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GOE 289 (MVA 289) AIRFOIL (goe289-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 289 (MVA 289) AIRFOIL (goe289-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.93 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe289-il-1000000.txt
Download as CSV file: xf-goe289-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 289 (MVA 289) 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
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.1664   0.12764   0.12587  -0.0745   0.9862   0.0255
 -13.500  -0.1498   0.12499   0.12322  -0.0771   0.9835   0.0257
 -13.250  -0.4650   0.05452   0.05213  -0.1199   0.9724   0.0253
 -12.500  -0.4550   0.03071   0.02741  -0.1636   0.9365   0.0253
 -12.250  -0.4485   0.02693   0.02328  -0.1672   0.9179   0.0254
 -12.000  -0.4424   0.02539   0.02154  -0.1661   0.9023   0.0255
 -11.750  -0.4357   0.02400   0.01999  -0.1644   0.8886   0.0257
 -11.500  -0.4258   0.02299   0.01887  -0.1625   0.8756   0.0259
 -11.250  -0.4154   0.02210   0.01787  -0.1604   0.8632   0.0260
 -11.000  -0.4029   0.02129   0.01693  -0.1586   0.8506   0.0262
 -10.750  -0.3886   0.02061   0.01613  -0.1568   0.8375   0.0263
 -10.500  -0.3737   0.01993   0.01533  -0.1550   0.8231   0.0265
 -10.250  -0.3566   0.01940   0.01471  -0.1535   0.8088   0.0268
 -10.000  -0.3398   0.01879   0.01397  -0.1520   0.7945   0.0271
  -9.750  -0.3226   0.01815   0.01320  -0.1504   0.7811   0.0272
  -9.500  -0.3046   0.01757   0.01248  -0.1489   0.7689   0.0274
  -9.250  -0.2854   0.01697   0.01177  -0.1476   0.7581   0.0275
  -9.000  -0.2655   0.01642   0.01111  -0.1464   0.7489   0.0277
  -8.750  -0.2448   0.01593   0.01051  -0.1452   0.7398   0.0279
  -8.500  -0.2236   0.01545   0.00993  -0.1442   0.7320   0.0282
  -8.250  -0.2017   0.01498   0.00938  -0.1432   0.7244   0.0283
  -8.000  -0.1798   0.01458   0.00888  -0.1421   0.7172   0.0285
  -7.750  -0.1567   0.01415   0.00839  -0.1413   0.7107   0.0287
  -7.500  -0.1336   0.01384   0.00799  -0.1404   0.7036   0.0289
  -7.250  -0.1100   0.01354   0.00762  -0.1397   0.6974   0.0291
  -7.000  -0.0862   0.01319   0.00722  -0.1389   0.6908   0.0293
  -6.750  -0.0668   0.01247   0.00642  -0.1375   0.6838   0.0298
  -6.500  -0.0440   0.01202   0.00595  -0.1366   0.6776   0.0302
  -6.250  -0.0204   0.01172   0.00561  -0.1358   0.6704   0.0306
  -6.000   0.0031   0.01147   0.00530  -0.1349   0.6633   0.0310
  -5.750   0.0277   0.01120   0.00499  -0.1342   0.6560   0.0314
  -5.500   0.0514   0.01100   0.00472  -0.1334   0.6481   0.0318
  -5.250   0.0763   0.01077   0.00445  -0.1327   0.6407   0.0322
  -5.000   0.1006   0.01059   0.00421  -0.1319   0.6327   0.0326
  -4.750   0.1254   0.01042   0.00399  -0.1313   0.6250   0.0330
  -4.500   0.1501   0.01027   0.00379  -0.1306   0.6164   0.0334
  -4.250   0.1748   0.01012   0.00358  -0.1298   0.6084   0.0338
  -4.000   0.1987   0.00989   0.00330  -0.1290   0.5998   0.0348
  -3.750   0.2232   0.00975   0.00311  -0.1282   0.5919   0.0357
  -3.500   0.2481   0.00964   0.00295  -0.1276   0.5837   0.0368
  -3.250   0.2728   0.00956   0.00283  -0.1268   0.5759   0.0381
  -3.000   0.2978   0.00946   0.00269  -0.1262   0.5679   0.0398
  -2.750   0.3218   0.00938   0.00257  -0.1253   0.5601   0.0429
  -2.500   0.3462   0.00918   0.00244  -0.1246   0.5530   0.0590
  -2.250   0.3691   0.00901   0.00238  -0.1236   0.5459   0.0982
  -2.000   0.3944   0.00895   0.00236  -0.1231   0.5399   0.1125
  -1.750   0.4197   0.00894   0.00234  -0.1225   0.5334   0.1224
  -1.500   0.4437   0.00894   0.00233  -0.1217   0.5266   0.1317
  -1.250   0.4695   0.00892   0.00231  -0.1212   0.5209   0.1401
  -1.000   0.4940   0.00891   0.00230  -0.1205   0.5145   0.1504
  -0.750   0.5180   0.00890   0.00230  -0.1197   0.5087   0.1629
  -0.500   0.5431   0.00884   0.00228  -0.1191   0.5036   0.1811
  -0.250   0.5664   0.00875   0.00229  -0.1182   0.4980   0.2172
   0.000   0.5882   0.00866   0.00233  -0.1171   0.4924   0.2765
   0.250   0.6127   0.00859   0.00237  -0.1164   0.4876   0.3189
   0.500   0.6366   0.00861   0.00242  -0.1156   0.4818   0.3468
   0.750   0.6591   0.00868   0.00249  -0.1145   0.4758   0.3665
   1.000   0.6840   0.00867   0.00253  -0.1139   0.4710   0.3867
   1.250   0.7070   0.00870   0.00257  -0.1129   0.4655   0.4022
   1.500   0.7275   0.00876   0.00262  -0.1114   0.4599   0.4158
   1.750   0.7504   0.00877   0.00266  -0.1103   0.4554   0.4309
   2.000   0.7722   0.00878   0.00272  -0.1091   0.4500   0.4516
   2.250   0.7917   0.00879   0.00280  -0.1075   0.4445   0.4886
   2.500   0.8099   0.00866   0.00293  -0.1056   0.4397   0.5899
   2.750   0.8239   0.00843   0.00308  -0.1027   0.4347   0.7305
   3.000   0.9685   0.00852   0.00359  -0.1286   0.4232   1.0000
   3.250   0.9894   0.00864   0.00367  -0.1272   0.4178   1.0000
   3.500   1.0071   0.00878   0.00377  -0.1252   0.4124   1.0000
   3.750   1.0246   0.00892   0.00388  -0.1231   0.4074   1.0000
   4.000   1.0441   0.00903   0.00397  -0.1214   0.4025   1.0000
   4.250   1.0623   0.00919   0.00409  -0.1195   0.3971   1.0000
   4.500   1.0802   0.00937   0.00423  -0.1176   0.3919   1.0000
   4.750   1.1013   0.00950   0.00435  -0.1163   0.3876   1.0000
   5.000   1.1210   0.00967   0.00450  -0.1148   0.3827   1.0000
   5.250   1.1392   0.00990   0.00468  -0.1131   0.3774   1.0000
   5.500   1.1605   0.01005   0.00484  -0.1120   0.3735   1.0000
   5.750   1.1813   0.01023   0.00500  -0.1107   0.3692   1.0000
   6.000   1.2007   0.01046   0.00520  -0.1093   0.3646   1.0000
   6.250   1.2191   0.01073   0.00545  -0.1077   0.3600   1.0000
   6.500   1.2412   0.01090   0.00563  -0.1069   0.3571   1.0000
   6.750   1.2622   0.01110   0.00584  -0.1058   0.3537   1.0000
   7.000   1.2819   0.01136   0.00609  -0.1045   0.3500   1.0000
   7.250   1.3000   0.01168   0.00638  -0.1031   0.3463   1.0000
   7.500   1.3201   0.01195   0.00665  -0.1019   0.3432   1.0000
   7.750   1.3418   0.01216   0.00689  -0.1011   0.3402   1.0000
   8.000   1.3613   0.01245   0.00718  -0.1000   0.3357   1.0000
   8.250   1.3785   0.01285   0.00755  -0.0985   0.3308   1.0000
   8.500   1.3974   0.01319   0.00789  -0.0973   0.3272   1.0000
   8.750   1.4186   0.01344   0.00817  -0.0965   0.3222   1.0000
   9.000   1.4369   0.01383   0.00855  -0.0954   0.3184   1.0000
   9.250   1.4527   0.01433   0.00903  -0.0938   0.3140   1.0000
   9.500   1.4724   0.01467   0.00941  -0.0929   0.3111   1.0000
   9.750   1.4924   0.01501   0.00978  -0.0921   0.3079   1.0000
  10.000   1.5107   0.01544   0.01022  -0.0911   0.3042   1.0000
  10.250   1.5255   0.01604   0.01080  -0.0896   0.2995   1.0000
  10.500   1.5429   0.01652   0.01132  -0.0885   0.2960   1.0000
  10.750   1.5620   0.01694   0.01176  -0.0877   0.2917   1.0000
  11.000   1.5776   0.01755   0.01237  -0.0865   0.2869   1.0000
  11.250   1.5905   0.01831   0.01313  -0.0850   0.2818   1.0000
  11.500   1.6089   0.01879   0.01366  -0.0842   0.2776   1.0000
  11.750   1.6216   0.01960   0.01446  -0.0828   0.2702   1.0000
  12.000   1.6344   0.02043   0.01529  -0.0815   0.2625   1.0000
  12.250   1.6419   0.02162   0.01644  -0.0797   0.2520   1.0000
  12.500   1.6462   0.02305   0.01781  -0.0777   0.2355   1.0000
  12.750   1.6384   0.02537   0.01999  -0.0747   0.2102   1.0000
  13.000   1.6218   0.02850   0.02296  -0.0714   0.1809   1.0000
  13.250   1.5857   0.03341   0.02764  -0.0672   0.1410   1.0000
  13.500   1.5571   0.03810   0.03220  -0.0642   0.1104   1.0000
  13.750   1.5292   0.04304   0.03706  -0.0618   0.0863   1.0000
  14.000   1.5096   0.04745   0.04143  -0.0602   0.0695   1.0000
  14.250   1.4869   0.05242   0.04635  -0.0588   0.0499   1.0000
  14.500   1.4648   0.05753   0.05143  -0.0578   0.0347   1.0000
  14.750   1.4519   0.06183   0.05576  -0.0572   0.0290   1.0000
  15.000   1.4464   0.06536   0.05936  -0.0569   0.0267   1.0000
  15.250   1.4369   0.06939   0.06344  -0.0566   0.0244   1.0000
  15.500   1.4340   0.07271   0.06683  -0.0564   0.0235   1.0000
  15.750   1.4283   0.07643   0.07062  -0.0564   0.0225   1.0000
  16.000   1.4212   0.08036   0.07462  -0.0564   0.0216   1.0000
  16.250   1.4148   0.08422   0.07855  -0.0565   0.0211   1.0000
  16.500   1.4092   0.08801   0.08241  -0.0566   0.0204   1.0000
  16.750   1.4040   0.09182   0.08630  -0.0568   0.0199   1.0000
  17.000   1.3995   0.09557   0.09013  -0.0571   0.0195   1.0000
  17.250   1.3948   0.09934   0.09396  -0.0575   0.0191   1.0000
  17.500   1.3878   0.10345   0.09815  -0.0580   0.0186   1.0000
  17.750   1.3810   0.10760   0.10236  -0.0585   0.0182   1.0000
  18.000   1.3731   0.11192   0.10674  -0.0592   0.0178   1.0000
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