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DORNIER A-5 AIRFOIL (doa5-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: DORNIER A-5 AIRFOIL (doa5-il)
Reynolds number: 1,000,000
Max Cl/Cd: 68.73 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-doa5-il-1000000-n5.txt
Download as CSV file: xf-doa5-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DORNIER A-5 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0826   0.08017   0.07696  -0.0819   1.0000   0.0172
 -19.500  -1.0957   0.07489   0.07156  -0.0844   0.9999   0.0173
 -19.250  -1.1007   0.07035   0.06691  -0.0872   0.9996   0.0174
 -19.000  -1.1004   0.06667   0.06315  -0.0894   0.9993   0.0176
 -18.750  -1.1020   0.06288   0.05926  -0.0916   0.9990   0.0177
 -18.500  -1.1031   0.05924   0.05551  -0.0936   0.9985   0.0178
 -18.250  -1.0986   0.05637   0.05256  -0.0953   0.9980   0.0180
 -18.000  -1.0943   0.05357   0.04967  -0.0968   0.9974   0.0182
 -17.750  -1.0879   0.05107   0.04709  -0.0982   0.9967   0.0184
 -17.500  -1.0796   0.04881   0.04474  -0.0994   0.9960   0.0186
 -17.250  -1.0709   0.04664   0.04248  -0.1006   0.9952   0.0187
 -17.000  -1.0610   0.04463   0.04039  -0.1017   0.9945   0.0189
 -16.500  -1.0401   0.04096   0.03655  -0.1032   0.9927   0.0191
 -16.250  -1.0290   0.03935   0.03487  -0.1036   0.9915   0.0192
 -16.000  -1.0187   0.03762   0.03306  -0.1042   0.9900   0.0193
 -15.750  -1.0106   0.03571   0.03109  -0.1046   0.9886   0.0197
 -15.500  -0.9980   0.03420   0.02952  -0.1052   0.9872   0.0198
 -15.250  -0.9825   0.03291   0.02820  -0.1059   0.9859   0.0201
 -15.000  -0.9671   0.03162   0.02686  -0.1066   0.9848   0.0202
 -14.750  -0.9484   0.03058   0.02578  -0.1074   0.9839   0.0204
 -14.500  -0.9319   0.02955   0.02470  -0.1077   0.9825   0.0207
 -14.250  -0.9188   0.02861   0.02373  -0.1071   0.9800   0.0209
 -14.000  -0.9031   0.02757   0.02263  -0.1072   0.9781   0.0210
 -13.750  -0.8842   0.02666   0.02168  -0.1076   0.9765   0.0213
 -13.500  -0.8644   0.02575   0.02072  -0.1082   0.9752   0.0215
 -13.250  -0.8437   0.02486   0.01978  -0.1088   0.9741   0.0217
 -13.000  -0.8210   0.02410   0.01898  -0.1096   0.9731   0.0221
 -12.750  -0.7985   0.02326   0.01809  -0.1104   0.9723   0.0223
 -12.500  -0.7820   0.02252   0.01730  -0.1099   0.9694   0.0224
 -12.250  -0.7611   0.02180   0.01654  -0.1101   0.9672   0.0226
 -12.000  -0.7383   0.02106   0.01575  -0.1107   0.9652   0.0227
 -11.750  -0.7117   0.02039   0.01504  -0.1119   0.9636   0.0229
 -11.500  -0.6857   0.01954   0.01416  -0.1134   0.9621   0.0232
 -11.000  -0.6458   0.01816   0.01273  -0.1133   0.9544   0.0239
 -10.750  -0.6224   0.01755   0.01209  -0.1138   0.9508   0.0241
 -10.500  -0.5940   0.01695   0.01147  -0.1153   0.9485   0.0244
 -10.250  -0.5816   0.01649   0.01098  -0.1133   0.9404   0.0247
 -10.000  -0.5542   0.01594   0.01041  -0.1144   0.9359   0.0250
  -9.750  -0.5294   0.01543   0.00987  -0.1150   0.9308   0.0253
  -9.500  -0.4984   0.01491   0.00932  -0.1167   0.9263   0.0256
  -9.250  -0.4623   0.01442   0.00878  -0.1195   0.9228   0.0260
  -9.000  -0.4338   0.01395   0.00828  -0.1208   0.9177   0.0262
  -8.750  -0.4053   0.01352   0.00781  -0.1219   0.9123   0.0267
  -8.500  -0.3752   0.01312   0.00736  -0.1233   0.9077   0.0270
  -8.250  -0.3623   0.01263   0.00684  -0.1215   0.9001   0.0274
  -8.000  -0.3444   0.01221   0.00637  -0.1205   0.8932   0.0279
  -7.750  -0.3287   0.01187   0.00601  -0.1189   0.8858   0.0282
  -7.500  -0.3095   0.01156   0.00568  -0.1177   0.8772   0.0288
  -7.250  -0.2906   0.01130   0.00539  -0.1164   0.8673   0.0293
  -7.000  -0.2693   0.01106   0.00510  -0.1156   0.8571   0.0299
  -6.500  -0.2255   0.01066   0.00458  -0.1139   0.8390   0.0311
  -6.250  -0.2030   0.01049   0.00435  -0.1131   0.8308   0.0318
  -6.000  -0.1807   0.01029   0.00412  -0.1123   0.8242   0.0331
  -5.750  -0.1577   0.01013   0.00393  -0.1116   0.8170   0.0343
  -5.500  -0.1332   0.00998   0.00376  -0.1112   0.8125   0.0358
  -5.250  -0.1094   0.00981   0.00359  -0.1106   0.8082   0.0377
  -5.000  -0.0855   0.00963   0.00341  -0.1100   0.8038   0.0406
  -4.750  -0.0607   0.00948   0.00326  -0.1096   0.7997   0.0435
  -4.500  -0.0356   0.00932   0.00311  -0.1093   0.7966   0.0485
  -4.250  -0.0102   0.00916   0.00299  -0.1090   0.7934   0.0571
  -4.000   0.0149   0.00901   0.00288  -0.1086   0.7899   0.0646
  -3.750   0.0391   0.00888   0.00275  -0.1080   0.7833   0.0695
  -3.500   0.0635   0.00879   0.00264  -0.1074   0.7758   0.0741
  -3.250   0.0880   0.00868   0.00253  -0.1068   0.7683   0.0782
  -3.000   0.1118   0.00855   0.00241  -0.1061   0.7594   0.0847
  -2.750   0.1354   0.00836   0.00229  -0.1054   0.7504   0.1049
  -2.500   0.1570   0.00815   0.00216  -0.1043   0.7381   0.1401
  -2.250   0.1798   0.00803   0.00206  -0.1034   0.7262   0.1652
  -2.000   0.2006   0.00777   0.00192  -0.1022   0.7133   0.2138
  -1.750   0.2115   0.00651   0.00147  -0.0998   0.6992   0.4750
  -1.500   0.2309   0.00643   0.00143  -0.0981   0.6757   0.5172
  -1.250   0.2506   0.00646   0.00142  -0.0964   0.6556   0.5352
  -1.000   0.2718   0.00649   0.00143  -0.0950   0.6392   0.5515
  -0.750   0.2923   0.00656   0.00145  -0.0935   0.6194   0.5619
  -0.500   0.3108   0.00670   0.00148  -0.0915   0.5917   0.5691
  -0.250   0.3282   0.00687   0.00153  -0.0893   0.5627   0.5751
   0.000   0.3478   0.00702   0.00160  -0.0876   0.5399   0.5832
   0.250   0.3634   0.00731   0.00170  -0.0851   0.4919   0.5915
   0.500   0.3761   0.00772   0.00187  -0.0820   0.4230   0.5996
   0.750   0.3934   0.00804   0.00202  -0.0800   0.3905   0.6060
   1.000   0.4140   0.00823   0.00214  -0.0785   0.3688   0.6130
   1.250   0.4348   0.00843   0.00226  -0.0771   0.3464   0.6188
   1.500   0.4569   0.00861   0.00235  -0.0760   0.3321   0.6232
   1.750   0.4791   0.00875   0.00246  -0.0749   0.3201   0.6274
   2.000   0.5017   0.00889   0.00257  -0.0739   0.3081   0.6341
   2.250   0.5241   0.00904   0.00268  -0.0729   0.2971   0.6400
   2.500   0.5452   0.00923   0.00282  -0.0716   0.2807   0.6456
   2.750   0.5677   0.00936   0.00295  -0.0705   0.2699   0.6523
   3.000   0.5872   0.00962   0.00310  -0.0690   0.2450   0.6568
   3.250   0.6016   0.01008   0.00335  -0.0665   0.1994   0.6609
   3.500   0.6199   0.01040   0.00358  -0.0647   0.1762   0.6657
   3.750   0.6400   0.01065   0.00377  -0.0633   0.1635   0.6705
   4.000   0.6616   0.01085   0.00393  -0.0622   0.1577   0.6740
   4.250   0.6833   0.01103   0.00411  -0.0611   0.1538   0.6775
   4.500   0.7049   0.01121   0.00429  -0.0600   0.1496   0.6811
   4.750   0.7270   0.01138   0.00447  -0.0590   0.1468   0.6859
   5.000   0.7493   0.01155   0.00464  -0.0580   0.1447   0.6886
   5.250   0.7711   0.01173   0.00484  -0.0570   0.1422   0.6933
   5.500   0.7926   0.01193   0.00505  -0.0559   0.1395   0.6970
   5.750   0.8134   0.01217   0.00528  -0.0547   0.1357   0.7004
   6.000   0.8347   0.01237   0.00549  -0.0536   0.1331   0.7036
   6.250   0.8566   0.01256   0.00569  -0.0526   0.1304   0.7064
   6.500   0.8773   0.01280   0.00593  -0.0515   0.1240   0.7091
   6.750   0.8976   0.01306   0.00618  -0.0502   0.1178   0.7116
   7.000   0.9167   0.01338   0.00645  -0.0489   0.1073   0.7142
   7.250   0.9359   0.01369   0.00673  -0.0475   0.1025   0.7169
   7.500   0.9553   0.01400   0.00702  -0.0462   0.0983   0.7194
   7.750   0.9751   0.01430   0.00731  -0.0450   0.0953   0.7217
   8.000   0.9942   0.01462   0.00763  -0.0437   0.0929   0.7241
   8.250   1.0120   0.01500   0.00801  -0.0422   0.0895   0.7263
   8.500   1.0305   0.01535   0.00839  -0.0408   0.0869   0.7287
   8.750   1.0501   0.01565   0.00872  -0.0396   0.0856   0.7312
   9.000   1.0695   0.01597   0.00907  -0.0384   0.0837   0.7336
   9.250   1.0885   0.01631   0.00944  -0.0372   0.0816   0.7361
   9.500   1.1065   0.01671   0.00984  -0.0359   0.0785   0.7381
   9.750   1.1239   0.01713   0.01025  -0.0345   0.0758   0.7396
  10.000   1.1420   0.01752   0.01066  -0.0332   0.0727   0.7410
  10.250   1.1596   0.01793   0.01110  -0.0319   0.0704   0.7424
  10.500   1.1759   0.01842   0.01157  -0.0304   0.0669   0.7438
  10.750   1.1927   0.01888   0.01205  -0.0290   0.0651   0.7452
  11.000   1.2093   0.01936   0.01256  -0.0277   0.0633   0.7467
  11.250   1.2248   0.01992   0.01311  -0.0262   0.0609   0.7483
  11.500   1.2400   0.02050   0.01371  -0.0247   0.0588   0.7499
  11.750   1.2565   0.02101   0.01425  -0.0235   0.0578   0.7514
  12.000   1.2720   0.02157   0.01485  -0.0221   0.0564   0.7527
  12.250   1.2865   0.02222   0.01551  -0.0207   0.0542   0.7540
  12.500   1.3000   0.02293   0.01623  -0.0192   0.0522   0.7553
  12.750   1.3141   0.02362   0.01695  -0.0178   0.0507   0.7567
  13.000   1.3293   0.02423   0.01761  -0.0166   0.0496   0.7584
  13.250   1.3432   0.02492   0.01836  -0.0153   0.0480   0.7600
  13.500   1.3562   0.02571   0.01916  -0.0139   0.0454   0.7614
  13.750   1.3681   0.02657   0.02004  -0.0125   0.0439   0.7626
  14.000   1.3811   0.02738   0.02088  -0.0113   0.0417   0.7639
  14.250   1.3932   0.02827   0.02180  -0.0100   0.0399   0.7652
  14.500   1.4034   0.02929   0.02285  -0.0086   0.0379   0.7664
  14.750   1.4147   0.03028   0.02386  -0.0074   0.0360   0.7674
  15.000   1.4245   0.03138   0.02499  -0.0061   0.0346   0.7684
  15.250   1.4337   0.03256   0.02620  -0.0048   0.0330   0.7693
  15.500   1.4430   0.03375   0.02743  -0.0036   0.0320   0.7703
  15.750   1.4524   0.03497   0.02870  -0.0025   0.0308   0.7712
  16.000   1.4602   0.03634   0.03011  -0.0014   0.0297   0.7719
  16.250   1.4673   0.03780   0.03161  -0.0004   0.0285   0.7729
  16.500   1.4737   0.03935   0.03323   0.0006   0.0274   0.7738
  16.750   1.4816   0.04083   0.03477   0.0014   0.0267   0.7748
  17.000   1.4878   0.04250   0.03650   0.0022   0.0259   0.7757
  17.250   1.4925   0.04433   0.03839   0.0030   0.0248   0.7765
  17.500   1.4956   0.04638   0.04049   0.0036   0.0239   0.7773
  17.750   1.5003   0.04834   0.04253   0.0041   0.0232   0.7782
  18.000   1.5039   0.05047   0.04473   0.0045   0.0224   0.7789
  18.250   1.5068   0.05273   0.04706   0.0048   0.0217   0.7798
  18.500   1.5076   0.05527   0.04966   0.0050   0.0208   0.7805
  18.750   1.5069   0.05806   0.05252   0.0050   0.0200   0.7812
  19.000   1.5072   0.06082   0.05537   0.0048   0.0192   0.7819
  19.250   1.5059   0.06386   0.05849   0.0044   0.0184   0.7826
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