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BOEING 103 AIRFOIL (boe103-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: BOEING 103 AIRFOIL (boe103-il)
Reynolds number: 1,000,000
Max Cl/Cd: 88.97 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-boe103-il-1000000-n5.txt
Download as CSV file: xf-boe103-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: BOEING 103 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -1.1259   0.03762   0.03444  -0.0938   1.0000   0.0106
 -16.000  -1.1367   0.03384   0.03050  -0.0956   1.0000   0.0107
 -15.750  -1.1447   0.03141   0.02795  -0.0950   1.0000   0.0109
 -15.500  -1.1535   0.02975   0.02619  -0.0922   1.0000   0.0110
 -15.250  -1.1647   0.02860   0.02496  -0.0876   1.0000   0.0111
 -15.000  -1.1656   0.02749   0.02376  -0.0841   1.0000   0.0113
 -14.750  -1.1627   0.02647   0.02264  -0.0811   1.0000   0.0115
 -14.500  -1.1517   0.02542   0.02149  -0.0795   0.9996   0.0117
 -14.250  -1.1276   0.02440   0.02039  -0.0801   0.9982   0.0120
 -14.000  -1.1016   0.02361   0.01956  -0.0808   0.9968   0.0124
 -13.750  -1.0743   0.02291   0.01882  -0.0816   0.9955   0.0128
 -13.500  -1.0462   0.02223   0.01809  -0.0825   0.9943   0.0132
 -13.250  -1.0203   0.02155   0.01734  -0.0829   0.9925   0.0136
 -13.000  -0.9944   0.02084   0.01655  -0.0833   0.9902   0.0140
 -12.750  -0.9672   0.02011   0.01572  -0.0839   0.9882   0.0144
 -12.500  -0.9387   0.01945   0.01499  -0.0847   0.9865   0.0147
 -12.250  -0.9076   0.01905   0.01457  -0.0858   0.9852   0.0152
 -12.000  -0.8769   0.01873   0.01425  -0.0867   0.9834   0.0155
 -11.750  -0.8494   0.01838   0.01387  -0.0869   0.9790   0.0159
 -11.500  -0.8186   0.01796   0.01341  -0.0878   0.9759   0.0163
 -11.250  -0.7881   0.01749   0.01287  -0.0887   0.9728   0.0167
 -11.000  -0.7631   0.01702   0.01235  -0.0884   0.9661   0.0171
 -10.750  -0.7331   0.01654   0.01179  -0.0892   0.9620   0.0175
 -10.500  -0.7056   0.01613   0.01130  -0.0893   0.9552   0.0178
 -10.250  -0.6762   0.01562   0.01073  -0.0899   0.9488   0.0182
 -10.000  -0.6478   0.01522   0.01029  -0.0902   0.9404   0.0186
  -9.750  -0.6185   0.01489   0.00992  -0.0906   0.9316   0.0189
  -9.500  -0.5908   0.01461   0.00958  -0.0907   0.9214   0.0192
  -9.250  -0.5636   0.01435   0.00927  -0.0906   0.9116   0.0195
  -8.750  -0.5106   0.01381   0.00858  -0.0902   0.8927   0.0204
  -8.500  -0.4846   0.01349   0.00817  -0.0899   0.8839   0.0207
  -8.250  -0.4584   0.01320   0.00782  -0.0895   0.8752   0.0211
  -8.000  -0.4321   0.01295   0.00748  -0.0892   0.8670   0.0215
  -7.750  -0.4056   0.01270   0.00716  -0.0890   0.8586   0.0217
  -7.500  -0.3792   0.01244   0.00683  -0.0886   0.8507   0.0219
  -7.250  -0.3544   0.01189   0.00622  -0.0882   0.8423   0.0224
  -7.000  -0.3285   0.01156   0.00585  -0.0878   0.8344   0.0228
  -6.750  -0.3020   0.01129   0.00553  -0.0875   0.8263   0.0232
  -6.500  -0.2756   0.01104   0.00522  -0.0872   0.8182   0.0235
  -6.250  -0.2489   0.01079   0.00493  -0.0869   0.8096   0.0238
  -6.000  -0.2223   0.01057   0.00466  -0.0866   0.8016   0.0242
  -5.750  -0.1954   0.01036   0.00441  -0.0864   0.7930   0.0247
  -5.500  -0.1687   0.01015   0.00415  -0.0861   0.7843   0.0250
  -5.250  -0.1418   0.00994   0.00389  -0.0858   0.7750   0.0254
  -5.000  -0.1150   0.00975   0.00365  -0.0855   0.7665   0.0257
  -4.750  -0.0881   0.00958   0.00342  -0.0852   0.7568   0.0260
  -4.500  -0.0610   0.00942   0.00322  -0.0850   0.7471   0.0262
  -4.250  -0.0342   0.00930   0.00303  -0.0846   0.7357   0.0265
  -4.000  -0.0075   0.00919   0.00286  -0.0843   0.7222   0.0266
  -3.750   0.0187   0.00900   0.00260  -0.0839   0.7072   0.0273
  -3.500   0.0452   0.00887   0.00241  -0.0835   0.6925   0.0281
  -3.250   0.0719   0.00878   0.00226  -0.0832   0.6783   0.0287
  -3.000   0.0988   0.00871   0.00213  -0.0829   0.6647   0.0293
  -2.750   0.1255   0.00866   0.00202  -0.0825   0.6497   0.0299
  -2.500   0.1524   0.00862   0.00191  -0.0822   0.6362   0.0304
  -2.000   0.2070   0.00853   0.00175  -0.0818   0.6154   0.0318
  -1.750   0.2343   0.00850   0.00168  -0.0816   0.6060   0.0325
  -1.500   0.2619   0.00845   0.00161  -0.0815   0.5976   0.0348
  -1.250   0.2892   0.00841   0.00156  -0.0813   0.5889   0.0380
  -1.000   0.3157   0.00820   0.00149  -0.0810   0.5787   0.0864
  -0.750   0.3423   0.00811   0.00147  -0.0807   0.5661   0.1211
  -0.500   0.3691   0.00807   0.00146  -0.0805   0.5527   0.1469
  -0.250   0.3959   0.00806   0.00146  -0.0803   0.5402   0.1683
   0.000   0.4228   0.00802   0.00147  -0.0801   0.5277   0.1960
   0.250   0.4492   0.00795   0.00147  -0.0798   0.5125   0.2409
   0.500   0.4739   0.00767   0.00149  -0.0794   0.4958   0.3691
   0.750   0.4990   0.00748   0.00154  -0.0789   0.4796   0.4739
   1.000   0.5236   0.00733   0.00161  -0.0784   0.4613   0.5750
   1.250   0.5476   0.00729   0.00171  -0.0777   0.4333   0.6608
   1.500   0.5705   0.00747   0.00185  -0.0767   0.3900   0.7148
   1.750   0.5925   0.00760   0.00201  -0.0756   0.3529   0.7832
   2.000   0.6135   0.00762   0.00219  -0.0740   0.3279   0.8700
   2.250   0.6366   0.00775   0.00234  -0.0728   0.3095   0.9174
   2.500   0.6633   0.00795   0.00248  -0.0725   0.2896   0.9537
   2.750   0.6974   0.00818   0.00263  -0.0739   0.2718   0.9763
   3.000   0.7325   0.00844   0.00277  -0.0756   0.2534   0.9887
   3.250   0.7648   0.00869   0.00292  -0.0768   0.2341   0.9951
   3.500   0.7972   0.00896   0.00308  -0.0780   0.2144   0.9991
   3.750   0.8205   0.00925   0.00324  -0.0772   0.1949   1.0000
   4.000   0.8415   0.00955   0.00343  -0.0759   0.1746   1.0000
   4.250   0.8629   0.00987   0.00363  -0.0747   0.1546   1.0000
   4.500   0.8844   0.01021   0.00386  -0.0735   0.1354   1.0000
   4.750   0.9065   0.01054   0.00410  -0.0725   0.1184   1.0000
   5.000   0.9293   0.01085   0.00432  -0.0716   0.1057   1.0000
   5.250   0.9528   0.01112   0.00454  -0.0709   0.0981   1.0000
   5.500   0.9767   0.01136   0.00475  -0.0702   0.0926   1.0000
   5.750   1.0007   0.01160   0.00496  -0.0696   0.0888   1.0000
   6.000   1.0247   0.01184   0.00517  -0.0690   0.0860   1.0000
   6.250   1.0488   0.01208   0.00540  -0.0684   0.0833   1.0000
   6.500   1.0732   0.01229   0.00561  -0.0678   0.0820   1.0000
   6.750   1.0975   0.01250   0.00582  -0.0673   0.0810   1.0000
   7.000   1.1215   0.01272   0.00606  -0.0667   0.0797   1.0000
   7.250   1.1452   0.01296   0.00630  -0.0661   0.0784   1.0000
   7.500   1.1682   0.01324   0.00657  -0.0654   0.0760   1.0000
   7.750   1.1903   0.01357   0.00687  -0.0645   0.0722   1.0000
   8.000   1.2131   0.01384   0.00715  -0.0638   0.0704   1.0000
   8.250   1.2359   0.01410   0.00742  -0.0630   0.0688   1.0000
   8.500   1.2569   0.01442   0.00772  -0.0620   0.0645   1.0000
   8.750   1.2756   0.01482   0.00809  -0.0606   0.0578   1.0000
   9.000   1.2872   0.01563   0.00873  -0.0581   0.0386   1.0000
   9.250   1.3050   0.01609   0.00919  -0.0566   0.0358   1.0000
   9.500   1.3227   0.01657   0.00966  -0.0551   0.0336   1.0000
   9.750   1.3409   0.01701   0.01013  -0.0538   0.0320   1.0000
  10.000   1.3589   0.01746   0.01060  -0.0525   0.0311   1.0000
  10.250   1.3759   0.01798   0.01114  -0.0510   0.0298   1.0000
  10.500   1.3917   0.01857   0.01174  -0.0495   0.0282   1.0000
  10.750   1.4073   0.01919   0.01239  -0.0480   0.0266   1.0000
  11.000   1.4245   0.01971   0.01294  -0.0468   0.0258   1.0000
  11.500   1.4437   0.02178   0.01499  -0.0426   0.0118   1.0000
  11.750   1.4565   0.02265   0.01591  -0.0411   0.0107   1.0000
  12.000   1.4687   0.02358   0.01690  -0.0396   0.0098   1.0000
  12.250   1.4797   0.02462   0.01799  -0.0381   0.0091   1.0000
  12.500   1.4923   0.02558   0.01900  -0.0369   0.0087   1.0000
  12.750   1.5037   0.02665   0.02012  -0.0356   0.0083   1.0000
  13.000   1.5141   0.02782   0.02135  -0.0343   0.0079   1.0000
  13.250   1.5234   0.02911   0.02271  -0.0331   0.0076   1.0000
  13.500   1.5314   0.03056   0.02421  -0.0319   0.0072   1.0000
  13.750   1.5402   0.03196   0.02567  -0.0308   0.0070   1.0000
  14.000   1.5484   0.03345   0.02723  -0.0298   0.0068   1.0000
  14.250   1.5557   0.03507   0.02892  -0.0289   0.0066   1.0000
  14.500   1.5619   0.03683   0.03075  -0.0280   0.0064   1.0000
  14.750   1.5669   0.03874   0.03272  -0.0272   0.0062   1.0000
  15.000   1.5709   0.04082   0.03488  -0.0265   0.0060   1.0000
  15.250   1.5736   0.04311   0.03724  -0.0260   0.0058   1.0000
  15.500   1.5745   0.04564   0.03985  -0.0255   0.0056   1.0000
  15.750   1.5755   0.04825   0.04255  -0.0252   0.0055   1.0000
  16.000   1.5768   0.05090   0.04528  -0.0250   0.0054   1.0000
  16.250   1.5769   0.05377   0.04824  -0.0250   0.0053   1.0000
  16.500   1.5757   0.05686   0.05143  -0.0251   0.0052   1.0000
  16.750   1.5732   0.06017   0.05482  -0.0254   0.0051   1.0000
  17.000   1.5697   0.06368   0.05844  -0.0258   0.0050   1.0000
  17.250   1.5650   0.06745   0.06230  -0.0264   0.0049   1.0000
  17.500   1.5588   0.07148   0.06644  -0.0271   0.0048   1.0000
  17.750   1.5512   0.07579   0.07084  -0.0280   0.0047   1.0000
  18.000   1.5419   0.08043   0.07559  -0.0292   0.0047   1.0000
  18.250   1.5318   0.08528   0.08056  -0.0305   0.0046   1.0000
  18.500   1.5193   0.09059   0.08598  -0.0321   0.0046   1.0000
  18.750   1.5059   0.09612   0.09162  -0.0339   0.0045   1.0000
  19.000   1.4911   0.10201   0.09764  -0.0360   0.0045   1.0000
  19.250   1.4753   0.10815   0.10389  -0.0383   0.0045   1.0000
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