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FX 74-130 WP1 (fx74130wp1-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 74-130 WP1 (fx74130wp1-il)
Reynolds number: 1,000,000
Max Cl/Cd: 145.62 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx74130wp1-il-1000000-n5.txt
Download as CSV file: xf-fx74130wp1-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 74-130 WP1                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.1369   0.08418   0.08135  -0.1178   0.7941   0.0057
 -10.250  -0.1353   0.08042   0.07760  -0.1196   0.7931   0.0056
 -10.000  -0.1337   0.07680   0.07398  -0.1214   0.7919   0.0054
  -9.750  -0.1357   0.07247   0.06966  -0.1237   0.7905   0.0052
  -9.500  -0.1431   0.06705   0.06426  -0.1267   0.7888   0.0051
  -9.250  -0.1562   0.06062   0.05788  -0.1316   0.7874   0.0049
  -9.000  -0.1777   0.05437   0.05162  -0.1358   0.7857   0.0048
  -8.500  -0.3383   0.02323   0.01914  -0.1238   0.7804   0.0045
  -8.250  -0.3241   0.02114   0.01678  -0.1226   0.7793   0.0046
  -8.000  -0.3045   0.01993   0.01539  -0.1219   0.7782   0.0047
  -7.750  -0.2850   0.01852   0.01374  -0.1212   0.7771   0.0049
  -7.500  -0.2638   0.01729   0.01230  -0.1207   0.7760   0.0052
  -7.250  -0.2417   0.01609   0.01090  -0.1201   0.7750   0.0053
  -7.000  -0.2180   0.01523   0.00988  -0.1199   0.7741   0.0056
  -6.750  -0.1942   0.01433   0.00884  -0.1195   0.7733   0.0057
  -6.500  -0.1697   0.01357   0.00796  -0.1193   0.7724   0.0059
  -6.250  -0.1447   0.01294   0.00723  -0.1191   0.7714   0.0060
  -6.000  -0.1195   0.01236   0.00655  -0.1190   0.7703   0.0061
  -5.750  -0.0942   0.01183   0.00595  -0.1188   0.7691   0.0062
  -5.500  -0.0682   0.01143   0.00549  -0.1188   0.7679   0.0063
  -5.250  -0.0419   0.01109   0.00511  -0.1188   0.7668   0.0064
  -5.000  -0.0172   0.01046   0.00440  -0.1186   0.7658   0.0069
  -4.750   0.0092   0.01012   0.00403  -0.1186   0.7647   0.0072
  -4.500   0.0359   0.00981   0.00370  -0.1187   0.7637   0.0075
  -4.250   0.0628   0.00954   0.00339  -0.1188   0.7626   0.0079
  -4.000   0.0900   0.00930   0.00311  -0.1189   0.7615   0.0085
  -3.750   0.1175   0.00911   0.00287  -0.1191   0.7603   0.0091
  -3.500   0.1449   0.00891   0.00266  -0.1193   0.7592   0.0097
  -3.250   0.1723   0.00869   0.00244  -0.1195   0.7580   0.0113
  -3.000   0.2001   0.00854   0.00229  -0.1198   0.7567   0.0127
  -2.750   0.2279   0.00840   0.00214  -0.1200   0.7554   0.0151
  -2.500   0.2558   0.00824   0.00203  -0.1203   0.7541   0.0223
  -2.250   0.2837   0.00807   0.00192  -0.1206   0.7528   0.0386
  -2.000   0.3114   0.00784   0.00182  -0.1210   0.7514   0.0776
  -1.750   0.3391   0.00756   0.00172  -0.1214   0.7500   0.1408
  -1.500   0.3666   0.00716   0.00163  -0.1219   0.7486   0.2525
  -1.250   0.3944   0.00659   0.00154  -0.1227   0.7473   0.4161
  -1.000   0.4225   0.00563   0.00156  -0.1238   0.7460   0.7292
  -0.750   0.4508   0.00572   0.00171  -0.1239   0.7446   0.7705
  -0.500   0.4794   0.00581   0.00180  -0.1242   0.7430   0.7843
  -0.250   0.5083   0.00588   0.00185  -0.1246   0.7412   0.7927
   0.000   0.5363   0.00594   0.00193  -0.1247   0.7393   0.7983
   0.250   0.5650   0.00601   0.00198  -0.1250   0.7376   0.8037
   0.500   0.5937   0.00605   0.00201  -0.1254   0.7360   0.8076
   0.750   0.6220   0.00608   0.00203  -0.1257   0.7343   0.8098
   1.000   0.6507   0.00610   0.00205  -0.1261   0.7325   0.8110
   1.250   0.6791   0.00611   0.00208  -0.1264   0.7298   0.8120
   1.500   0.7075   0.00611   0.00209  -0.1268   0.7262   0.8131
   1.750   0.7358   0.00611   0.00209  -0.1271   0.7223   0.8141
   2.000   0.7641   0.00612   0.00208  -0.1274   0.7185   0.8149
   2.250   0.7923   0.00613   0.00212  -0.1277   0.7127   0.8156
   2.500   0.8199   0.00614   0.00211  -0.1279   0.7063   0.8164
   2.750   0.8477   0.00616   0.00214  -0.1281   0.6984   0.8171
   3.000   0.8748   0.00620   0.00215  -0.1282   0.6892   0.8177
   3.250   0.9011   0.00626   0.00220  -0.1281   0.6775   0.8183
   3.500   0.9267   0.00637   0.00226  -0.1279   0.6629   0.8188
   3.750   0.9509   0.00653   0.00236  -0.1274   0.6420   0.8195
   4.000   0.9727   0.00679   0.00250  -0.1264   0.6122   0.8202
   4.250   0.9827   0.00750   0.00287  -0.1231   0.5367   0.8210
   4.500   0.9849   0.00852   0.00346  -0.1184   0.4487   0.8219
   4.750   0.9880   0.00944   0.00401  -0.1140   0.3724   0.8228
   5.000   0.9908   0.01020   0.00450  -0.1095   0.3134   0.8238
   5.250   0.9947   0.01087   0.00496  -0.1053   0.2678   0.8247
   5.500   0.9987   0.01164   0.00552  -0.1012   0.2224   0.8257
   5.750   1.0056   0.01237   0.00608  -0.0979   0.1844   0.8269
   6.000   1.0141   0.01309   0.00667  -0.0949   0.1523   0.8279
   6.250   1.0246   0.01380   0.00726  -0.0925   0.1242   0.8288
   6.500   1.0356   0.01453   0.00787  -0.0902   0.0985   0.8296
   6.750   1.0477   0.01526   0.00850  -0.0881   0.0759   0.8304
   7.000   1.0610   0.01596   0.00912  -0.0863   0.0576   0.8311
   7.250   1.0758   0.01661   0.00972  -0.0847   0.0453   0.8318
   7.500   1.0913   0.01723   0.01031  -0.0833   0.0363   0.8325
   7.750   1.1068   0.01788   0.01093  -0.0819   0.0288   0.8331
   8.000   1.1232   0.01848   0.01153  -0.0807   0.0246   0.8337
   8.250   1.1394   0.01911   0.01216  -0.0795   0.0208   0.8343
   8.500   1.1565   0.01969   0.01277  -0.0784   0.0193   0.8349
   8.750   1.1729   0.02031   0.01341  -0.0772   0.0175   0.8357
   9.000   1.1884   0.02100   0.01412  -0.0760   0.0154   0.8365
   9.250   1.2049   0.02164   0.01479  -0.0749   0.0143   0.8373
   9.500   1.2216   0.02227   0.01547  -0.0738   0.0135   0.8382
   9.750   1.2375   0.02296   0.01620  -0.0728   0.0125   0.8390
  10.000   1.2530   0.02370   0.01696  -0.0716   0.0114   0.8398
  10.250   1.2673   0.02453   0.01782  -0.0704   0.0101   0.8405
  10.500   1.2834   0.02523   0.01856  -0.0694   0.0095   0.8413
  10.750   1.2988   0.02599   0.01937  -0.0684   0.0088   0.8421
  11.000   1.3136   0.02682   0.02023  -0.0673   0.0080   0.8428
  11.250   1.3272   0.02773   0.02117  -0.0662   0.0072   0.8436
  11.500   1.3411   0.02865   0.02213  -0.0651   0.0067   0.8444
  11.750   1.3555   0.02954   0.02308  -0.0640   0.0062   0.8452
  12.000   1.3690   0.03051   0.02412  -0.0630   0.0057   0.8461
  12.250   1.3818   0.03156   0.02520  -0.0619   0.0051   0.8469
  12.500   1.3935   0.03273   0.02641  -0.0607   0.0045   0.8476
  12.750   1.4059   0.03384   0.02758  -0.0597   0.0043   0.8484
  13.000   1.4180   0.03501   0.02882  -0.0587   0.0041   0.8493
  13.250   1.4296   0.03623   0.03013  -0.0577   0.0038   0.8502
  13.500   1.4404   0.03754   0.03150  -0.0566   0.0036   0.8512
  13.750   1.4509   0.03890   0.03293  -0.0557   0.0033   0.8522
  14.000   1.4605   0.04039   0.03449  -0.0547   0.0032   0.8533
  14.250   1.4687   0.04205   0.03625  -0.0536   0.0029   0.8544
  14.500   1.4752   0.04391   0.03821  -0.0525   0.0027   0.8556
  14.750   1.4835   0.04562   0.04001  -0.0517   0.0027   0.8568
  15.000   1.4914   0.04739   0.04187  -0.0509   0.0026   0.8581
  15.250   1.4991   0.04923   0.04381  -0.0502   0.0026   0.8595
  15.500   1.5054   0.05127   0.04596  -0.0495   0.0025   0.8609
  15.750   1.5113   0.05341   0.04819  -0.0488   0.0024   0.8623
  16.000   1.5166   0.05563   0.05052  -0.0483   0.0023   0.8639
  16.250   1.5204   0.05807   0.05308  -0.0478   0.0022   0.8656
  16.500   1.5245   0.06055   0.05566  -0.0474   0.0022   0.8673
  16.750   1.5268   0.06332   0.05855  -0.0472   0.0021   0.8692
  17.000   1.5282   0.06626   0.06163  -0.0470   0.0021   0.8712
  17.250   1.5285   0.06944   0.06493  -0.0470   0.0020   0.8732
  17.500   1.5279   0.07280   0.06841  -0.0472   0.0020   0.8753
  18.000   1.5231   0.08033   0.07621  -0.0481   0.0019   0.8801
  18.250   1.5190   0.08452   0.08054  -0.0489   0.0019   0.8830
  18.500   1.5137   0.08902   0.08517  -0.0500   0.0018   0.8862
  18.750   1.5065   0.09393   0.09024  -0.0514   0.0018   0.8894
  19.000   1.4980   0.09919   0.09565  -0.0532   0.0018   0.8932
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