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RYAN BQM-34 FIREBEE WING AIRFOIL (bqm34-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: RYAN BQM-34 FIREBEE WING AIRFOIL (bqm34-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.84 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-bqm34-il-1000000.txt
Download as CSV file: xf-bqm34-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -1.0296   0.09982   0.09752  -0.0043   1.0000   0.0092
 -16.250  -1.0652   0.08820   0.08574  -0.0111   1.0000   0.0091
 -16.000  -1.0935   0.07849   0.07587  -0.0169   1.0000   0.0091
 -15.750  -1.1103   0.07121   0.06845  -0.0215   1.0000   0.0090
 -15.500  -1.1291   0.06391   0.06100  -0.0261   1.0000   0.0090
 -15.250  -1.1385   0.05852   0.05549  -0.0295   1.0000   0.0089
 -15.000  -1.1586   0.05190   0.04869  -0.0334   1.0000   0.0090
 -14.750  -1.1817   0.04551   0.04211  -0.0366   1.0000   0.0091
 -14.500  -1.1883   0.04179   0.03825  -0.0379   1.0000   0.0091
 -14.250  -1.1987   0.03799   0.03429  -0.0387   1.0000   0.0091
 -14.000  -1.2052   0.03502   0.03120  -0.0386   1.0000   0.0093
 -13.750  -1.2093   0.03255   0.02859  -0.0378   1.0000   0.0094
 -13.500  -1.2101   0.03062   0.02655  -0.0364   1.0000   0.0095
 -13.250  -1.2065   0.02924   0.02508  -0.0348   1.0000   0.0096
 -13.000  -1.2002   0.02818   0.02397  -0.0330   1.0000   0.0098
 -12.750  -1.1970   0.02694   0.02263  -0.0304   1.0000   0.0100
 -12.500  -1.1921   0.02591   0.02150  -0.0276   1.0000   0.0100
 -12.250  -1.1834   0.02505   0.02056  -0.0252   1.0000   0.0103
 -12.000  -1.1722   0.02401   0.01941  -0.0233   1.0000   0.0104
 -11.750  -1.1583   0.02312   0.01842  -0.0216   1.0000   0.0107
 -11.500  -1.1438   0.02219   0.01738  -0.0200   1.0000   0.0109
 -11.250  -1.1278   0.02133   0.01643  -0.0185   1.0000   0.0111
 -11.000  -1.1115   0.02046   0.01546  -0.0170   1.0000   0.0113
 -10.750  -1.0931   0.01976   0.01467  -0.0157   1.0000   0.0114
 -10.500  -1.0755   0.01893   0.01375  -0.0143   1.0000   0.0116
 -10.250  -1.0630   0.01753   0.01222  -0.0122   1.0000   0.0121
 -10.000  -1.0445   0.01677   0.01141  -0.0109   1.0000   0.0125
  -9.750  -1.0241   0.01619   0.01079  -0.0098   1.0000   0.0129
  -9.500  -1.0033   0.01566   0.01021  -0.0087   1.0000   0.0134
  -9.250  -0.9820   0.01516   0.00966  -0.0076   1.0000   0.0139
  -9.000  -0.9605   0.01470   0.00914  -0.0066   1.0000   0.0144
  -8.750  -0.9382   0.01433   0.00872  -0.0056   1.0000   0.0148
  -8.500  -0.9202   0.01348   0.00781  -0.0040   1.0000   0.0159
  -8.250  -0.8984   0.01307   0.00739  -0.0030   1.0000   0.0169
  -8.000  -0.8758   0.01273   0.00703  -0.0020   1.0000   0.0179
  -7.750  -0.8528   0.01246   0.00672  -0.0011   1.0000   0.0188
  -7.500  -0.8327   0.01187   0.00609   0.0003   1.0000   0.0204
  -7.250  -0.8107   0.01152   0.00574   0.0014   1.0000   0.0218
  -7.000  -0.7882   0.01124   0.00545   0.0024   1.0000   0.0232
  -6.750  -0.7667   0.01087   0.00504   0.0037   1.0000   0.0250
  -6.500  -0.7454   0.01052   0.00471   0.0049   1.0000   0.0274
  -6.250  -0.7233   0.01029   0.00447   0.0060   1.0000   0.0294
  -6.000  -0.7024   0.00996   0.00414   0.0074   1.0000   0.0326
  -5.750  -0.6790   0.00971   0.00390   0.0082   0.9998   0.0361
  -5.500  -0.6439   0.00939   0.00360   0.0065   0.9976   0.0419
  -5.250  -0.6084   0.00911   0.00336   0.0047   0.9951   0.0490
  -5.000  -0.5744   0.00881   0.00311   0.0033   0.9921   0.0589
  -4.750  -0.5406   0.00848   0.00286   0.0019   0.9883   0.0742
  -4.500  -0.5054   0.00817   0.00265   0.0001   0.9851   0.0933
  -4.250  -0.4718   0.00783   0.00243  -0.0013   0.9809   0.1201
  -4.000  -0.4386   0.00748   0.00222  -0.0025   0.9750   0.1529
  -3.500  -0.3718   0.00674   0.00183  -0.0052   0.9595   0.2393
  -3.250  -0.3407   0.00635   0.00165  -0.0061   0.9469   0.2964
  -3.000  -0.3122   0.00599   0.00149  -0.0063   0.9306   0.3550
  -2.750  -0.2860   0.00571   0.00136  -0.0059   0.9116   0.4108
  -2.500  -0.2609   0.00549   0.00125  -0.0052   0.8918   0.4617
  -2.250  -0.2358   0.00532   0.00118  -0.0045   0.8721   0.5050
  -2.000  -0.2103   0.00522   0.00111  -0.0039   0.8533   0.5410
  -1.750  -0.1846   0.00513   0.00106  -0.0033   0.8355   0.5725
  -1.500  -0.1587   0.00507   0.00102  -0.0027   0.8188   0.6009
  -1.250  -0.1327   0.00502   0.00099  -0.0022   0.8024   0.6255
  -1.000  -0.1063   0.00500   0.00097  -0.0017   0.7862   0.6473
  -0.750  -0.0799   0.00497   0.00095  -0.0013   0.7702   0.6675
  -0.500  -0.0534   0.00496   0.00094  -0.0008   0.7535   0.6860
  -0.250  -0.0267   0.00495   0.00093  -0.0004   0.7365   0.7034
   0.000   0.0000   0.00495   0.00093   0.0000   0.7200   0.7199
   0.250   0.0267   0.00495   0.00093   0.0004   0.7034   0.7366
   0.500   0.0533   0.00496   0.00094   0.0008   0.6862   0.7536
   0.750   0.0799   0.00497   0.00095   0.0013   0.6674   0.7700
   1.000   0.1062   0.00500   0.00097   0.0017   0.6475   0.7862
   1.250   0.1327   0.00502   0.00099   0.0022   0.6258   0.8023
   1.500   0.1587   0.00507   0.00102   0.0027   0.6009   0.8187
   1.750   0.1846   0.00513   0.00106   0.0033   0.5724   0.8356
   2.250   0.2357   0.00532   0.00118   0.0046   0.5047   0.8722
   2.500   0.2608   0.00549   0.00125   0.0052   0.4611   0.8919
   2.750   0.2860   0.00571   0.00136   0.0059   0.4109   0.9117
   3.000   0.3122   0.00599   0.00149   0.0063   0.3551   0.9306
   3.250   0.3407   0.00635   0.00165   0.0061   0.2954   0.9470
   3.500   0.3718   0.00674   0.00183   0.0052   0.2391   0.9596
   4.000   0.4386   0.00747   0.00222   0.0026   0.1528   0.9751
   4.250   0.4717   0.00783   0.00243   0.0013   0.1201   0.9810
   4.500   0.5054   0.00817   0.00265  -0.0001   0.0933   0.9851
   4.750   0.5406   0.00848   0.00286  -0.0019   0.0740   0.9884
   5.000   0.5744   0.00881   0.00311  -0.0033   0.0589   0.9921
   5.250   0.6086   0.00911   0.00336  -0.0048   0.0491   0.9952
   5.500   0.6440   0.00939   0.00360  -0.0065   0.0418   0.9977
   5.750   0.6791   0.00971   0.00390  -0.0082   0.0361   0.9998
   6.000   0.7023   0.00996   0.00414  -0.0074   0.0327   1.0000
   6.250   0.7231   0.01029   0.00447  -0.0060   0.0294   1.0000
   6.500   0.7452   0.01052   0.00471  -0.0049   0.0274   1.0000
   6.750   0.7666   0.01087   0.00505  -0.0036   0.0250   1.0000
   7.000   0.7881   0.01124   0.00545  -0.0024   0.0232   1.0000
   7.250   0.8106   0.01152   0.00574  -0.0014   0.0218   1.0000
   7.500   0.8327   0.01186   0.00608  -0.0003   0.0204   1.0000
   7.750   0.8528   0.01245   0.00672   0.0011   0.0188   1.0000
   8.000   0.8757   0.01273   0.00703   0.0020   0.0178   1.0000
   8.250   0.8984   0.01306   0.00738   0.0030   0.0168   1.0000
   8.500   0.9202   0.01347   0.00780   0.0040   0.0159   1.0000
   8.750   0.9381   0.01433   0.00872   0.0057   0.0148   1.0000
   9.000   0.9604   0.01471   0.00916   0.0066   0.0145   1.0000
   9.250   0.9820   0.01517   0.00967   0.0076   0.0139   1.0000
   9.500   1.0032   0.01568   0.01023   0.0087   0.0134   1.0000
   9.750   1.0242   0.01620   0.01079   0.0098   0.0129   1.0000
  10.000   1.0447   0.01676   0.01140   0.0109   0.0125   1.0000
  10.250   1.0633   0.01751   0.01220   0.0122   0.0121   1.0000
  10.500   1.0763   0.01886   0.01367   0.0142   0.0116   1.0000
  10.750   1.0928   0.01981   0.01473   0.0157   0.0114   1.0000
  11.000   1.1115   0.02048   0.01548   0.0170   0.0113   1.0000
  11.250   1.1282   0.02132   0.01642   0.0184   0.0111   1.0000
  11.500   1.1446   0.02214   0.01733   0.0199   0.0109   1.0000
  11.750   1.1588   0.02310   0.01840   0.0215   0.0107   1.0000
  12.000   1.1730   0.02397   0.01937   0.0232   0.0104   1.0000
  12.250   1.1850   0.02494   0.02043   0.0250   0.0102   1.0000
  12.500   1.1935   0.02585   0.02143   0.0274   0.0100   1.0000
  12.750   1.1988   0.02685   0.02252   0.0302   0.0099   1.0000
  13.000   1.2049   0.02785   0.02359   0.0325   0.0097   1.0000
  13.250   1.2090   0.02909   0.02491   0.0345   0.0095   1.0000
  13.500   1.2109   0.03060   0.02650   0.0363   0.0093   1.0000
  13.750   1.2081   0.03276   0.02883   0.0377   0.0094   1.0000
  14.000   1.2042   0.03519   0.03135   0.0384   0.0092   1.0000
  14.250   1.1994   0.03803   0.03433   0.0385   0.0091   1.0000
  14.500   1.1877   0.04200   0.03847   0.0377   0.0090   1.0000
  14.750   1.1805   0.04586   0.04247   0.0362   0.0091   1.0000
  15.000   1.1707   0.05040   0.04716   0.0340   0.0091   1.0000
  15.250   1.1376   0.05892   0.05591   0.0290   0.0089   1.0000
  15.500   1.1320   0.06374   0.06083   0.0259   0.0090   1.0000
  15.750   1.1146   0.07077   0.06801   0.0214   0.0090   1.0000
  16.000   1.0879   0.07990   0.07730   0.0157   0.0090   1.0000
  16.250   1.0635   0.08893   0.08647   0.0103   0.0091   1.0000
  16.500   1.0397   0.09810   0.09576   0.0050   0.0091   1.0000
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