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WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il)
Reynolds number: 1,000,000
Max Cl/Cd: 126.87 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx05188-il-1000000.txt
Download as CSV file: xf-fx05188-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 05-188 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  -0.5840   0.10069   0.09860  -0.0776   0.9546   0.0177
 -16.250  -0.5973   0.08979   0.08752  -0.0884   0.9422   0.0179
 -16.000  -0.6039   0.08054   0.07805  -0.0973   0.9262   0.0164
 -15.750  -0.6244   0.06995   0.06711  -0.1079   0.9049   0.0164
 -15.500  -0.6424   0.06110   0.05792  -0.1166   0.8888   0.0161
 -15.250  -0.6500   0.05506   0.05157  -0.1227   0.8750   0.0162
 -15.000  -0.6599   0.04990   0.04612  -0.1265   0.8637   0.0161
 -14.750  -0.6657   0.04602   0.04201  -0.1287   0.8552   0.0161
 -14.500  -0.6704   0.04253   0.03827  -0.1302   0.8475   0.0161
 -14.250  -0.6705   0.03977   0.03531  -0.1310   0.8409   0.0160
 -14.000  -0.6686   0.03728   0.03264  -0.1312   0.8349   0.0160
 -13.750  -0.6615   0.03543   0.03061  -0.1316   0.8288   0.0162
 -13.500  -0.6542   0.03376   0.02881  -0.1314   0.8236   0.0164
 -13.250  -0.6455   0.03227   0.02718  -0.1312   0.8181   0.0165
 -13.000  -0.6367   0.03134   0.02612  -0.1310   0.8123   0.0169
 -12.750  -0.6257   0.03004   0.02470  -0.1305   0.8075   0.0169
 -12.500  -0.6111   0.02869   0.02324  -0.1300   0.8026   0.0169
 -12.250  -0.5985   0.02772   0.02216  -0.1294   0.7975   0.0170
 -12.000  -0.5926   0.02711   0.02143  -0.1285   0.7922   0.0172
 -11.750  -0.5745   0.02597   0.02020  -0.1279   0.7882   0.0173
 -11.500  -0.5468   0.02460   0.01874  -0.1278   0.7847   0.0174
 -11.250  -0.5252   0.02377   0.01785  -0.1274   0.7811   0.0176
 -11.000  -0.5047   0.02297   0.01702  -0.1269   0.7774   0.0179
 -10.750  -0.4865   0.02224   0.01628  -0.1262   0.7741   0.0181
 -10.500  -0.4688   0.02158   0.01559  -0.1255   0.7704   0.0182
 -10.250  -0.4517   0.02091   0.01489  -0.1248   0.7668   0.0184
 -10.000  -0.4344   0.02033   0.01426  -0.1241   0.7633   0.0186
  -9.750  -0.4178   0.01969   0.01359  -0.1232   0.7601   0.0188
  -9.500  -0.4009   0.01910   0.01299  -0.1224   0.7569   0.0192
  -9.250  -0.3846   0.01850   0.01235  -0.1215   0.7539   0.0194
  -9.000  -0.3688   0.01791   0.01172  -0.1204   0.7509   0.0195
  -8.750  -0.3528   0.01734   0.01112  -0.1194   0.7481   0.0198
  -8.500  -0.3371   0.01678   0.01051  -0.1183   0.7454   0.0202
  -8.250  -0.3205   0.01628   0.01000  -0.1173   0.7434   0.0205
  -8.000  -0.3038   0.01579   0.00950  -0.1163   0.7410   0.0207
  -7.750  -0.2864   0.01537   0.00904  -0.1152   0.7387   0.0210
  -7.500  -0.2759   0.01467   0.00830  -0.1133   0.7364   0.0214
  -7.250  -0.2678   0.01395   0.00755  -0.1109   0.7339   0.0218
  -7.000  -0.2581   0.01350   0.00705  -0.1085   0.7312   0.0220
  -6.750  -0.2452   0.01306   0.00659  -0.1068   0.7291   0.0225
  -6.500  -0.2272   0.01263   0.00614  -0.1060   0.7274   0.0231
  -6.250  -0.2065   0.01226   0.00577  -0.1055   0.7256   0.0236
  -6.000  -0.1845   0.01195   0.00544  -0.1050   0.7236   0.0243
  -5.750  -0.1613   0.01168   0.00514  -0.1047   0.7216   0.0249
  -5.500  -0.1371   0.01144   0.00488  -0.1046   0.7195   0.0255
  -5.250  -0.1132   0.01113   0.00454  -0.1044   0.7175   0.0269
  -5.000  -0.0877   0.01091   0.00429  -0.1045   0.7154   0.0288
  -4.750  -0.0611   0.01073   0.00410  -0.1047   0.7131   0.0313
  -4.500  -0.0361   0.01038   0.00384  -0.1047   0.7118   0.0459
  -4.250  -0.0151   0.00938   0.00334  -0.1049   0.7100   0.1616
  -4.000   0.0091   0.00791   0.00268  -0.1064   0.7079   0.3670
  -3.750   0.0393   0.00725   0.00239  -0.1080   0.7058   0.4680
  -3.500   0.0700   0.00699   0.00228  -0.1090   0.7038   0.5199
  -3.250   0.1005   0.00685   0.00222  -0.1099   0.7018   0.5524
  -3.000   0.1311   0.00677   0.00220  -0.1108   0.6997   0.5790
  -2.750   0.1618   0.00679   0.00224  -0.1116   0.6971   0.5977
  -2.500   0.1919   0.00680   0.00228  -0.1122   0.6952   0.6114
  -2.250   0.2218   0.00681   0.00229  -0.1128   0.6933   0.6225
  -2.000   0.2515   0.00685   0.00235  -0.1133   0.6911   0.6329
  -1.750   0.2815   0.00688   0.00236  -0.1139   0.6888   0.6390
  -1.500   0.3113   0.00694   0.00242  -0.1144   0.6865   0.6446
  -1.250   0.3413   0.00700   0.00244  -0.1149   0.6842   0.6500
  -1.000   0.3714   0.00706   0.00245  -0.1156   0.6815   0.6535
  -0.750   0.4010   0.00713   0.00252  -0.1161   0.6784   0.6565
  -0.500   0.4300   0.00713   0.00254  -0.1164   0.6757   0.6597
  -0.250   0.4593   0.00714   0.00255  -0.1168   0.6724   0.6631
   0.000   0.4888   0.00716   0.00255  -0.1173   0.6690   0.6664
   0.250   0.5184   0.00719   0.00255  -0.1178   0.6659   0.6693
   0.500   0.5476   0.00726   0.00260  -0.1183   0.6625   0.6722
   0.750   0.5764   0.00726   0.00266  -0.1186   0.6597   0.6750
   1.000   0.6054   0.00729   0.00270  -0.1189   0.6562   0.6781
   1.250   0.6346   0.00732   0.00274  -0.1194   0.6528   0.6812
   1.500   0.6640   0.00737   0.00276  -0.1198   0.6494   0.6836
   1.750   0.6930   0.00740   0.00277  -0.1203   0.6458   0.6859
   2.000   0.7218   0.00738   0.00280  -0.1206   0.6420   0.6880
   2.250   0.7503   0.00738   0.00283  -0.1209   0.6371   0.6900
   2.500   0.7782   0.00742   0.00285  -0.1211   0.6316   0.6920
   2.750   0.8067   0.00744   0.00291  -0.1214   0.6258   0.6942
   3.000   0.8348   0.00749   0.00295  -0.1216   0.6197   0.6964
   3.250   0.8628   0.00756   0.00301  -0.1218   0.6144   0.6983
   3.500   0.8913   0.00762   0.00308  -0.1222   0.6085   0.6999
   3.750   0.9182   0.00771   0.00313  -0.1222   0.6007   0.7013
   4.000   0.9450   0.00774   0.00316  -0.1222   0.5899   0.7035
   4.250   0.9709   0.00784   0.00325  -0.1220   0.5792   0.7052
   4.750   1.0215   0.00811   0.00349  -0.1214   0.5558   0.7087
   5.000   1.0466   0.00826   0.00362  -0.1211   0.5439   0.7105
   5.250   1.0708   0.00844   0.00377  -0.1206   0.5301   0.7122
   5.500   1.0945   0.00864   0.00393  -0.1200   0.5166   0.7137
   5.750   1.1177   0.00885   0.00411  -0.1194   0.5020   0.7151
   6.000   1.1400   0.00909   0.00430  -0.1186   0.4843   0.7164
   6.250   1.1579   0.00947   0.00457  -0.1170   0.4556   0.7175
   6.750   1.1791   0.01048   0.00528  -0.1111   0.3897   0.7211
   7.000   1.1860   0.01103   0.00571  -0.1074   0.3602   0.7227
   7.250   1.1882   0.01181   0.00631  -0.1031   0.3233   0.7242
   7.500   1.1826   0.01290   0.00717  -0.0978   0.2757   0.7258
   7.750   1.1758   0.01416   0.00820  -0.0926   0.2315   0.7274
   8.000   1.1704   0.01552   0.00937  -0.0882   0.1922   0.7291
   8.250   1.1692   0.01687   0.01055  -0.0846   0.1598   0.7308
   8.500   1.1698   0.01825   0.01178  -0.0815   0.1301   0.7323
   8.750   1.1692   0.01979   0.01315  -0.0785   0.0996   0.7337
   9.000   1.1759   0.02101   0.01429  -0.0764   0.0849   0.7348
   9.250   1.1864   0.02201   0.01528  -0.0749   0.0761   0.7369
   9.500   1.1976   0.02300   0.01627  -0.0735   0.0681   0.7386
   9.750   1.2071   0.02413   0.01738  -0.0719   0.0586   0.7400
  10.000   1.2124   0.02558   0.01873  -0.0701   0.0434   0.7414
  10.250   1.2181   0.02703   0.02013  -0.0683   0.0334   0.7427
  10.500   1.2285   0.02823   0.02133  -0.0671   0.0302   0.7439
  10.750   1.2391   0.02945   0.02257  -0.0660   0.0286   0.7450
  11.000   1.2487   0.03076   0.02391  -0.0648   0.0270   0.7461
  11.250   1.2598   0.03200   0.02519  -0.0638   0.0262   0.7473
  11.500   1.2719   0.03320   0.02644  -0.0630   0.0256   0.7485
  11.750   1.2830   0.03451   0.02779  -0.0621   0.0250   0.7498
  12.000   1.2938   0.03587   0.02919  -0.0613   0.0243   0.7508
  12.250   1.3033   0.03737   0.03072  -0.0604   0.0237   0.7518
  12.500   1.3117   0.03898   0.03238  -0.0596   0.0230   0.7533
  12.750   1.3167   0.04096   0.03443  -0.0586   0.0222   0.7546
  13.000   1.3260   0.04258   0.03612  -0.0579   0.0219   0.7560
  13.250   1.3362   0.04416   0.03776  -0.0573   0.0217   0.7574
  13.500   1.3455   0.04585   0.03951  -0.0568   0.0214   0.7588
  13.750   1.3551   0.04755   0.04127  -0.0563   0.0211   0.7602
  14.000   1.3628   0.04948   0.04327  -0.0558   0.0207   0.7617
  14.250   1.3711   0.05138   0.04523  -0.0554   0.0204   0.7632
  14.500   1.3784   0.05344   0.04735  -0.0551   0.0201   0.7648
  14.750   1.3856   0.05553   0.04949  -0.0548   0.0197   0.7664
  15.000   1.3911   0.05787   0.05188  -0.0545   0.0194   0.7679
  15.250   1.3961   0.06029   0.05437  -0.0544   0.0191   0.7698
  15.500   1.3970   0.06325   0.05740  -0.0542   0.0186   0.7716
  15.750   1.3944   0.06669   0.06094  -0.0541   0.0183   0.7731
  16.000   1.3982   0.06942   0.06375  -0.0541   0.0181   0.7750
  16.250   1.4057   0.07177   0.06617  -0.0544   0.0179   0.7770
  16.500   1.4125   0.07422   0.06869  -0.0546   0.0178   0.7792
  16.750   1.4181   0.07688   0.07143  -0.0550   0.0176   0.7813
  17.000   1.4239   0.07952   0.07413  -0.0553   0.0174   0.7834
  17.250   1.4283   0.08239   0.07709  -0.0558   0.0171   0.7856
  17.500   1.4331   0.08521   0.08000  -0.0564   0.0169   0.7879
  17.750   1.4371   0.08822   0.08309  -0.0570   0.0167   0.7904
  18.000   1.4418   0.09113   0.08608  -0.0577   0.0164   0.7930
  18.250   1.4453   0.09427   0.08928  -0.0585   0.0162   0.7957
  18.500   1.4488   0.09740   0.09247  -0.0594   0.0160   0.7984
  18.750   1.4512   0.10073   0.09587  -0.0604   0.0158   0.8009
  19.000   1.4532   0.10412   0.09934  -0.0615   0.0156   0.8037
  19.250   1.4544   0.10766   0.10296  -0.0627   0.0154   0.8066
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