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WASP (smoothed) (waspsm-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: WASP (smoothed) (waspsm-il)
Reynolds number: 200,000
Max Cl/Cd: 69.71 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-waspsm-il-200000.txt
Download as CSV file: xf-waspsm-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WASP (smoothed)                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -8.750  -0.4212   0.09706   0.09349  -0.0268   1.0000   0.0498
  -8.500  -0.4284   0.09349   0.09000  -0.0307   1.0000   0.0502
  -8.250  -0.4343   0.08986   0.08643  -0.0336   1.0000   0.0503
  -8.000  -0.4394   0.08376   0.08040  -0.0377   1.0000   0.0507
  -7.750  -0.4317   0.08123   0.07789  -0.0315   1.0000   0.0519
  -7.500  -0.4251   0.07879   0.07548  -0.0302   1.0000   0.0530
  -7.250  -0.4210   0.07588   0.07260  -0.0306   1.0000   0.0542
  -7.000  -0.4180   0.07256   0.06931  -0.0321   1.0000   0.0559
  -6.750  -0.4160   0.06865   0.06543  -0.0348   1.0000   0.0583
  -6.500  -0.4202   0.06160   0.05802  -0.0448   1.0000   0.0624
  -6.250  -0.4242   0.05565   0.05204  -0.0446   1.0000   0.0636
  -6.000  -0.4158   0.05436   0.05092  -0.0413   1.0000   0.0652
  -5.750  -0.4088   0.05262   0.04920  -0.0394   1.0000   0.0671
  -5.500  -0.4018   0.04980   0.04629  -0.0388   1.0000   0.0697
  -5.250  -0.3961   0.04413   0.03999  -0.0408   1.0000   0.0771
  -5.000  -0.3828   0.03294   0.02809  -0.0404   1.0000   0.0476
  -4.750  -0.3544   0.02471   0.01850  -0.0413   0.9981   0.0409
  -4.500  -0.3155   0.02313   0.01679  -0.0443   0.9940   0.0440
  -4.250  -0.2764   0.02124   0.01451  -0.0465   0.9892   0.0469
  -4.000  -0.2372   0.01946   0.01231  -0.0485   0.9844   0.0490
  -3.750  -0.1983   0.01776   0.01041  -0.0508   0.9797   0.0535
  -3.500  -0.1592   0.01677   0.00931  -0.0529   0.9739   0.0582
  -3.250  -0.1187   0.01568   0.00810  -0.0552   0.9687   0.0644
  -3.000  -0.0789   0.01487   0.00730  -0.0576   0.9630   0.0735
  -2.750  -0.0395   0.01400   0.00647  -0.0598   0.9566   0.0863
  -2.500   0.0042   0.01315   0.00573  -0.0629   0.9529   0.1098
  -2.250   0.0398   0.01245   0.00522  -0.0644   0.9440   0.1534
  -2.000   0.0821   0.01154   0.00480  -0.0675   0.9391   0.2623
  -1.750   0.1125   0.01081   0.00462  -0.0680   0.9277   0.4081
  -1.500   0.1409   0.01012   0.00450  -0.0678   0.9160   0.5669
  -1.250   0.2401   0.00879   0.00421  -0.0822   0.9192   1.0000
  -1.000   0.2753   0.00871   0.00396  -0.0833   0.9037   1.0000
  -0.750   0.3074   0.00865   0.00374  -0.0838   0.8863   1.0000
  -0.500   0.3381   0.00861   0.00354  -0.0840   0.8683   1.0000
  -0.250   0.3676   0.00860   0.00338  -0.0839   0.8494   1.0000
   0.000   0.3944   0.00863   0.00326  -0.0833   0.8280   1.0000
   0.250   0.4220   0.00868   0.00315  -0.0828   0.8072   1.0000
   0.500   0.4477   0.00876   0.00309  -0.0819   0.7847   1.0000
   0.750   0.4736   0.00888   0.00304  -0.0811   0.7626   1.0000
   1.000   0.4985   0.00901   0.00303  -0.0802   0.7396   1.0000
   1.250   0.5234   0.00916   0.00302  -0.0792   0.7171   1.0000
   1.500   0.5477   0.00932   0.00306  -0.0782   0.6939   1.0000
   1.750   0.5722   0.00951   0.00309  -0.0772   0.6719   1.0000
   2.000   0.5963   0.00969   0.00316  -0.0762   0.6492   1.0000
   2.250   0.6204   0.00990   0.00323  -0.0752   0.6277   1.0000
   2.500   0.6444   0.01011   0.00334  -0.0742   0.6061   1.0000
   2.750   0.6684   0.01033   0.00345  -0.0732   0.5854   1.0000
   3.000   0.6924   0.01058   0.00357  -0.0723   0.5662   1.0000
   3.250   0.7164   0.01081   0.00374  -0.0713   0.5463   1.0000
   3.500   0.7404   0.01106   0.00391  -0.0704   0.5277   1.0000
   3.750   0.7644   0.01133   0.00409  -0.0695   0.5100   1.0000
   4.000   0.7884   0.01160   0.00429  -0.0686   0.4930   1.0000
   4.250   0.8123   0.01189   0.00452  -0.0678   0.4762   1.0000
   4.500   0.8363   0.01216   0.00476  -0.0669   0.4595   1.0000
   4.750   0.8601   0.01244   0.00501  -0.0660   0.4430   1.0000
   5.000   0.8839   0.01274   0.00527  -0.0651   0.4265   1.0000
   5.250   0.9075   0.01304   0.00557  -0.0643   0.4104   1.0000
   5.500   0.9310   0.01336   0.00587  -0.0634   0.3945   1.0000
   5.750   0.9543   0.01369   0.00619  -0.0624   0.3784   1.0000
   6.000   0.9774   0.01404   0.00652  -0.0615   0.3625   1.0000
   6.250   1.0005   0.01442   0.00690  -0.0606   0.3470   1.0000
   6.500   1.0232   0.01481   0.00727  -0.0596   0.3314   1.0000
   6.750   1.0458   0.01522   0.00768  -0.0586   0.3161   1.0000
   7.000   1.0678   0.01564   0.00808  -0.0576   0.3002   1.0000
   7.250   1.0890   0.01600   0.00846  -0.0564   0.2810   1.0000
   7.500   1.1102   0.01636   0.00883  -0.0553   0.2613   1.0000
   7.750   1.1313   0.01680   0.00926  -0.0541   0.2446   1.0000
   8.000   1.1521   0.01726   0.00973  -0.0530   0.2287   1.0000
   8.250   1.1724   0.01776   0.01023  -0.0518   0.2126   1.0000
   8.500   1.1929   0.01823   0.01076  -0.0507   0.1956   1.0000
   8.750   1.2130   0.01873   0.01130  -0.0495   0.1759   1.0000
   9.000   1.2315   0.01936   0.01191  -0.0482   0.1516   1.0000
   9.250   1.2453   0.02044   0.01277  -0.0462   0.1056   1.0000
   9.500   1.2495   0.02244   0.01438  -0.0430   0.0639   1.0000
   9.750   1.2565   0.02407   0.01600  -0.0400   0.0520   1.0000
  10.000   1.2627   0.02562   0.01757  -0.0371   0.0456   1.0000
  10.250   1.2683   0.02705   0.01910  -0.0339   0.0417   1.0000
  10.500   1.2734   0.02840   0.02054  -0.0308   0.0388   1.0000
  10.750   1.2752   0.03004   0.02223  -0.0277   0.0367   1.0000
  11.000   1.2718   0.03241   0.02462  -0.0243   0.0350   1.0000
  11.250   1.2785   0.03404   0.02639  -0.0221   0.0338   1.0000
  11.500   1.2852   0.03572   0.02821  -0.0201   0.0324   1.0000
  11.750   1.2909   0.03750   0.03011  -0.0183   0.0308   1.0000
  12.000   1.2958   0.03940   0.03210  -0.0167   0.0294   1.0000
  12.250   1.3007   0.04156   0.03431  -0.0152   0.0284   1.0000
  12.500   1.3078   0.04427   0.03707  -0.0135   0.0274   1.0000
  12.750   1.3144   0.04746   0.04044  -0.0120   0.0267   1.0000
  13.000   1.3156   0.04995   0.04316  -0.0106   0.0263   1.0000
  13.250   1.3145   0.05273   0.04617  -0.0096   0.0259   1.0000
  13.500   1.3110   0.05579   0.04946  -0.0088   0.0255   1.0000
  13.750   1.3055   0.05916   0.05306  -0.0084   0.0250   1.0000
  14.000   1.2981   0.06287   0.05699  -0.0084   0.0246   1.0000
  14.250   1.2890   0.06692   0.06125  -0.0089   0.0242   1.0000
  14.500   1.2782   0.07136   0.06591  -0.0099   0.0239   1.0000
  14.750   1.2655   0.07628   0.07104  -0.0113   0.0237   1.0000
  15.000   1.2506   0.08176   0.07673  -0.0133   0.0236   1.0000
  15.250   1.2329   0.08790   0.08308  -0.0160   0.0236   1.0000
  15.500   1.2132   0.09478   0.09019  -0.0194   0.0237   1.0000
  15.750   1.1914   0.10247   0.09809  -0.0236   0.0238   1.0000
  16.000   1.1677   0.11103   0.10685  -0.0286   0.0241   1.0000
  16.250   1.1420   0.12063   0.11664  -0.0345   0.0245   1.0000
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