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FX 75-VG-166/22 (fx75vg166-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 75-VG-166/22 (fx75vg166-il)
Reynolds number: 1,000,000
Max Cl/Cd: 107.76 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx75vg166-il-1000000.txt
Download as CSV file: xf-fx75vg166-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 75-VG-166/22                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.6691   0.06785   0.06444  -0.0986   0.7446   0.0093
 -15.500  -0.4605   0.06794   0.06485  -0.1012   0.7423   0.0108
 -15.250  -0.7505   0.04824   0.04412  -0.1102   0.7440   0.0091
 -15.000  -0.6759   0.05453   0.05085  -0.1096   0.7434   0.0099
 -14.750  -0.7267   0.04523   0.04110  -0.1129   0.7431   0.0096
 -14.500  -0.7561   0.03942   0.03491  -0.1131   0.7426   0.0093
 -14.250  -0.7230   0.04044   0.03609  -0.1144   0.7420   0.0099
 -14.000  -0.7399   0.03616   0.03149  -0.1138   0.7415   0.0097
 -13.750  -0.7399   0.03360   0.02873  -0.1135   0.7408   0.0097
 -13.500  -0.7197   0.03323   0.02836  -0.1143   0.7400   0.0101
 -13.250  -0.7163   0.03139   0.02637  -0.1131   0.7397   0.0103
 -13.000  -0.7070   0.03023   0.02510  -0.1121   0.7393   0.0105
 -12.750  -0.6985   0.02884   0.02359  -0.1109   0.7387   0.0105
 -12.500  -0.6896   0.02741   0.02202  -0.1096   0.7380   0.0107
 -12.250  -0.6785   0.02610   0.02058  -0.1084   0.7374   0.0107
 -12.000  -0.6632   0.02540   0.01980  -0.1075   0.7367   0.0110
 -11.750  -0.6504   0.02408   0.01837  -0.1063   0.7359   0.0109
 -11.500  -0.6331   0.02360   0.01782  -0.1056   0.7352   0.0111
 -11.250  -0.6196   0.02230   0.01638  -0.1043   0.7344   0.0115
 -11.000  -0.6004   0.02190   0.01594  -0.1036   0.7336   0.0112
 -10.750  -0.5874   0.02067   0.01466  -0.1022   0.7329   0.0120
 -10.500  -0.5700   0.02004   0.01399  -0.1012   0.7322   0.0123
 -10.250  -0.5526   0.01939   0.01329  -0.1001   0.7316   0.0124
 -10.000  -0.5328   0.01900   0.01288  -0.0994   0.7309   0.0128
  -9.750  -0.5144   0.01846   0.01229  -0.0983   0.7303   0.0131
  -9.500  -0.4954   0.01800   0.01177  -0.0974   0.7296   0.0136
  -9.250  -0.4764   0.01753   0.01126  -0.0964   0.7290   0.0139
  -9.000  -0.4592   0.01696   0.01064  -0.0951   0.7284   0.0146
  -8.750  -0.4419   0.01645   0.01011  -0.0938   0.7277   0.0153
  -8.500  -0.4219   0.01613   0.00978  -0.0929   0.7270   0.0160
  -8.250  -0.4029   0.01578   0.00940  -0.0918   0.7263   0.0164
  -8.000  -0.3824   0.01558   0.00918  -0.0909   0.7253   0.0172
  -7.750  -0.3656   0.01522   0.00878  -0.0893   0.7244   0.0180
  -7.500  -0.3499   0.01470   0.00827  -0.0876   0.7239   0.0190
  -7.250  -0.3318   0.01436   0.00792  -0.0862   0.7233   0.0196
  -7.000  -0.3128   0.01406   0.00763  -0.0849   0.7226   0.0208
  -6.750  -0.2948   0.01375   0.00729  -0.0834   0.7217   0.0215
  -6.500  -0.2799   0.01336   0.00690  -0.0813   0.7207   0.0232
  -6.250  -0.2634   0.01311   0.00666  -0.0795   0.7198   0.0244
  -6.000  -0.2461   0.01293   0.00647  -0.0778   0.7189   0.0259
  -5.750  -0.2310   0.01271   0.00624  -0.0757   0.7179   0.0278
  -5.500  -0.2136   0.01251   0.00606  -0.0739   0.7170   0.0302
  -5.250  -0.1935   0.01232   0.00586  -0.0726   0.7161   0.0334
  -5.000  -0.1734   0.01210   0.00566  -0.0714   0.7153   0.0382
  -4.750  -0.1533   0.01186   0.00546  -0.0702   0.7145   0.0464
  -4.500  -0.1340   0.01157   0.00527  -0.0689   0.7137   0.0658
  -4.250  -0.1152   0.01124   0.00508  -0.0675   0.7130   0.0985
  -4.000  -0.0981   0.01083   0.00488  -0.0658   0.7122   0.1537
  -3.750  -0.0819   0.01037   0.00469  -0.0640   0.7113   0.2250
  -3.500  -0.0685   0.00983   0.00452  -0.0618   0.7102   0.3241
  -3.250  -0.0585   0.00908   0.00428  -0.0590   0.7088   0.4535
  -3.000  -0.0481   0.00824   0.00393  -0.0561   0.7077   0.5837
  -2.750  -0.0346   0.00775   0.00393  -0.0532   0.7064   0.7059
  -2.500  -0.0064   0.00802   0.00431  -0.0531   0.7053   0.7373
  -2.250   0.0230   0.00823   0.00449  -0.0534   0.7042   0.7506
  -2.000   0.0524   0.00846   0.00469  -0.0538   0.7031   0.7613
  -1.750   0.0821   0.00872   0.00492  -0.0541   0.7021   0.7689
  -1.500   0.1133   0.00907   0.00527  -0.0546   0.7010   0.7737
  -1.250   0.1428   0.00936   0.00552  -0.0549   0.7000   0.7806
  -1.000   0.1738   0.00965   0.00584  -0.0553   0.6992   0.7833
  -0.750   0.2048   0.00996   0.00615  -0.0557   0.6984   0.7858
  -0.500   0.2350   0.01012   0.00631  -0.0561   0.6975   0.7879
  -0.250   0.2646   0.01018   0.00634  -0.0565   0.6967   0.7900
   0.000   0.2939   0.01023   0.00635  -0.0570   0.6956   0.7927
   0.250   0.3222   0.01033   0.00640  -0.0574   0.6944   0.7955
   0.500   0.3486   0.01020   0.00631  -0.0572   0.6929   0.7967
   0.750   0.3759   0.01016   0.00629  -0.0572   0.6912   0.7976
   1.000   0.4038   0.01011   0.00626  -0.0574   0.6895   0.7984
   1.250   0.4322   0.01008   0.00624  -0.0576   0.6879   0.7994
   1.500   0.4609   0.01005   0.00621  -0.0578   0.6864   0.8004
   1.750   0.4900   0.00998   0.00614  -0.0582   0.6850   0.8014
   2.000   0.5194   0.00985   0.00600  -0.0587   0.6835   0.8024
   2.250   0.5487   0.00973   0.00586  -0.0592   0.6821   0.8033
   2.500   0.5777   0.00967   0.00579  -0.0596   0.6803   0.8043
   2.750   0.6039   0.00960   0.00577  -0.0595   0.6780   0.8056
   3.000   0.6312   0.00955   0.00573  -0.0597   0.6757   0.8071
   3.250   0.6596   0.00937   0.00556  -0.0600   0.6723   0.8083
   3.500   0.6887   0.00913   0.00529  -0.0604   0.6683   0.8093
   3.750   0.7161   0.00902   0.00518  -0.0604   0.6625   0.8103
   4.000   0.7419   0.00884   0.00503  -0.0602   0.6577   0.8113
   4.250   0.7685   0.00870   0.00490  -0.0602   0.6540   0.8121
   4.500   0.7951   0.00863   0.00485  -0.0601   0.6499   0.8127
   4.750   0.8212   0.00857   0.00485  -0.0600   0.6438   0.8133
   5.000   0.8472   0.00850   0.00477  -0.0597   0.6373   0.8139
   5.250   0.8729   0.00848   0.00479  -0.0595   0.6283   0.8146
   5.500   0.8974   0.00847   0.00478  -0.0590   0.6174   0.8152
   5.750   0.9192   0.00853   0.00479  -0.0579   0.5991   0.8160
   6.000   0.9374   0.00870   0.00487  -0.0562   0.5705   0.8170
   6.250   0.9482   0.00908   0.00509  -0.0529   0.5319   0.8184
   6.500   0.9542   0.00957   0.00541  -0.0489   0.4884   0.8199
   6.750   0.9560   0.01012   0.00578  -0.0441   0.4494   0.8212
   7.000   0.9545   0.01062   0.00613  -0.0387   0.4152   0.8225
   7.250   0.9431   0.01116   0.00653  -0.0313   0.3829   0.8239
   7.500   0.9332   0.01191   0.00715  -0.0246   0.3538   0.8250
   7.750   0.9185   0.01282   0.00795  -0.0176   0.3257   0.8266
   8.000   0.9085   0.01419   0.00924  -0.0128   0.3026   0.8278
   8.250   0.9005   0.01546   0.01038  -0.0081   0.2737   0.8287
   8.500   0.8919   0.01680   0.01154  -0.0035   0.2384   0.8296
   8.750   0.8894   0.01799   0.01255   0.0001   0.2060   0.8303
   9.000   0.8971   0.01883   0.01332   0.0021   0.1873   0.8309
   9.250   0.9011   0.01987   0.01421   0.0046   0.1604   0.8315
   9.500   0.9086   0.02083   0.01506   0.0064   0.1381   0.8319
   9.750   0.9208   0.02161   0.01579   0.0076   0.1251   0.8323
  10.000   0.9328   0.02244   0.01654   0.0088   0.1097   0.8327
  10.250   0.9441   0.02334   0.01735   0.0100   0.0932   0.8331
  10.500   0.9551   0.02431   0.01823   0.0110   0.0778   0.8334
  10.750   0.9669   0.02527   0.01912   0.0119   0.0630   0.8337
  11.000   0.9760   0.02645   0.02018   0.0130   0.0457   0.8340
  11.250   0.9892   0.02747   0.02115   0.0136   0.0368   0.8342
  11.500   1.0025   0.02853   0.02219   0.0141   0.0309   0.8344
  11.750   1.0165   0.02958   0.02321   0.0144   0.0259   0.8346
  12.000   1.0336   0.03046   0.02412   0.0145   0.0246   0.8348
  12.250   1.0478   0.03155   0.02521   0.0147   0.0224   0.8350
  12.500   1.0618   0.03271   0.02640   0.0149   0.0211   0.8351
  12.750   1.0785   0.03369   0.02742   0.0149   0.0199   0.8353
  13.000   1.0935   0.03483   0.02858   0.0149   0.0187   0.8354
  13.250   1.1035   0.03637   0.03016   0.0152   0.0174   0.8355
  13.500   1.1191   0.03747   0.03131   0.0151   0.0166   0.8357
  13.750   1.1337   0.03867   0.03256   0.0151   0.0160   0.8359
  14.000   1.1473   0.04001   0.03394   0.0150   0.0153   0.8361
  14.250   1.1598   0.04146   0.03544   0.0150   0.0149   0.8362
  14.500   1.1670   0.04335   0.03738   0.0152   0.0140   0.8363
  14.750   1.1757   0.04519   0.03928   0.0152   0.0135   0.8364
  15.000   1.1908   0.04652   0.04067   0.0148   0.0131   0.8364
  15.250   1.1995   0.04843   0.04265   0.0147   0.0130   0.8364
  15.500   1.2123   0.05001   0.04427   0.0143   0.0124   0.8365
  15.750   1.2226   0.05179   0.04612   0.0141   0.0121   0.8366
  16.000   1.2323   0.05369   0.04807   0.0137   0.0117   0.8366
  16.250   1.2388   0.05588   0.05033   0.0135   0.0117   0.8368
  16.500   1.2332   0.05935   0.05387   0.0136   0.0109   0.8368
  16.750   1.2439   0.06121   0.05579   0.0131   0.0111   0.8370
  17.000   1.2374   0.06483   0.05952   0.0131   0.0108   0.8371
  17.250   1.2477   0.06685   0.06161   0.0124   0.0105   0.8372
  17.500   1.2492   0.06982   0.06466   0.0118   0.0106   0.8372
  17.750   1.2538   0.07252   0.06746   0.0111   0.0104   0.8371
  18.000   1.2571   0.07543   0.07045   0.0103   0.0102   0.8371
  18.250   1.2587   0.07853   0.07365   0.0095   0.0101   0.8370
  18.500   1.2613   0.08156   0.07675   0.0085   0.0099   0.8370
  18.750   1.2660   0.08444   0.07970   0.0074   0.0096   0.8369
  19.000   1.2610   0.08845   0.08382   0.0063   0.0096   0.8369
  19.250   1.2627   0.09179   0.08722   0.0050   0.0094   0.8368
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