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SD7037-092-88 (sd7037-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: SD7037-092-88 (sd7037-il)
Reynolds number: 100,000
Max Cl/Cd: 55.44 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sd7037-il-100000-n5.txt
Download as CSV file: xf-sd7037-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD7037-092-88                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -8.250  -0.3778   0.08804   0.08314  -0.0346   1.0000   0.0384
  -8.000  -0.3935   0.08256   0.07776  -0.0371   1.0000   0.0316
  -7.750  -0.3982   0.08013   0.07541  -0.0359   1.0000   0.0309
  -7.500  -0.4064   0.07740   0.07277  -0.0354   1.0000   0.0303
  -7.250  -0.4137   0.07407   0.06952  -0.0362   1.0000   0.0296
  -7.000  -0.4208   0.07021   0.06570  -0.0376   1.0000   0.0288
  -6.750  -0.4379   0.05831   0.05353  -0.0458   1.0000   0.0255
  -6.500  -0.4362   0.05510   0.05026  -0.0455   1.0000   0.0253
  -6.250  -0.4323   0.05162   0.04667  -0.0455   1.0000   0.0250
  -6.000  -0.4260   0.04769   0.04255  -0.0458   1.0000   0.0247
  -5.750  -0.4007   0.04230   0.03673  -0.0501   0.9957   0.0243
  -5.500  -0.3709   0.03712   0.03098  -0.0541   0.9904   0.0240
  -5.250  -0.3383   0.03280   0.02603  -0.0573   0.9858   0.0240
  -5.000  -0.3064   0.02942   0.02202  -0.0593   0.9809   0.0242
  -4.750  -0.2723   0.02685   0.01877  -0.0611   0.9761   0.0254
  -4.500  -0.2373   0.02509   0.01680  -0.0632   0.9721   0.0271
  -4.250  -0.2063   0.02352   0.01496  -0.0641   0.9660   0.0281
  -4.000  -0.1709   0.02201   0.01320  -0.0656   0.9614   0.0294
  -3.750  -0.1367   0.02078   0.01176  -0.0668   0.9564   0.0307
  -3.500  -0.1043   0.01971   0.01056  -0.0676   0.9500   0.0327
  -3.250  -0.0669   0.01889   0.00973  -0.0697   0.9455   0.0380
  -3.000  -0.0364   0.01812   0.00888  -0.0703   0.9379   0.0447
  -2.750   0.0000   0.01724   0.00799  -0.0719   0.9324   0.0637
  -2.500   0.0318   0.01634   0.00750  -0.0730   0.9254   0.1361
  -2.250   0.0635   0.01544   0.00722  -0.0742   0.9183   0.2743
  -2.000   0.0943   0.01477   0.00699  -0.0748   0.9109   0.4076
  -1.750   0.1228   0.01413   0.00687  -0.0746   0.9029   0.5627
  -1.500   0.1473   0.01366   0.00679  -0.0730   0.8938   0.7016
  -1.250   0.1749   0.01328   0.00664  -0.0716   0.8862   0.8240
  -1.000   0.2211   0.01297   0.00634  -0.0743   0.8784   0.9529
  -0.750   0.2640   0.01280   0.00597  -0.0771   0.8705   1.0000
  -0.500   0.2911   0.01276   0.00577  -0.0767   0.8578   1.0000
  -0.250   0.3190   0.01272   0.00558  -0.0765   0.8451   1.0000
   0.000   0.3472   0.01268   0.00540  -0.0763   0.8322   1.0000
   0.250   0.3756   0.01264   0.00524  -0.0761   0.8188   1.0000
   0.500   0.4038   0.01261   0.00509  -0.0758   0.8045   1.0000
   0.750   0.4319   0.01258   0.00496  -0.0755   0.7894   1.0000
   1.000   0.4600   0.01258   0.00485  -0.0752   0.7735   1.0000
   1.250   0.4879   0.01258   0.00475  -0.0748   0.7569   1.0000
   1.500   0.5158   0.01261   0.00468  -0.0744   0.7395   1.0000
   2.000   0.5700   0.01277   0.00464  -0.0735   0.7018   1.0000
   2.250   0.5966   0.01288   0.00467  -0.0729   0.6817   1.0000
   2.750   0.6491   0.01320   0.00480  -0.0718   0.6402   1.0000
   3.000   0.6750   0.01340   0.00490  -0.0712   0.6190   1.0000
   3.250   0.7005   0.01362   0.00506  -0.0705   0.5973   1.0000
   3.500   0.7259   0.01387   0.00523  -0.0699   0.5752   1.0000
   3.750   0.7510   0.01413   0.00542  -0.0692   0.5532   1.0000
   4.000   0.7758   0.01442   0.00566  -0.0685   0.5306   1.0000
   4.250   0.8004   0.01472   0.00590  -0.0679   0.5083   1.0000
   4.500   0.8248   0.01505   0.00617  -0.0671   0.4856   1.0000
   4.750   0.8489   0.01540   0.00646  -0.0664   0.4630   1.0000
   5.000   0.8728   0.01577   0.00681  -0.0657   0.4403   1.0000
   5.250   0.8964   0.01617   0.00717  -0.0649   0.4176   1.0000
   5.500   0.9197   0.01659   0.00755  -0.0641   0.3951   1.0000
   5.750   0.9428   0.01704   0.00797  -0.0633   0.3727   1.0000
   6.000   0.9654   0.01752   0.00844  -0.0625   0.3507   1.0000
   6.250   0.9879   0.01802   0.00893  -0.0617   0.3289   1.0000
   6.500   1.0100   0.01855   0.00945  -0.0608   0.3077   1.0000
   6.750   1.0315   0.01913   0.01002  -0.0599   0.2873   1.0000
   7.000   1.0531   0.01971   0.01062  -0.0590   0.2672   1.0000
   7.250   1.0739   0.02035   0.01126  -0.0580   0.2479   1.0000
   7.500   1.0942   0.02103   0.01193  -0.0570   0.2298   1.0000
   7.750   1.1144   0.02171   0.01268  -0.0560   0.2115   1.0000
   8.000   1.1339   0.02244   0.01344  -0.0549   0.1941   1.0000
   8.250   1.1527   0.02322   0.01425  -0.0538   0.1778   1.0000
   8.500   1.1708   0.02405   0.01512  -0.0525   0.1624   1.0000
   8.750   1.1882   0.02492   0.01604  -0.0513   0.1481   1.0000
   9.000   1.2049   0.02584   0.01704  -0.0499   0.1346   1.0000
   9.250   1.2204   0.02682   0.01809  -0.0484   0.1212   1.0000
   9.500   1.2340   0.02787   0.01913  -0.0469   0.1061   1.0000
   9.750   1.2478   0.02890   0.02022  -0.0454   0.0881   1.0000
  10.000   1.2585   0.03010   0.02138  -0.0436   0.0722   1.0000
  10.250   1.2671   0.03138   0.02271  -0.0415   0.0613   1.0000
  10.500   1.2738   0.03284   0.02426  -0.0393   0.0521   1.0000
  10.750   1.2776   0.03454   0.02603  -0.0369   0.0449   1.0000
  11.000   1.2776   0.03656   0.02810  -0.0346   0.0393   1.0000
  11.250   1.2787   0.03861   0.03031  -0.0325   0.0348   1.0000
  11.500   1.2766   0.04097   0.03275  -0.0306   0.0318   1.0000
  11.750   1.2741   0.04352   0.03545  -0.0291   0.0294   1.0000
  12.000   1.2723   0.04617   0.03828  -0.0280   0.0273   1.0000
  12.250   1.2689   0.04909   0.04134  -0.0273   0.0256   1.0000
  12.500   1.2634   0.05243   0.04481  -0.0270   0.0247   1.0000
  12.750   1.2567   0.05612   0.04863  -0.0271   0.0239   1.0000
  13.000   1.2522   0.05982   0.05256  -0.0274   0.0232   1.0000
  13.250   1.2468   0.06380   0.05675  -0.0280   0.0225   1.0000
  13.500   1.2409   0.06801   0.06115  -0.0290   0.0220   1.0000
  13.750   1.2342   0.07254   0.06586  -0.0303   0.0215   1.0000
  14.000   1.2272   0.07724   0.07075  -0.0318   0.0212   1.0000
  14.250   1.2191   0.08232   0.07601  -0.0338   0.0208   1.0000
  14.500   1.2102   0.08775   0.08161  -0.0361   0.0205   1.0000
  14.750   1.2011   0.09340   0.08745  -0.0386   0.0203   1.0000
  15.000   1.1911   0.09945   0.09367  -0.0415   0.0201   1.0000
  15.250   1.1802   0.10590   0.10029  -0.0448   0.0200   1.0000
  15.500   1.1683   0.11282   0.10739  -0.0486   0.0199   1.0000
  15.750   1.1548   0.12043   0.11518  -0.0529   0.0198   1.0000
  16.000   1.1389   0.12900   0.12394  -0.0580   0.0199   1.0000
  16.250   1.1179   0.13944   0.13459  -0.0644   0.0201   1.0000
  16.500   1.0881   0.15333   0.14869  -0.0729   0.0206   1.0000
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