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AVISTAR (avistar-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: AVISTAR (avistar-il)
Reynolds number: 1,000,000
Max Cl/Cd: 71.44 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-avistar-il-1000000-n5.txt
Download as CSV file: xf-avistar-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AVISTAR                                         
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -1.0117   0.08044   0.07788  -0.0462   1.0000   0.0174
 -16.750  -1.0736   0.06588   0.06302  -0.0558   1.0000   0.0174
 -16.500  -1.1020   0.05773   0.05466  -0.0612   1.0000   0.0174
 -16.250  -1.1215   0.05143   0.04817  -0.0651   1.0000   0.0174
 -16.000  -1.1341   0.04655   0.04313  -0.0677   1.0000   0.0175
 -15.750  -1.1427   0.04256   0.03898  -0.0694   1.0000   0.0175
 -15.500  -1.1491   0.03910   0.03538  -0.0705   1.0000   0.0176
 -15.250  -1.1525   0.03624   0.03240  -0.0709   1.0000   0.0177
 -15.000  -1.1523   0.03394   0.03000  -0.0708   1.0000   0.0178
 -14.750  -1.1486   0.03215   0.02813  -0.0703   1.0000   0.0179
 -14.500  -1.1443   0.03056   0.02644  -0.0693   1.0000   0.0179
 -14.250  -1.1361   0.02939   0.02521  -0.0682   1.0000   0.0181
 -14.000  -1.1275   0.02831   0.02407  -0.0669   1.0000   0.0182
 -13.750  -1.1175   0.02742   0.02312  -0.0654   1.0000   0.0183
 -13.500  -1.1069   0.02663   0.02227  -0.0636   1.0000   0.0184
 -13.250  -1.0962   0.02589   0.02147  -0.0617   1.0000   0.0185
 -13.000  -1.0855   0.02523   0.02077  -0.0595   1.0000   0.0186
 -12.750  -1.0757   0.02454   0.02001  -0.0571   0.9995   0.0187
 -12.500  -1.0533   0.02373   0.01913  -0.0572   0.9863   0.0189
 -12.250  -1.0299   0.02291   0.01822  -0.0574   0.9679   0.0191
 -12.000  -1.0093   0.02216   0.01736  -0.0568   0.9436   0.0192
 -11.750  -0.9931   0.02151   0.01657  -0.0551   0.9205   0.0194
 -11.500  -0.9758   0.02089   0.01581  -0.0536   0.9038   0.0196
 -11.000  -0.9378   0.01966   0.01434  -0.0512   0.8816   0.0200
 -10.750  -0.9178   0.01908   0.01364  -0.0502   0.8726   0.0201
 -10.500  -0.8967   0.01851   0.01297  -0.0493   0.8652   0.0203
 -10.250  -0.8751   0.01800   0.01236  -0.0484   0.8578   0.0204
 -10.000  -0.8531   0.01752   0.01178  -0.0476   0.8506   0.0205
  -9.750  -0.8321   0.01689   0.01108  -0.0467   0.8423   0.0208
  -9.500  -0.8100   0.01643   0.01054  -0.0458   0.8338   0.0210
  -9.250  -0.7865   0.01604   0.01011  -0.0452   0.8269   0.0212
  -9.000  -0.7625   0.01571   0.00973  -0.0447   0.8194   0.0214
  -8.750  -0.7379   0.01544   0.00941  -0.0442   0.8126   0.0216
  -8.500  -0.7133   0.01513   0.00906  -0.0437   0.8056   0.0219
  -8.250  -0.6886   0.01482   0.00870  -0.0432   0.7993   0.0221
  -8.000  -0.6641   0.01448   0.00830  -0.0427   0.7949   0.0224
  -7.750  -0.6393   0.01412   0.00790  -0.0423   0.7906   0.0227
  -7.500  -0.6144   0.01377   0.00751  -0.0418   0.7855   0.0229
  -7.250  -0.5896   0.01345   0.00712  -0.0413   0.7802   0.0232
  -7.000  -0.5645   0.01313   0.00675  -0.0408   0.7754   0.0235
  -6.750  -0.5390   0.01283   0.00641  -0.0404   0.7710   0.0237
  -6.500  -0.5135   0.01255   0.00608  -0.0401   0.7660   0.0239
  -6.250  -0.4887   0.01221   0.00570  -0.0395   0.7610   0.0242
  -6.000  -0.4633   0.01192   0.00539  -0.0391   0.7564   0.0246
  -5.750  -0.4370   0.01169   0.00516  -0.0388   0.7509   0.0249
  -5.500  -0.4109   0.01148   0.00492  -0.0385   0.7446   0.0253
  -5.250  -0.3848   0.01127   0.00468  -0.0382   0.7386   0.0256
  -5.000  -0.3584   0.01106   0.00444  -0.0379   0.7324   0.0260
  -4.750  -0.3322   0.01085   0.00421  -0.0376   0.7257   0.0264
  -4.500  -0.3058   0.01066   0.00398  -0.0373   0.7193   0.0268
  -4.250  -0.2792   0.01048   0.00376  -0.0370   0.7119   0.0271
  -4.000  -0.2528   0.01032   0.00356  -0.0367   0.7039   0.0275
  -3.750  -0.2262   0.01013   0.00335  -0.0364   0.6956   0.0278
  -3.500  -0.2002   0.00996   0.00314  -0.0360   0.6855   0.0284
  -3.250  -0.1734   0.00983   0.00299  -0.0358   0.6740   0.0290
  -3.000  -0.1467   0.00973   0.00285  -0.0356   0.6620   0.0297
  -2.750  -0.1201   0.00964   0.00271  -0.0353   0.6490   0.0303
  -2.500  -0.0934   0.00955   0.00258  -0.0350   0.6356   0.0308
  -2.250  -0.0667   0.00947   0.00246  -0.0348   0.6221   0.0314
  -2.000  -0.0400   0.00940   0.00234  -0.0345   0.6086   0.0320
  -1.750  -0.0137   0.00933   0.00222  -0.0342   0.5951   0.0329
  -1.500   0.0130   0.00928   0.00214  -0.0339   0.5820   0.0338
  -1.250   0.0399   0.00924   0.00207  -0.0337   0.5698   0.0349
  -1.000   0.0668   0.00922   0.00200  -0.0335   0.5582   0.0361
  -0.750   0.0935   0.00919   0.00194  -0.0332   0.5461   0.0373
  -0.500   0.1202   0.00916   0.00188  -0.0330   0.5344   0.0388
  -0.250   0.1469   0.00916   0.00184  -0.0327   0.5224   0.0405
   0.000   0.1738   0.00915   0.00181  -0.0325   0.5120   0.0422
   0.250   0.2007   0.00912   0.00178  -0.0323   0.5040   0.0454
   0.500   0.2278   0.00910   0.00175  -0.0321   0.4965   0.0498
   0.750   0.2544   0.00907   0.00173  -0.0318   0.4891   0.0607
   1.000   0.2697   0.00802   0.00159  -0.0296   0.4836   0.3644
   1.250   0.2932   0.00775   0.00159  -0.0288   0.4772   0.4551
   1.500   0.3166   0.00751   0.00160  -0.0280   0.4713   0.5374
   1.750   0.3395   0.00724   0.00164  -0.0269   0.4659   0.6328
   2.000   0.3641   0.00717   0.00169  -0.0262   0.4588   0.6841
   2.250   0.3895   0.00716   0.00174  -0.0257   0.4495   0.7140
   2.750   0.4398   0.00716   0.00185  -0.0245   0.4257   0.7711
   3.000   0.4640   0.00717   0.00193  -0.0237   0.4110   0.8045
   3.250   0.4875   0.00714   0.00204  -0.0227   0.3928   0.8666
   3.500   0.5156   0.00731   0.00215  -0.0228   0.3620   0.9032
   3.750   0.5443   0.00787   0.00242  -0.0236   0.2926   0.9206
   4.000   0.5877   0.00842   0.00275  -0.0277   0.2420   0.9326
   4.250   0.6391   0.00919   0.00318  -0.0338   0.1743   0.9402
   4.500   0.6834   0.01075   0.00413  -0.0388   0.0321   0.9485
   4.750   0.7325   0.01109   0.00443  -0.0439   0.0273   0.9555
   5.000   0.7762   0.01141   0.00473  -0.0476   0.0250   0.9635
   5.250   0.7944   0.01176   0.00506  -0.0456   0.0237   0.9951
   5.500   0.8306   0.01206   0.00533  -0.0477   0.0223   0.9978
   5.750   0.8650   0.01232   0.00558  -0.0494   0.0213   0.9994
   6.000   0.8944   0.01258   0.00582  -0.0500   0.0204   1.0000
   6.250   0.9166   0.01285   0.00608  -0.0491   0.0197   1.0000
   6.500   0.9382   0.01316   0.00637  -0.0480   0.0191   1.0000
   6.750   0.9600   0.01345   0.00666  -0.0469   0.0187   1.0000
   7.000   0.9816   0.01374   0.00696  -0.0459   0.0183   1.0000
   7.250   1.0029   0.01405   0.00727  -0.0448   0.0180   1.0000
   7.500   1.0238   0.01437   0.00759  -0.0436   0.0176   1.0000
   7.750   1.0444   0.01471   0.00794  -0.0424   0.0173   1.0000
   8.000   1.0645   0.01506   0.00830  -0.0411   0.0169   1.0000
   8.250   1.0841   0.01544   0.00868  -0.0398   0.0167   1.0000
   8.500   1.1029   0.01585   0.00910  -0.0383   0.0164   1.0000
   8.750   1.1207   0.01632   0.00958  -0.0367   0.0161   1.0000
   9.000   1.1365   0.01686   0.01014  -0.0348   0.0158   1.0000
   9.250   1.1504   0.01735   0.01065  -0.0325   0.0157   1.0000
   9.500   1.1618   0.01781   0.01115  -0.0297   0.0156   1.0000
   9.750   1.1736   0.01832   0.01170  -0.0272   0.0154   1.0000
  10.000   1.1862   0.01888   0.01229  -0.0250   0.0153   1.0000
  10.250   1.1991   0.01949   0.01294  -0.0229   0.0151   1.0000
  10.500   1.2123   0.02015   0.01363  -0.0211   0.0149   1.0000
  10.750   1.2250   0.02087   0.01439  -0.0193   0.0147   1.0000
  11.000   1.2372   0.02169   0.01524  -0.0176   0.0146   1.0000
  11.250   1.2490   0.02258   0.01617  -0.0159   0.0144   1.0000
  11.500   1.2606   0.02352   0.01716  -0.0144   0.0143   1.0000
  11.750   1.2719   0.02453   0.01821  -0.0130   0.0141   1.0000
  12.000   1.2827   0.02562   0.01934  -0.0116   0.0140   1.0000
  12.250   1.2928   0.02680   0.02057  -0.0103   0.0139   1.0000
  12.500   1.3026   0.02805   0.02186  -0.0091   0.0138   1.0000
  12.750   1.3116   0.02940   0.02326  -0.0079   0.0137   1.0000
  13.000   1.3197   0.03087   0.02477  -0.0068   0.0136   1.0000
  13.250   1.3272   0.03245   0.02640  -0.0058   0.0135   1.0000
  13.500   1.3331   0.03420   0.02821  -0.0048   0.0134   1.0000
  13.750   1.3378   0.03611   0.03017  -0.0038   0.0133   1.0000
  14.000   1.3411   0.03822   0.03234  -0.0030   0.0132   1.0000
  14.250   1.3420   0.04062   0.03481  -0.0022   0.0131   1.0000
  14.500   1.3417   0.04321   0.03747  -0.0016   0.0130   1.0000
  14.750   1.3424   0.04581   0.04016  -0.0011   0.0129   1.0000
  15.000   1.3458   0.04822   0.04263  -0.0009   0.0129   1.0000
  15.250   1.3486   0.05075   0.04523  -0.0008   0.0128   1.0000
  15.500   1.3510   0.05338   0.04794  -0.0007   0.0128   1.0000
  15.750   1.3523   0.05619   0.05083  -0.0008   0.0127   1.0000
  16.000   1.3537   0.05905   0.05376  -0.0009   0.0127   1.0000
  16.250   1.3547   0.06200   0.05679  -0.0012   0.0126   1.0000
  16.500   1.3548   0.06506   0.05993  -0.0014   0.0126   1.0000
  16.750   1.3553   0.06814   0.06308  -0.0018   0.0125   1.0000
  17.000   1.3551   0.07132   0.06634  -0.0022   0.0125   1.0000
  17.250   1.3543   0.07463   0.06972  -0.0028   0.0124   1.0000
  17.750   1.3526   0.08128   0.07653  -0.0039   0.0123   1.0000
  18.000   1.3514   0.08475   0.08009  -0.0047   0.0123   1.0000
  18.250   1.3502   0.08824   0.08365  -0.0055   0.0122   1.0000
  18.500   1.3488   0.09177   0.08726  -0.0063   0.0121   1.0000
  18.750   1.3466   0.09545   0.09102  -0.0073   0.0120   1.0000
  19.000   1.3451   0.09906   0.09470  -0.0083   0.0119   1.0000
  19.250   1.3423   0.10291   0.09863  -0.0094   0.0119   1.0000
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