1.0000
  14.750   1.7377   0.02605   0.02120  -0.0074   0.2603   1.0000
  15.000   1.7441   0.02745   0.02273  -0.0071   0.2579   1.0000
  15.250   1.7495   0.02904   0.02444  -0.0070   0.2545   1.0000
  15.500   1.7555   0.03068   0.02614  -0.0071   0.2515   1.0000
  15.750   1.7600   0.03248   0.02795  -0.0071   0.2482   1.0000
  16.000   1.7576   0.03519   0.03086  -0.0076   0.2449   1.0000
  16.250   1.7534   0.03815   0.03396  -0.0082   0.2403   1.0000
  16.500   1.7469   0.04133   0.03719  -0.0087   0.2362   1.0000
  16.750   1.7346   0.04524   0.04123  -0.0094   0.2314   1.0000
  17.000   1.7159   0.04991   0.04602  -0.0103   0.2261   1.0000
  17.250   1.6914   0.05537   0.05154  -0.0115   0.2204   1.0000
  17.500   1.6642   0.06131   0.05759  -0.0127   0.2147   1.0000
  17.750   1.6320   0.06796   0.06427  -0.0142   0.2088   1.0000
  18.000   1.5975   0.07509   0.07150  -0.0159   0.2027   1.0000
  18.250   1.5667   0.08185   0.07826  -0.0175   0.1962   1.0000
  18.500   1.5314   0.08939   0.08591  -0.0194   0.1887   1.0000
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