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TRAINER60 (trainer60-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: TRAINER60 (trainer60-il)
Reynolds number: 200,000
Max Cl/Cd: 51.65 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-trainer60-il-200000.txt
Download as CSV file: xf-trainer60-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: TRAINER60                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.2099   0.13163   0.12645   0.0179   1.0000   0.0488
 -19.500  -1.2307   0.12376   0.11834   0.0130   1.0000   0.0492
 -19.250  -1.2469   0.11696   0.11132   0.0090   1.0000   0.0495
 -19.000  -1.2615   0.11064   0.10478   0.0054   1.0000   0.0500
 -18.750  -1.2740   0.10483   0.09874   0.0023   1.0000   0.0504
 -18.500  -1.2851   0.09934   0.09302  -0.0006   1.0000   0.0507
 -18.250  -1.2662   0.09898   0.09277   0.0009   1.0000   0.0517
 -18.000  -1.2570   0.09694   0.09075   0.0006   1.0000   0.0526
 -17.750  -1.2532   0.09398   0.08773  -0.0003   1.0000   0.0533
 -17.500  -1.2513   0.09074   0.08440  -0.0013   1.0000   0.0541
 -17.250  -1.2516   0.08712   0.08065  -0.0026   1.0000   0.0551
 -17.000  -1.2523   0.08345   0.07683  -0.0039   1.0000   0.0559
 -16.750  -1.2505   0.08028   0.07354  -0.0048   1.0000   0.0569
 -16.500  -1.2364   0.07921   0.07259  -0.0040   1.0000   0.0583
 -16.250  -1.2309   0.07664   0.07003  -0.0045   1.0000   0.0596
 -16.000  -1.2278   0.07372   0.06703  -0.0053   1.0000   0.0611
 -15.750  -1.2269   0.07044   0.06362  -0.0062   1.0000   0.0625
 -15.500  -1.2205   0.06825   0.06146  -0.0061   1.0000   0.0641
 -15.250  -1.2169   0.06562   0.05886  -0.0065   1.0000   0.0658
 -15.000  -1.2149   0.06272   0.05592  -0.0070   1.0000   0.0676
 -14.750  -1.2136   0.05974   0.05282  -0.0076   1.0000   0.0696
 -14.500  -1.2136   0.05688   0.05001  -0.0078   1.0000   0.0716
 -14.250  -1.2147   0.05376   0.04688  -0.0083   1.0000   0.0738
 -14.000  -1.2148   0.05071   0.04375  -0.0089   1.0000   0.0767
 -13.750  -1.2185   0.04737   0.04042  -0.0094   1.0000   0.0795
 -13.500  -1.2208   0.04415   0.03718  -0.0099   1.0000   0.0831
 -13.250  -1.2232   0.04096   0.03397  -0.0103   1.0000   0.0873
 -13.000  -1.2258   0.03783   0.03083  -0.0107   1.0000   0.0928
 -12.750  -1.2294   0.03475   0.02778  -0.0108   1.0000   0.0994
 -12.500  -1.2316   0.03201   0.02508  -0.0106   1.0000   0.1086
 -12.250  -1.2324   0.02966   0.02278  -0.0099   1.0000   0.1210
 -12.000  -1.2294   0.02790   0.02102  -0.0088   1.0000   0.1356
 -11.750  -1.2235   0.02663   0.01972  -0.0072   1.0000   0.1488
 -11.500  -1.2174   0.02566   0.01875  -0.0050   1.0000   0.1592
 -11.250  -1.2063   0.02489   0.01792  -0.0031   1.0000   0.1686
 -11.000  -1.1910   0.02427   0.01720  -0.0017   1.0000   0.1775
 -10.750  -1.1748   0.02357   0.01652  -0.0004   1.0000   0.1850
 -10.500  -1.1566   0.02307   0.01593   0.0007   1.0000   0.1928
 -10.250  -1.1372   0.02245   0.01528   0.0016   1.0000   0.1996
 -10.000  -1.1171   0.02192   0.01475   0.0026   1.0000   0.2065
  -9.750  -1.0962   0.02151   0.01419   0.0035   1.0000   0.2131
  -9.500  -1.0746   0.02084   0.01365   0.0042   1.0000   0.2198
  -9.250  -1.0525   0.02040   0.01315   0.0049   1.0000   0.2266
  -9.000  -1.0299   0.01988   0.01260   0.0056   1.0000   0.2329
  -8.750  -1.0076   0.01937   0.01217   0.0063   1.0000   0.2397
  -8.500  -0.9848   0.01898   0.01170   0.0070   1.0000   0.2466
  -8.250  -0.9624   0.01845   0.01125   0.0077   1.0000   0.2535
  -8.000  -0.9406   0.01809   0.01092   0.0085   1.0000   0.2619
  -7.750  -0.9201   0.01770   0.01059   0.0095   1.0000   0.2712
  -7.500  -0.8885   0.01723   0.01014   0.0082   0.9754   0.2824
  -7.250  -0.8326   0.01667   0.00964   0.0021   0.9667   0.2942
  -7.000  -0.7738   0.01618   0.00908  -0.0046   0.9554   0.3068
  -6.750  -0.7203   0.01585   0.00876  -0.0103   0.9401   0.3210
  -6.500  -0.6791   0.01566   0.00861  -0.0133   0.9227   0.3342
  -6.250  -0.6537   0.01561   0.00853  -0.0127   0.9027   0.3474
  -6.000  -0.6317   0.01553   0.00845  -0.0113   0.8844   0.3609
  -5.750  -0.6108   0.01533   0.00830  -0.0096   0.8676   0.3738
  -5.500  -0.5893   0.01515   0.00806  -0.0081   0.8515   0.3876
  -5.250  -0.5667   0.01496   0.00790  -0.0067   0.8359   0.4004
  -5.000  -0.5433   0.01476   0.00770  -0.0054   0.8213   0.4126
  -4.750  -0.5196   0.01466   0.00750  -0.0042   0.8082   0.4255
  -4.500  -0.4947   0.01451   0.00738  -0.0032   0.7948   0.4364
  -4.250  -0.4698   0.01446   0.00722  -0.0023   0.7818   0.4481
  -4.000  -0.4433   0.01436   0.00712  -0.0017   0.7701   0.4576
  -3.750  -0.4178   0.01434   0.00703  -0.0009   0.7568   0.4681
  -3.500  -0.3909   0.01431   0.00696  -0.0003   0.7454   0.4771
  -3.250  -0.3653   0.01432   0.00694   0.0004   0.7323   0.4871
  -3.000  -0.3385   0.01434   0.00688   0.0010   0.7215   0.4962
  -2.750  -0.3122   0.01434   0.00691   0.0016   0.7094   0.5049
  -2.500  -0.2857   0.01442   0.00681   0.0023   0.6993   0.5142
  -2.250  -0.2588   0.01437   0.00686   0.0027   0.6874   0.5216
  -2.000  -0.2320   0.01444   0.00684   0.0033   0.6771   0.5309
  -1.750  -0.2057   0.01443   0.00682   0.0039   0.6658   0.5395
  -1.500  -0.1784   0.01445   0.00684   0.0044   0.6556   0.5475
  -1.250  -0.1520   0.01452   0.00684   0.0050   0.6457   0.5567
  -1.000  -0.1247   0.01447   0.00682   0.0054   0.6354   0.5647
  -0.750  -0.0973   0.01455   0.00684   0.0058   0.6267   0.5735
  -0.500  -0.0715   0.01455   0.00684   0.0065   0.6160   0.5838
  -0.250  -0.0440   0.01454   0.00687   0.0070   0.6071   0.5937
   0.000  -0.0184   0.01464   0.00692   0.0077   0.5975   0.6057
   0.250   0.0093   0.01451   0.00686   0.0082   0.5868   0.6149
   0.500   0.0362   0.01449   0.00680   0.0087   0.5763   0.6245
   0.750   0.0634   0.01437   0.00669   0.0091   0.5650   0.6335
   1.000   0.0913   0.01436   0.00666   0.0094   0.5563   0.6425
   1.250   0.1181   0.01435   0.00666   0.0099   0.5466   0.6523
   1.500   0.1468   0.01428   0.00662   0.0100   0.5385   0.6608
   1.750   0.1744   0.01431   0.00667   0.0103   0.5298   0.6706
   2.000   0.2023   0.01428   0.00668   0.0106   0.5209   0.6804
   2.500   0.2579   0.01437   0.00678   0.0111   0.5041   0.7003
   2.750   0.2866   0.01434   0.00681   0.0112   0.4954   0.7093
   3.000   0.3143   0.01443   0.00690   0.0114   0.4870   0.7203
   3.250   0.3425   0.01443   0.00700   0.0116   0.4777   0.7306
   3.500   0.3706   0.01455   0.00705   0.0118   0.4694   0.7425
   3.750   0.3983   0.01456   0.00721   0.0120   0.4595   0.7536
   4.000   0.4261   0.01463   0.00726   0.0123   0.4499   0.7662
   4.250   0.4537   0.01469   0.00742   0.0125   0.4395   0.7782
   4.500   0.4806   0.01476   0.00751   0.0130   0.4291   0.7930
   4.750   0.5071   0.01487   0.00772   0.0135   0.4180   0.8069
   5.000   0.5325   0.01498   0.00785   0.0143   0.4065   0.8217
   5.250   0.5562   0.01511   0.00807   0.0155   0.3934   0.8379
   5.500   0.5784   0.01530   0.00821   0.0169   0.3808   0.8552
   5.750   0.5993   0.01543   0.00840   0.0186   0.3665   0.8741
   6.000   0.6190   0.01560   0.00858   0.0205   0.3525   0.8953
   6.250   0.6427   0.01573   0.00863   0.0214   0.3388   0.9169
   6.500   0.6816   0.01580   0.00865   0.0188   0.3226   0.9371
   6.750   0.7427   0.01601   0.00888   0.0113   0.3045   0.9517
   7.000   0.8117   0.01643   0.00934   0.0021   0.2884   0.9609
   7.250   0.8735   0.01694   0.00986  -0.0053   0.2733   0.9694
   7.500   0.9072   0.01768   0.01046  -0.0071   0.2625   1.0000
   7.750   0.9319   0.01805   0.01084  -0.0070   0.2530   1.0000
   8.000   0.9562   0.01860   0.01128  -0.0067   0.2447   1.0000
   8.250   0.9814   0.01900   0.01173  -0.0066   0.2364   1.0000
   8.500   1.0056   0.01964   0.01223  -0.0064   0.2293   1.0000
   8.750   1.0308   0.02009   0.01277  -0.0063   0.2231   1.0000
   9.000   1.0554   0.02059   0.01328  -0.0061   0.2166   1.0000
   9.250   1.0793   0.02129   0.01389  -0.0059   0.2104   1.0000
   9.500   1.1035   0.02173   0.01446  -0.0056   0.2041   1.0000
   9.750   1.1264   0.02230   0.01501  -0.0053   0.1973   1.0000
  10.000   1.1491   0.02293   0.01567  -0.0049   0.1909   1.0000
  10.250   1.1711   0.02345   0.01628  -0.0045   0.1836   1.0000
  10.500   1.1914   0.02416   0.01697  -0.0040   0.1764   1.0000
  10.750   1.2115   0.02473   0.01765  -0.0034   0.1674   1.0000
  11.000   1.2298   0.02548   0.01847  -0.0028   0.1574   1.0000
  11.250   1.2453   0.02637   0.01939  -0.0019   0.1447   1.0000
  11.500   1.2536   0.02752   0.02055  -0.0003   0.1294   1.0000
  11.750   1.2545   0.02928   0.02225   0.0014   0.1144   1.0000
  12.000   1.2536   0.03160   0.02449   0.0024   0.1026   1.0000
  12.250   1.2536   0.03416   0.02703   0.0028   0.0942   1.0000
  12.500   1.2537   0.03693   0.02982   0.0028   0.0878   1.0000
  12.750   1.2513   0.04010   0.03296   0.0024   0.0839   1.0000
  13.000   1.2529   0.04292   0.03585   0.0021   0.0801   1.0000
  13.250   1.2510   0.04615   0.03907   0.0015   0.0775   1.0000
  13.500   1.2505   0.04922   0.04217   0.0012   0.0751   1.0000
  13.750   1.2521   0.05211   0.04514   0.0007   0.0730   1.0000
  14.000   1.2527   0.05509   0.04814   0.0003   0.0711   1.0000
  14.250   1.2532   0.05795   0.05094   0.0001   0.0695   1.0000
  14.500   1.2563   0.06064   0.05369  -0.0001   0.0680   1.0000
  14.750   1.2590   0.06344   0.05658  -0.0006   0.0666   1.0000
  15.000   1.2625   0.06613   0.05931  -0.0010   0.0651   1.0000
  15.250   1.2674   0.06861   0.06178  -0.0012   0.0638   1.0000
  15.500   1.2785   0.07005   0.06311  -0.0005   0.0624   1.0000
  15.750   1.2808   0.07307   0.06625  -0.0011   0.0613   1.0000
  16.000   1.2834   0.07608   0.06938  -0.0018   0.0603   1.0000
  16.250   1.2868   0.07899   0.07237  -0.0025   0.0593   1.0000
  16.500   1.2919   0.08163   0.07506  -0.0029   0.0584   1.0000
  16.750   1.2993   0.08390   0.07736  -0.0031   0.0576   1.0000
  17.000   1.3112   0.08544   0.07886  -0.0027   0.0567   1.0000
  17.250   1.3282   0.08620   0.07954  -0.0014   0.0558   1.0000
  17.500   1.3219   0.09067   0.08422  -0.0033   0.0553   1.0000
  17.750   1.3172   0.09495   0.08867  -0.0049   0.0549   1.0000
  18.000   1.3102   0.09966   0.09356  -0.0070   0.0544   1.0000
  18.250   1.3030   0.10449   0.09856  -0.0091   0.0540   1.0000
  18.500   1.2940   0.10972   0.10397  -0.0116   0.0535   1.0000
  18.750   1.2841   0.11516   0.10958  -0.0144   0.0530   1.0000
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