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RYAN BQM-34 FIREBEE WING AIRFOIL (bqm34-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: RYAN BQM-34 FIREBEE WING AIRFOIL (bqm34-il)
Reynolds number: 100,000
Max Cl/Cd: 34.85 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-bqm34-il-100000-n5.txt
Download as CSV file: xf-bqm34-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RYAN BQM-34 FIREBEE WING AIRFOIL                
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.7445   0.09633   0.09094  -0.0084   1.0000   0.0298
 -12.000  -0.7632   0.08717   0.08178  -0.0141   1.0000   0.0294
 -11.750  -0.7897   0.07735   0.07188  -0.0213   1.0000   0.0289
 -11.500  -0.8178   0.06915   0.06356  -0.0274   1.0000   0.0285
 -11.250  -0.8432   0.06295   0.05717  -0.0309   1.0000   0.0283
 -11.000  -0.8657   0.05818   0.05219  -0.0320   1.0000   0.0282
 -10.750  -0.8851   0.05440   0.04817  -0.0311   1.0000   0.0283
 -10.500  -0.9030   0.05097   0.04445  -0.0287   1.0000   0.0286
 -10.250  -0.9132   0.04745   0.04052  -0.0265   1.0000   0.0292
 -10.000  -0.9179   0.04410   0.03665  -0.0242   1.0000   0.0298
  -9.750  -0.9103   0.04171   0.03411  -0.0228   1.0000   0.0307
  -9.500  -0.8997   0.03968   0.03191  -0.0215   1.0000   0.0316
  -9.250  -0.8880   0.03750   0.02949  -0.0201   1.0000   0.0325
  -9.000  -0.8745   0.03533   0.02703  -0.0187   1.0000   0.0336
  -8.750  -0.8590   0.03330   0.02470  -0.0173   1.0000   0.0351
  -8.500  -0.8420   0.03154   0.02251  -0.0159   1.0000   0.0373
  -8.250  -0.8240   0.02991   0.02089  -0.0150   1.0000   0.0392
  -8.000  -0.8049   0.02854   0.01942  -0.0139   1.0000   0.0412
  -7.750  -0.7849   0.02715   0.01785  -0.0128   1.0000   0.0438
  -7.500  -0.7648   0.02586   0.01638  -0.0116   1.0000   0.0470
  -7.250  -0.7455   0.02474   0.01528  -0.0105   1.0000   0.0502
  -7.000  -0.7253   0.02366   0.01408  -0.0093   1.0000   0.0539
  -6.750  -0.7058   0.02262   0.01298  -0.0081   1.0000   0.0586
  -6.500  -0.6862   0.02174   0.01209  -0.0068   1.0000   0.0640
  -6.250  -0.6668   0.02083   0.01113  -0.0054   1.0000   0.0702
  -6.000  -0.6472   0.02005   0.01031  -0.0041   1.0000   0.0784
  -5.750  -0.6282   0.01922   0.00952  -0.0027   1.0000   0.0877
  -5.500  -0.6089   0.01847   0.00882  -0.0013   1.0000   0.1007
  -5.250  -0.5895   0.01776   0.00816   0.0001   1.0000   0.1180
  -5.000  -0.5705   0.01705   0.00756   0.0015   1.0000   0.1417
  -4.750  -0.5515   0.01636   0.00703   0.0029   1.0000   0.1745
  -4.500  -0.5328   0.01567   0.00656   0.0043   1.0000   0.2175
  -4.250  -0.5148   0.01498   0.00616   0.0058   1.0000   0.2734
  -4.000  -0.4973   0.01433   0.00581   0.0075   1.0000   0.3397
  -3.750  -0.4800   0.01377   0.00559   0.0093   1.0000   0.4115
  -3.500  -0.4623   0.01335   0.00546   0.0113   1.0000   0.4789
  -3.250  -0.4443   0.01306   0.00539   0.0132   1.0000   0.5371
  -3.000  -0.4258   0.01288   0.00533   0.0152   1.0000   0.5860
  -2.750  -0.4073   0.01275   0.00533   0.0171   1.0000   0.6267
  -2.500  -0.3818   0.01269   0.00534   0.0176   0.9964   0.6652
  -2.250  -0.3456   0.01266   0.00535   0.0161   0.9869   0.7012
  -2.000  -0.3096   0.01264   0.00536   0.0146   0.9774   0.7322
  -1.750  -0.2722   0.01264   0.00539   0.0130   0.9686   0.7607
  -1.500  -0.2358   0.01263   0.00539   0.0116   0.9589   0.7874
  -1.250  -0.1984   0.01264   0.00542   0.0101   0.9496   0.8110
  -1.000  -0.1583   0.01264   0.00543   0.0079   0.9412   0.8330
  -0.750  -0.1209   0.01265   0.00545   0.0064   0.9301   0.8512
  -0.500  -0.0811   0.01266   0.00546   0.0044   0.9196   0.8677
  -0.250  -0.0393   0.01266   0.00546   0.0020   0.9094   0.8825
   0.000   0.0000   0.01266   0.00546   0.0000   0.8964   0.8964
   0.250   0.0393   0.01266   0.00545  -0.0020   0.8824   0.9094
   0.500   0.0811   0.01266   0.00546  -0.0044   0.8677   0.9196
   0.750   0.1209   0.01265   0.00545  -0.0064   0.8512   0.9301
   1.000   0.1583   0.01264   0.00543  -0.0079   0.8330   0.9413
   1.250   0.1983   0.01264   0.00542  -0.0100   0.8110   0.9496
   1.500   0.2357   0.01263   0.00539  -0.0115   0.7873   0.9589
   1.750   0.2722   0.01264   0.00539  -0.0130   0.7606   0.9687
   2.000   0.3096   0.01264   0.00536  -0.0146   0.7324   0.9775
   2.250   0.3456   0.01266   0.00535  -0.0161   0.7013   0.9869
   2.500   0.3818   0.01269   0.00533  -0.0176   0.6653   0.9965
   2.750   0.4072   0.01275   0.00533  -0.0171   0.6271   1.0000
   3.000   0.4257   0.01288   0.00533  -0.0152   0.5863   1.0000
   3.250   0.4441   0.01306   0.00539  -0.0132   0.5369   1.0000
   3.500   0.4622   0.01335   0.00546  -0.0112   0.4786   1.0000
   3.750   0.4799   0.01377   0.00559  -0.0093   0.4113   1.0000
   4.000   0.4972   0.01433   0.00581  -0.0075   0.3397   1.0000
   4.250   0.5147   0.01498   0.00616  -0.0058   0.2735   1.0000
   4.500   0.5327   0.01567   0.00656  -0.0043   0.2176   1.0000
   4.750   0.5514   0.01636   0.00703  -0.0029   0.1745   1.0000
   5.000   0.5704   0.01705   0.00756  -0.0015   0.1418   1.0000
   5.250   0.5895   0.01776   0.00816  -0.0001   0.1180   1.0000
   5.500   0.6088   0.01847   0.00882   0.0013   0.1007   1.0000
   5.750   0.6282   0.01922   0.00952   0.0027   0.0876   1.0000
   6.000   0.6472   0.02004   0.01031   0.0041   0.0784   1.0000
   6.250   0.6668   0.02083   0.01112   0.0054   0.0700   1.0000
   6.500   0.6862   0.02174   0.01208   0.0068   0.0640   1.0000
   6.750   0.7058   0.02262   0.01298   0.0081   0.0585   1.0000
   7.000   0.7253   0.02367   0.01409   0.0093   0.0539   1.0000
   7.250   0.7455   0.02475   0.01529   0.0105   0.0502   1.0000
   7.500   0.7649   0.02586   0.01638   0.0116   0.0471   1.0000
   7.750   0.7850   0.02715   0.01785   0.0128   0.0438   1.0000
   8.000   0.8049   0.02854   0.01942   0.0139   0.0412   1.0000
   8.250   0.8241   0.02991   0.02088   0.0149   0.0392   1.0000
   8.500   0.8421   0.03153   0.02250   0.0159   0.0373   1.0000
   8.750   0.8591   0.03331   0.02471   0.0173   0.0351   1.0000
   9.000   0.8746   0.03533   0.02704   0.0186   0.0336   1.0000
   9.250   0.8882   0.03750   0.02949   0.0200   0.0325   1.0000
   9.500   0.8999   0.03969   0.03192   0.0215   0.0316   1.0000
   9.750   0.9106   0.04169   0.03409   0.0228   0.0307   1.0000
  10.000   0.9186   0.04413   0.03666   0.0241   0.0299   1.0000
  10.250   0.9138   0.04744   0.04051   0.0264   0.0292   1.0000
  10.500   0.9040   0.05094   0.04441   0.0286   0.0287   1.0000
  10.750   0.8858   0.05438   0.04815   0.0310   0.0283   1.0000
  11.000   0.8663   0.05819   0.05220   0.0320   0.0282   1.0000
  11.250   0.8446   0.06291   0.05712   0.0308   0.0284   1.0000
  11.500   0.8188   0.06915   0.06355   0.0273   0.0286   1.0000
  11.750   0.7920   0.07709   0.07160   0.0215   0.0290   1.0000
  12.000   0.7668   0.08651   0.08110   0.0145   0.0294   1.0000
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