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SD7034 (sd7034-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: SD7034 (sd7034-il)
Reynolds number: 100,000
Max Cl/Cd: 57.56 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sd7034-il-100000-n5.txt
Download as CSV file: xf-sd7034-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD7034                                          
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.250  -0.3324   0.09764   0.09275  -0.0353   1.0000   0.0324
  -9.000  -0.3254   0.09474   0.08988  -0.0357   1.0000   0.0319
  -8.750  -0.3222   0.09132   0.08652  -0.0368   1.0000   0.0315
  -8.500  -0.3206   0.08796   0.08323  -0.0380   1.0000   0.0310
  -8.250  -0.3217   0.08458   0.07993  -0.0392   1.0000   0.0305
  -8.000  -0.3278   0.08146   0.07693  -0.0398   1.0000   0.0303
  -7.750  -0.3430   0.07946   0.07506  -0.0382   1.0000   0.0299
  -7.500  -0.3402   0.07465   0.07031  -0.0435   0.9870   0.0296
  -7.250  -0.3213   0.06697   0.06259  -0.0555   0.9740   0.0297
  -7.000  -0.3019   0.05818   0.05366  -0.0681   0.9610   0.0301
  -6.750  -0.2863   0.04798   0.04307  -0.0793   0.9477   0.0309
  -6.500  -0.2710   0.03985   0.03428  -0.0855   0.9356   0.0314
  -6.250  -0.2514   0.03351   0.02705  -0.0888   0.9259   0.0322
  -6.000  -0.2282   0.03030   0.02334  -0.0898   0.9168   0.0334
  -5.750  -0.2024   0.02924   0.02214  -0.0902   0.9084   0.0357
  -5.500  -0.1764   0.02694   0.01928  -0.0906   0.9004   0.0386
  -5.250  -0.1512   0.02489   0.01679  -0.0904   0.8917   0.0405
  -5.000  -0.1240   0.02404   0.01585  -0.0906   0.8843   0.0437
  -4.750  -0.0981   0.02279   0.01425  -0.0901   0.8756   0.0473
  -4.500  -0.0712   0.02161   0.01291  -0.0899   0.8684   0.0504
  -4.250  -0.0456   0.02094   0.01214  -0.0895   0.8596   0.0551
  -4.000  -0.0185   0.01997   0.01095  -0.0889   0.8525   0.0597
  -3.750   0.0067   0.01934   0.01034  -0.0885   0.8436   0.0656
  -3.500   0.0334   0.01864   0.00953  -0.0879   0.8365   0.0732
  -3.250   0.0589   0.01814   0.00898  -0.0874   0.8274   0.0828
  -3.000   0.0854   0.01762   0.00843  -0.0869   0.8204   0.0953
  -2.750   0.1110   0.01721   0.00802  -0.0864   0.8110   0.1109
  -2.500   0.1376   0.01675   0.00757  -0.0859   0.8041   0.1308
  -2.250   0.1632   0.01637   0.00726  -0.0855   0.7945   0.1568
  -2.000   0.1897   0.01591   0.00691  -0.0850   0.7875   0.1968
  -1.750   0.2151   0.01549   0.00672  -0.0846   0.7779   0.2624
  -1.500   0.2409   0.01499   0.00654  -0.0841   0.7703   0.3664
  -1.250   0.2653   0.01455   0.00648  -0.0833   0.7612   0.4910
  -1.000   0.2884   0.01411   0.00643  -0.0818   0.7531   0.6241
  -0.750   0.3089   0.01366   0.00638  -0.0792   0.7444   0.7702
  -0.500   0.3557   0.01324   0.00608  -0.0819   0.7357   1.0000
  -0.250   0.3823   0.01328   0.00592  -0.0815   0.7270   1.0000
   0.000   0.4085   0.01338   0.00585  -0.0811   0.7168   1.0000
   0.250   0.4353   0.01344   0.00573  -0.0806   0.7081   1.0000
   0.500   0.4617   0.01354   0.00570  -0.0802   0.6978   1.0000
   0.750   0.4882   0.01364   0.00567  -0.0798   0.6877   1.0000
   1.000   0.5152   0.01371   0.00558  -0.0794   0.6787   1.0000
   1.250   0.5415   0.01384   0.00562  -0.0790   0.6674   1.0000
   1.500   0.5680   0.01396   0.00565  -0.0786   0.6567   1.0000
   1.750   0.5949   0.01405   0.00562  -0.0781   0.6469   1.0000
   2.000   0.6213   0.01419   0.00569  -0.0777   0.6354   1.0000
   2.250   0.6477   0.01434   0.00578  -0.0774   0.6239   1.0000
   2.500   0.6742   0.01448   0.00584  -0.0769   0.6128   1.0000
   2.750   0.7008   0.01462   0.00588  -0.0765   0.6019   1.0000
   3.000   0.7268   0.01480   0.00604  -0.0761   0.5892   1.0000
   3.250   0.7529   0.01498   0.00618  -0.0757   0.5768   1.0000
   3.500   0.7790   0.01517   0.00632  -0.0752   0.5644   1.0000
   3.750   0.8050   0.01536   0.00648  -0.0748   0.5520   1.0000
   4.000   0.8309   0.01557   0.00663  -0.0743   0.5394   1.0000
   4.250   0.8565   0.01580   0.00683  -0.0738   0.5260   1.0000
   4.500   0.8818   0.01605   0.00709  -0.0733   0.5123   1.0000
   4.750   0.9071   0.01632   0.00734  -0.0729   0.4986   1.0000
   5.000   0.9321   0.01660   0.00760  -0.0723   0.4847   1.0000
   5.250   0.9569   0.01689   0.00791  -0.0718   0.4707   1.0000
   5.500   0.9815   0.01721   0.00821  -0.0712   0.4564   1.0000
   5.750   1.0057   0.01755   0.00854  -0.0706   0.4421   1.0000
   6.000   1.0297   0.01791   0.00890  -0.0700   0.4276   1.0000
   6.250   1.0533   0.01830   0.00930  -0.0693   0.4130   1.0000
   6.500   1.0765   0.01871   0.00971  -0.0686   0.3983   1.0000
   6.750   1.0994   0.01914   0.01015  -0.0679   0.3837   1.0000
   7.000   1.1218   0.01960   0.01063  -0.0671   0.3690   1.0000
   7.250   1.1437   0.02009   0.01114  -0.0663   0.3542   1.0000
   7.500   1.1651   0.02061   0.01167  -0.0655   0.3397   1.0000
   7.750   1.1859   0.02116   0.01224  -0.0645   0.3251   1.0000
   8.000   1.2060   0.02174   0.01285  -0.0635   0.3106   1.0000
   8.250   1.2253   0.02236   0.01349  -0.0625   0.2960   1.0000
   8.500   1.2437   0.02302   0.01417  -0.0613   0.2814   1.0000
   8.750   1.2612   0.02371   0.01490  -0.0601   0.2667   1.0000
   9.000   1.2777   0.02445   0.01569  -0.0587   0.2521   1.0000
   9.250   1.2931   0.02523   0.01652  -0.0573   0.2378   1.0000
   9.500   1.3072   0.02606   0.01739  -0.0557   0.2238   1.0000
   9.750   1.3198   0.02695   0.01833  -0.0540   0.2102   1.0000
  10.000   1.3298   0.02788   0.01933  -0.0520   0.1972   1.0000
  10.250   1.3382   0.02891   0.02042  -0.0499   0.1847   1.0000
  10.500   1.3456   0.03007   0.02162  -0.0479   0.1727   1.0000
  10.750   1.3518   0.03136   0.02296  -0.0460   0.1613   1.0000
  11.000   1.3563   0.03284   0.02445  -0.0442   0.1503   1.0000
  11.250   1.3606   0.03444   0.02611  -0.0425   0.1394   1.0000
  11.500   1.3647   0.03615   0.02792  -0.0411   0.1291   1.0000
  11.750   1.3670   0.03809   0.02992  -0.0398   0.1199   1.0000
  12.000   1.3667   0.04034   0.03218  -0.0386   0.1120   1.0000
  12.250   1.3690   0.04252   0.03447  -0.0377   0.1038   1.0000
  12.500   1.3675   0.04511   0.03710  -0.0370   0.0973   1.0000
  12.750   1.3673   0.04771   0.03982  -0.0364   0.0907   1.0000
  13.000   1.3638   0.05074   0.04287  -0.0361   0.0859   1.0000
  13.250   1.3631   0.05363   0.04592  -0.0359   0.0804   1.0000
  13.500   1.3581   0.05706   0.04940  -0.0360   0.0764   1.0000
  13.750   1.3553   0.06038   0.05286  -0.0362   0.0723   1.0000
  14.000   1.3520   0.06389   0.05651  -0.0366   0.0686   1.0000
  14.250   1.3463   0.06779   0.06048  -0.0373   0.0657   1.0000
  14.500   1.3420   0.07166   0.06445  -0.0380   0.0628   1.0000
  14.750   1.3386   0.07558   0.06855  -0.0389   0.0598   1.0000
  15.000   1.3335   0.07984   0.07293  -0.0401   0.0572   1.0000
  15.250   1.3279   0.08422   0.07737  -0.0415   0.0551   1.0000
  15.500   1.3238   0.08849   0.08175  -0.0427   0.0529   1.0000
  15.750   1.3191   0.09305   0.08651  -0.0443   0.0507   1.0000
  16.000   1.3140   0.09776   0.09136  -0.0461   0.0488   1.0000
  16.250   1.3086   0.10255   0.09625  -0.0480   0.0470   1.0000
  16.500   1.3054   0.10683   0.10056  -0.0497   0.0454   1.0000
  16.750   1.3000   0.11187   0.10579  -0.0518   0.0440   1.0000
  17.000   1.2923   0.11753   0.11168  -0.0545   0.0426   1.0000
  17.250   1.2843   0.12336   0.11770  -0.0574   0.0413   1.0000
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