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GOE 435 AIRFOIL (goe435-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 435 AIRFOIL (goe435-il)
Reynolds number: 200,000
Max Cl/Cd: 52.39 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe435-il-200000.txt
Download as CSV file: xf-goe435-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 435 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.5181   0.10003   0.09519  -0.0740   1.0000   0.1080
 -15.750  -0.5203   0.09727   0.09249  -0.0755   0.9965   0.1096
 -15.500  -0.5042   0.09374   0.08898  -0.0800   0.9887   0.1117
 -15.250  -0.4524   0.09526   0.09059  -0.0823   0.9774   0.1127
 -15.000  -0.4103   0.09586   0.09123  -0.0845   0.9642   0.1138
 -14.750  -0.3852   0.09486   0.09025  -0.0863   0.9500   0.1157
 -14.500  -0.6346   0.05751   0.05218  -0.1067   0.9416   0.1369
 -14.250  -0.6475   0.05319   0.04769  -0.1093   0.9262   0.1418
 -14.000  -0.6723   0.04810   0.04228  -0.1118   0.9126   0.1462
 -13.750  -0.6671   0.04639   0.04054  -0.1125   0.8996   0.1493
 -13.500  -0.6739   0.04349   0.03746  -0.1139   0.8889   0.1528
 -13.250  -0.6878   0.03978   0.03346  -0.1165   0.8777   0.1559
 -13.000  -0.6805   0.03839   0.03200  -0.1168   0.8699   0.1583
 -12.750  -0.6660   0.03745   0.03108  -0.1177   0.8616   0.1611
 -12.500  -0.6597   0.03589   0.02942  -0.1189   0.8534   0.1642
 -12.250  -0.6595   0.03396   0.02727  -0.1203   0.8463   0.1669
 -12.000  -0.6604   0.03210   0.02518  -0.1222   0.8386   0.1689
 -11.750  -0.6427   0.03150   0.02461  -0.1222   0.8321   0.1713
 -11.500  -0.6240   0.03119   0.02433  -0.1219   0.8262   0.1739
 -11.250  -0.6077   0.03069   0.02375  -0.1224   0.8207   0.1768
 -11.000  -0.5918   0.03007   0.02304  -0.1233   0.8145   0.1794
 -10.750  -0.5758   0.02949   0.02230  -0.1238   0.8079   0.1817
 -10.500  -0.5581   0.02904   0.02164  -0.1241   0.8019   0.1835
 -10.250  -0.5337   0.02836   0.02096  -0.1238   0.7968   0.1860
 -10.000  -0.5085   0.02813   0.02080  -0.1238   0.7909   0.1884
  -9.750  -0.4845   0.02788   0.02057  -0.1238   0.7842   0.1911
  -9.500  -0.4612   0.02756   0.02016  -0.1239   0.7781   0.1939
  -9.250  -0.4373   0.02718   0.01963  -0.1240   0.7728   0.1961
  -9.000  -0.4136   0.02692   0.01923  -0.1243   0.7670   0.1979
  -8.750  -0.3898   0.02659   0.01879  -0.1244   0.7602   0.1993
  -8.500  -0.3643   0.02582   0.01804  -0.1244   0.7537   0.2013
  -8.250  -0.3372   0.02539   0.01760  -0.1243   0.7480   0.2032
  -8.000  -0.3104   0.02513   0.01730  -0.1244   0.7422   0.2050
  -7.750  -0.2851   0.02483   0.01702  -0.1244   0.7347   0.2071
  -7.500  -0.2586   0.02447   0.01659  -0.1244   0.7275   0.2087
  -7.250  -0.2309   0.02409   0.01609  -0.1246   0.7212   0.2101
  -7.000  -0.2039   0.02383   0.01572  -0.1247   0.7145   0.2114
  -6.750  -0.1779   0.02352   0.01537  -0.1247   0.7064   0.2127
  -6.500  -0.1500   0.02322   0.01496  -0.1249   0.6995   0.2139
  -6.250  -0.1214   0.02289   0.01449  -0.1252   0.6937   0.2152
  -6.000  -0.0950   0.02243   0.01407  -0.1252   0.6868   0.2172
  -5.750  -0.0683   0.02208   0.01376  -0.1251   0.6793   0.2187
  -5.500  -0.0399   0.02176   0.01341  -0.1253   0.6731   0.2201
  -5.250  -0.0105   0.02149   0.01306  -0.1255   0.6680   0.2213
  -5.000   0.0166   0.02131   0.01288  -0.1256   0.6614   0.2226
  -4.750   0.0441   0.02108   0.01265  -0.1256   0.6546   0.2242
  -4.500   0.0732   0.02083   0.01234  -0.1259   0.6492   0.2260
  -4.250   0.1031   0.02062   0.01204  -0.1263   0.6448   0.2277
  -4.000   0.1312   0.02052   0.01191  -0.1265   0.6397   0.2291
  -3.750   0.1588   0.02041   0.01179  -0.1266   0.6341   0.2304
  -3.500   0.1870   0.02011   0.01153  -0.1267   0.6291   0.2325
  -3.250   0.2163   0.01982   0.01126  -0.1270   0.6249   0.2349
  -3.000   0.2469   0.01965   0.01104  -0.1274   0.6211   0.2373
  -2.750   0.2730   0.01956   0.01104  -0.1273   0.6157   0.2395
  -2.500   0.3012   0.01939   0.01089  -0.1274   0.6100   0.2415
  -2.250   0.3312   0.01915   0.01058  -0.1277   0.6047   0.2434
  -2.000   0.3626   0.01897   0.01030  -0.1282   0.6000   0.2456
  -1.750   0.3886   0.01887   0.01031  -0.1281   0.5942   0.2482
  -1.500   0.4171   0.01870   0.01021  -0.1283   0.5892   0.2519
  -1.250   0.4472   0.01854   0.01006  -0.1288   0.5850   0.2568
  -1.000   0.4786   0.01842   0.00989  -0.1294   0.5812   0.2633
  -0.750   0.5069   0.01836   0.00995  -0.1298   0.5768   0.2740
  -0.500   0.5349   0.01829   0.01008  -0.1301   0.5721   0.2950
  -0.250   0.5645   0.01834   0.01030  -0.1305   0.5675   0.3344
   0.000   0.5958   0.01851   0.01040  -0.1309   0.5633   0.3647
   0.250   0.6281   0.01884   0.01060  -0.1315   0.5593   0.3836
   0.500   0.6530   0.01915   0.01107  -0.1310   0.5546   0.3951
   0.750   0.6810   0.01946   0.01130  -0.1310   0.5497   0.4061
   1.000   0.7095   0.01958   0.01149  -0.1309   0.5450   0.4145
   1.250   0.7406   0.01980   0.01162  -0.1313   0.5407   0.4231
   1.500   0.7683   0.02015   0.01190  -0.1313   0.5361   0.4306
   1.750   0.7924   0.02027   0.01218  -0.1306   0.5309   0.4370
   2.000   0.8195   0.02045   0.01238  -0.1304   0.5257   0.4437
   2.250   0.8496   0.02061   0.01245  -0.1306   0.5208   0.4508
   2.500   0.8795   0.02094   0.01265  -0.1310   0.5158   0.4559
   2.750   0.9011   0.02100   0.01287  -0.1301   0.5102   0.4612
   3.000   0.9264   0.02114   0.01306  -0.1296   0.5045   0.4668
   3.250   0.9554   0.02124   0.01310  -0.1297   0.4991   0.4718
   3.500   0.9846   0.02150   0.01327  -0.1300   0.4935   0.4765
   3.750   1.0046   0.02169   0.01353  -0.1288   0.4872   0.4802
   4.000   1.0295   0.02174   0.01357  -0.1284   0.4809   0.4844
   4.250   1.0583   0.02180   0.01359  -0.1285   0.4752   0.4896
   4.500   1.0798   0.02204   0.01389  -0.1275   0.4688   0.4940
   4.750   1.0988   0.02218   0.01409  -0.1262   0.4615   0.4977
   5.000   1.1238   0.02225   0.01409  -0.1258   0.4551   0.5019
   5.250   1.1474   0.02247   0.01426  -0.1252   0.4485   0.5059
   5.500   1.1618   0.02270   0.01454  -0.1232   0.4407   0.5092
   5.750   1.1834   0.02272   0.01455  -0.1223   0.4340   0.5140
   6.000   1.1979   0.02298   0.01486  -0.1203   0.4268   0.5186
   6.250   1.2067   0.02327   0.01522  -0.1175   0.4190   0.5231
   6.500   1.2295   0.02347   0.01529  -0.1168   0.4125   0.5286
   6.750   1.2379   0.02411   0.01601  -0.1144   0.4044   0.5328
   7.000   1.2538   0.02452   0.01639  -0.1131   0.3973   0.5371
   7.250   1.2689   0.02502   0.01692  -0.1117   0.3903   0.5418
   7.500   1.2798   0.02572   0.01767  -0.1100   0.3828   0.5469
   7.750   1.2999   0.02615   0.01799  -0.1092   0.3767   0.5538
   8.000   1.3089   0.02711   0.01902  -0.1075   0.3698   0.5600
   8.250   1.3232   0.02780   0.01974  -0.1063   0.3637   0.5671
   8.500   1.3432   0.02834   0.02021  -0.1056   0.3582   0.5755
   8.750   1.3516   0.02945   0.02142  -0.1041   0.3522   0.5835
   9.000   1.3661   0.03026   0.02224  -0.1031   0.3466   0.5922
   9.250   1.3885   0.03074   0.02265  -0.1027   0.3414   0.6030
   9.500   1.3950   0.03207   0.02411  -0.1012   0.3361   0.6149
   9.750   1.4066   0.03309   0.02524  -0.1001   0.3311   0.6290
  10.000   1.4282   0.03360   0.02571  -0.0996   0.3265   0.6495
  10.250   1.4412   0.03465   0.02687  -0.0986   0.3221   0.6734
  10.500   1.4475   0.03604   0.02844  -0.0972   0.3176   0.6998
  10.750   1.4587   0.03714   0.02963  -0.0960   0.3134   0.7309
  11.000   1.4795   0.03767   0.03011  -0.0954   0.3095   0.7652
  11.250   1.4961   0.03846   0.03095  -0.0944   0.3058   0.7960
  11.500   1.4972   0.04015   0.03282  -0.0927   0.3023   0.8242
  11.750   1.5031   0.04133   0.03417  -0.0910   0.2989   0.8639
  12.000   1.5098   0.04210   0.03503  -0.0891   0.2958   1.0000
  12.250   1.5318   0.04281   0.03563  -0.0891   0.2927   1.0000
  12.500   1.5630   0.04305   0.03572  -0.0895   0.2895   1.0000
  12.750   1.5573   0.04557   0.03840  -0.0881   0.2867   1.0000
  13.000   1.5585   0.04772   0.04065  -0.0872   0.2836   1.0000
  13.250   1.5653   0.04949   0.04245  -0.0866   0.2804   1.0000
  13.500   1.5790   0.05070   0.04363  -0.0861   0.2774   1.0000
  13.750   1.6026   0.05117   0.04398  -0.0860   0.2745   1.0000
  14.000   1.6212   0.05214   0.04492  -0.0857   0.2717   1.0000
  14.250   1.6065   0.05567   0.04865  -0.0845   0.2690   1.0000
  14.500   1.6008   0.05864   0.05174  -0.0837   0.2662   1.0000
  14.750   1.6025   0.06101   0.05418  -0.0832   0.2635   1.0000
  15.000   1.6131   0.06257   0.05574  -0.0828   0.2611   1.0000
  15.250   1.6317   0.06336   0.05649  -0.0826   0.2589   1.0000
  15.500   1.6599   0.06334   0.05637  -0.0824   0.2569   1.0000
  15.750   1.6603   0.06595   0.05907  -0.0819   0.2547   1.0000
  16.000   1.6250   0.07213   0.06553  -0.0813   0.2522   1.0000
  16.250   1.5943   0.07824   0.07187  -0.0811   0.2493   1.0000
  16.500   1.5779   0.08300   0.07677  -0.0812   0.2467   1.0000
  16.750   1.5822   0.08540   0.07920  -0.0812   0.2446   1.0000
  17.000   1.6046   0.08564   0.07938  -0.0810   0.2429   1.0000
  17.250   1.6380   0.08461   0.07825  -0.0807   0.2414   1.0000
  17.500   1.6662   0.08430   0.07787  -0.0803   0.2396   1.0000
  17.750   0.9888   0.19973   0.19514  -0.1241   0.1994   1.0000
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