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GOE 288 AIRFOIL (goe288-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 288 AIRFOIL (goe288-il)
Reynolds number: 1,000,000
Max Cl/Cd: 113.86 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe288-il-1000000-n5.txt
Download as CSV file: xf-goe288-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 288 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
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.6944   0.13306   0.13061  -0.0403   1.0000   0.0232
 -18.500  -0.7142   0.12533   0.12279  -0.0448   1.0000   0.0234
 -18.250  -0.7289   0.11870   0.11609  -0.0486   1.0000   0.0235
 -18.000  -0.7399   0.11290   0.11023  -0.0520   1.0000   0.0237
 -17.750  -0.7533   0.10674   0.10400  -0.0556   1.0000   0.0238
 -17.500  -0.7668   0.10071   0.09789  -0.0591   1.0000   0.0239
 -17.250  -0.7780   0.09514   0.09225  -0.0624   1.0000   0.0240
 -17.000  -0.7886   0.08977   0.08682  -0.0656   1.0000   0.0241
 -16.750  -0.7995   0.08441   0.08138  -0.0688   1.0000   0.0241
 -16.500  -0.8102   0.07919   0.07609  -0.0720   1.0000   0.0242
 -16.250  -0.8202   0.07416   0.07099  -0.0751   1.0000   0.0243
 -16.000  -0.8291   0.06940   0.06616  -0.0780   1.0000   0.0244
 -15.750  -0.8384   0.06470   0.06140  -0.0809   1.0000   0.0244
 -15.500  -0.8490   0.06002   0.05665  -0.0839   1.0000   0.0245
 -15.250  -0.8618   0.05538   0.05193  -0.0868   1.0000   0.0245
 -15.000  -0.8756   0.05080   0.04728  -0.0896   1.0000   0.0246
 -14.750  -0.8825   0.04597   0.04237  -0.0942   0.9919   0.0247
 -14.500  -0.8864   0.04104   0.03733  -0.0997   0.9764   0.0247
 -14.250  -0.8928   0.03611   0.03228  -0.1048   0.9540   0.0248
 -14.000  -0.8952   0.03076   0.02675  -0.1118   0.9306   0.0249
 -13.750  -0.8790   0.02622   0.02199  -0.1194   0.9124   0.0250
 -13.500  -0.8601   0.02437   0.01997  -0.1216   0.8962   0.0251
 -13.250  -0.8399   0.02308   0.01855  -0.1227   0.8805   0.0252
 -13.000  -0.8183   0.02204   0.01737  -0.1233   0.8650   0.0254
 -12.750  -0.7956   0.02114   0.01635  -0.1238   0.8497   0.0255
 -12.500  -0.7720   0.02036   0.01545  -0.1242   0.8337   0.0257
 -12.250  -0.7477   0.01971   0.01467  -0.1245   0.8166   0.0258
 -12.000  -0.7229   0.01912   0.01396  -0.1247   0.7979   0.0260
 -11.750  -0.6978   0.01858   0.01329  -0.1248   0.7772   0.0261
 -11.500  -0.6725   0.01808   0.01264  -0.1249   0.7553   0.0262
 -11.250  -0.6467   0.01762   0.01204  -0.1250   0.7337   0.0263
 -11.000  -0.6215   0.01696   0.01125  -0.1253   0.7141   0.0265
 -10.750  -0.5955   0.01640   0.01058  -0.1255   0.6968   0.0268
 -10.500  -0.5688   0.01591   0.00999  -0.1257   0.6813   0.0270
 -10.250  -0.5416   0.01548   0.00948  -0.1259   0.6680   0.0272
 -10.000  -0.5141   0.01511   0.00901  -0.1261   0.6556   0.0275
  -9.750  -0.4862   0.01474   0.00858  -0.1263   0.6449   0.0277
  -9.500  -0.4582   0.01442   0.00818  -0.1265   0.6353   0.0279
  -9.250  -0.4298   0.01411   0.00780  -0.1268   0.6260   0.0282
  -9.000  -0.4014   0.01383   0.00744  -0.1270   0.6174   0.0285
  -8.750  -0.3727   0.01354   0.00709  -0.1272   0.6100   0.0287
  -8.500  -0.3440   0.01328   0.00677  -0.1274   0.6029   0.0290
  -8.250  -0.3151   0.01303   0.00646  -0.1277   0.5972   0.0293
  -8.000  -0.2859   0.01278   0.00616  -0.1279   0.5919   0.0296
  -7.750  -0.2568   0.01256   0.00589  -0.1282   0.5862   0.0299
  -7.250  -0.1982   0.01212   0.00535  -0.1287   0.5767   0.0304
  -7.000  -0.1689   0.01186   0.00506  -0.1290   0.5711   0.0310
  -6.750  -0.1396   0.01167   0.00482  -0.1292   0.5646   0.0317
  -6.500  -0.1102   0.01150   0.00461  -0.1295   0.5586   0.0323
  -6.250  -0.0806   0.01133   0.00441  -0.1297   0.5527   0.0329
  -6.000  -0.0511   0.01118   0.00422  -0.1300   0.5472   0.0335
  -5.500   0.0083   0.01091   0.00387  -0.1305   0.5392   0.0349
  -5.250   0.0381   0.01074   0.00369  -0.1308   0.5349   0.0361
  -5.000   0.0678   0.01062   0.00354  -0.1311   0.5299   0.0375
  -4.750   0.0974   0.01053   0.00341  -0.1313   0.5248   0.0391
  -4.500   0.1272   0.01038   0.00326  -0.1316   0.5207   0.0422
  -4.250   0.1570   0.01024   0.00312  -0.1319   0.5164   0.0471
  -4.000   0.1868   0.01007   0.00298  -0.1322   0.5117   0.0572
  -3.750   0.2163   0.00988   0.00284  -0.1326   0.5066   0.0771
  -3.500   0.2461   0.00973   0.00275  -0.1329   0.5026   0.0935
  -3.250   0.2760   0.00964   0.00268  -0.1332   0.4986   0.1032
  -3.000   0.3058   0.00958   0.00262  -0.1335   0.4944   0.1102
  -2.750   0.3355   0.00952   0.00257  -0.1337   0.4905   0.1179
  -2.500   0.3651   0.00949   0.00252  -0.1340   0.4865   0.1252
  -2.250   0.3950   0.00941   0.00248  -0.1343   0.4835   0.1361
  -1.750   0.4545   0.00926   0.00239  -0.1349   0.4747   0.1650
  -1.500   0.4838   0.00919   0.00236  -0.1351   0.4692   0.1876
  -1.250   0.5135   0.00907   0.00234  -0.1355   0.4646   0.2188
  -1.000   0.5431   0.00901   0.00234  -0.1358   0.4592   0.2443
  -0.750   0.5724   0.00901   0.00236  -0.1360   0.4533   0.2645
  -0.500   0.6018   0.00901   0.00238  -0.1362   0.4481   0.2806
  -0.250   0.6312   0.00904   0.00241  -0.1364   0.4413   0.2921
   0.000   0.6601   0.00911   0.00246  -0.1365   0.4336   0.3018
   0.250   0.6893   0.00916   0.00250  -0.1367   0.4248   0.3103
   0.500   0.7179   0.00927   0.00256  -0.1368   0.4135   0.3174
   0.750   0.7460   0.00942   0.00263  -0.1368   0.3985   0.3226
   1.000   0.7738   0.00959   0.00273  -0.1368   0.3815   0.3289
   1.250   0.8014   0.00978   0.00285  -0.1367   0.3662   0.3353
   1.500   0.8291   0.00996   0.00297  -0.1367   0.3533   0.3417
   1.750   0.8569   0.01011   0.00309  -0.1367   0.3435   0.3503
   2.000   0.8845   0.01029   0.00323  -0.1366   0.3344   0.3585
   2.250   0.9125   0.01041   0.00335  -0.1366   0.3282   0.3671
   2.500   0.9403   0.01055   0.00347  -0.1366   0.3221   0.3724
   2.750   0.9677   0.01073   0.00361  -0.1365   0.3159   0.3761
   3.000   0.9958   0.01084   0.00372  -0.1365   0.3119   0.3800
   3.250   1.0235   0.01097   0.00384  -0.1365   0.3076   0.3845
   3.500   1.0508   0.01112   0.00399  -0.1364   0.3034   0.3896
   3.750   1.0780   0.01129   0.00414  -0.1363   0.2994   0.3944
   4.000   1.1056   0.01141   0.00427  -0.1363   0.2970   0.3989
   4.250   1.1332   0.01151   0.00440  -0.1363   0.2947   0.4041
   4.500   1.1605   0.01164   0.00454  -0.1362   0.2922   0.4095
   4.750   1.1875   0.01179   0.00469  -0.1361   0.2896   0.4149
   5.000   1.2141   0.01194   0.00487  -0.1359   0.2869   0.4222
   5.250   1.2404   0.01212   0.00505  -0.1357   0.2839   0.4295
   5.750   1.2932   0.01241   0.00540  -0.1353   0.2794   0.4457
   6.000   1.3197   0.01254   0.00558  -0.1351   0.2776   0.4567
   6.250   1.3458   0.01268   0.00576  -0.1349   0.2757   0.4720
   6.500   1.3715   0.01283   0.00597  -0.1346   0.2737   0.4913
   6.750   1.3969   0.01298   0.00619  -0.1343   0.2716   0.5167
   7.000   1.4218   0.01314   0.00643  -0.1339   0.2695   0.5539
   7.250   1.4462   0.01328   0.00672  -0.1335   0.2669   0.6189
   7.500   1.4644   0.01289   0.00703  -0.1317   0.2643   1.0000
   7.750   1.4892   0.01308   0.00724  -0.1312   0.2630   1.0000
   8.000   1.5132   0.01329   0.00747  -0.1307   0.2614   1.0000
   8.250   1.5366   0.01351   0.00770  -0.1300   0.2595   1.0000
   8.500   1.5590   0.01376   0.00796  -0.1291   0.2571   1.0000
   8.750   1.5791   0.01404   0.00825  -0.1279   0.2546   1.0000
   9.000   1.5983   0.01437   0.00857  -0.1265   0.2520   1.0000
   9.250   1.6171   0.01473   0.00894  -0.1251   0.2496   1.0000
   9.500   1.6367   0.01507   0.00930  -0.1239   0.2480   1.0000
   9.750   1.6575   0.01537   0.00963  -0.1229   0.2468   1.0000
  10.000   1.6777   0.01570   0.00999  -0.1218   0.2443   1.0000
  10.250   1.6969   0.01608   0.01039  -0.1207   0.2413   1.0000
  10.500   1.7150   0.01653   0.01086  -0.1194   0.2385   1.0000
  10.750   1.7317   0.01707   0.01139  -0.1180   0.2353   1.0000
  11.000   1.7485   0.01762   0.01196  -0.1166   0.2325   1.0000
  11.250   1.7672   0.01808   0.01246  -0.1156   0.2307   1.0000
  11.500   1.7850   0.01860   0.01302  -0.1145   0.2278   1.0000
  11.750   1.8001   0.01929   0.01372  -0.1131   0.2232   1.0000
  12.000   1.8125   0.02017   0.01459  -0.1115   0.2182   1.0000
  12.250   1.8287   0.02085   0.01530  -0.1104   0.2149   1.0000
  12.500   1.8430   0.02167   0.01615  -0.1091   0.2108   1.0000
  12.750   1.8537   0.02275   0.01723  -0.1076   0.2057   1.0000
  13.000   1.8651   0.02382   0.01832  -0.1062   0.2002   1.0000
  13.250   1.8721   0.02526   0.01975  -0.1046   0.1920   1.0000
  13.500   1.8777   0.02686   0.02134  -0.1029   0.1832   1.0000
  13.750   1.8742   0.02926   0.02369  -0.1008   0.1692   1.0000
  14.000   1.8557   0.03308   0.02740  -0.0981   0.1471   1.0000
  14.250   1.8208   0.03870   0.03288  -0.0950   0.1186   1.0000
  14.500   1.7930   0.04404   0.03816  -0.0930   0.0993   1.0000
  14.750   1.7731   0.04883   0.04294  -0.0917   0.0874   1.0000
  15.000   1.7634   0.05265   0.04678  -0.0909   0.0811   1.0000
  15.250   1.7541   0.05648   0.05065  -0.0902   0.0765   1.0000
  15.500   1.7501   0.05982   0.05405  -0.0897   0.0735   1.0000
  15.750   1.7450   0.06333   0.05762  -0.0893   0.0707   1.0000
  16.000   1.7375   0.06712   0.06147  -0.0890   0.0681   1.0000
  16.250   1.7336   0.07054   0.06495  -0.0887   0.0659   1.0000
  16.500   1.7270   0.07437   0.06884  -0.0886   0.0632   1.0000
  16.750   1.7175   0.07860   0.07313  -0.0885   0.0605   1.0000
  17.000   1.7096   0.08264   0.07722  -0.0885   0.0578   1.0000
  17.250   1.7002   0.08695   0.08159  -0.0886   0.0545   1.0000
  17.500   1.6876   0.09175   0.08646  -0.0889   0.0516   1.0000
  17.750   1.6748   0.09665   0.09141  -0.0894   0.0478   1.0000
  18.000   1.6597   0.10190   0.09672  -0.0900   0.0442   1.0000
  18.250   1.6442   0.10730   0.10217  -0.0908   0.0406   1.0000
  18.500   1.6287   0.11281   0.10775  -0.0917   0.0369   1.0000
  18.750   1.6126   0.11845   0.11344  -0.0929   0.0335   1.0000
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