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GOE 652 AIRFOIL (goe652-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 652 AIRFOIL (goe652-il)
Reynolds number: 500,000
Max Cl/Cd: 112.71 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe652-il-500000.txt
Download as CSV file: xf-goe652-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 652 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000   0.3256   0.09228   0.08877  -0.1590   0.8604   0.0669
  -9.750  -0.0193   0.04175   0.03753  -0.1864   0.8335   0.0654
  -9.500  -0.0241   0.03957   0.03527  -0.1869   0.8259   0.0658
  -9.250  -0.0208   0.03759   0.03326  -0.1881   0.8196   0.0663
  -9.000  -0.0142   0.03563   0.03128  -0.1898   0.8132   0.0669
  -8.750  -0.0039   0.03327   0.02883  -0.1931   0.8070   0.0675
  -8.500   0.0138   0.03088   0.02631  -0.1980   0.8009   0.0682
  -8.250   0.0339   0.02844   0.02381  -0.2031   0.7956   0.0690
  -8.000   0.0633   0.02586   0.02110  -0.2101   0.7903   0.0700
  -7.750   0.1013   0.02336   0.01841  -0.2183   0.7856   0.0709
  -7.500   0.1331   0.02273   0.01778  -0.2203   0.7811   0.0722
  -7.250   0.1694   0.02154   0.01657  -0.2247   0.7769   0.0736
  -7.000   0.2089   0.02008   0.01505  -0.2301   0.7726   0.0752
  -6.750   0.2525   0.01845   0.01329  -0.2365   0.7679   0.0768
  -6.500   0.2919   0.01742   0.01220  -0.2406   0.7629   0.0786
  -6.250   0.3334   0.01639   0.01108  -0.2452   0.7574   0.0806
  -6.000   0.3743   0.01524   0.00985  -0.2496   0.7524   0.0830
  -5.750   0.4137   0.01430   0.00885  -0.2533   0.7469   0.0856
  -5.500   0.4500   0.01370   0.00818  -0.2557   0.7414   0.0885
  -5.250   0.4857   0.01327   0.00761  -0.2576   0.7361   0.0919
  -5.000   0.5200   0.01285   0.00720  -0.2593   0.7315   0.0958
  -4.750   0.5532   0.01251   0.00680  -0.2605   0.7265   0.1000
  -4.500   0.5862   0.01220   0.00649  -0.2617   0.7212   0.1044
  -4.250   0.6188   0.01198   0.00616  -0.2626   0.7155   0.1092
  -4.000   0.6503   0.01179   0.00596  -0.2632   0.7096   0.1141
  -3.750   0.6816   0.01159   0.00575  -0.2638   0.7035   0.1191
  -3.500   0.7123   0.01148   0.00559  -0.2641   0.6976   0.1243
  -3.250   0.7434   0.01141   0.00544  -0.2646   0.6919   0.1294
  -3.000   0.7734   0.01132   0.00537  -0.2648   0.6864   0.1344
  -2.750   0.8037   0.01122   0.00524  -0.2650   0.6800   0.1393
  -2.500   0.8334   0.01121   0.00518  -0.2650   0.6738   0.1442
  -2.250   0.8632   0.01120   0.00511  -0.2651   0.6678   0.1491
  -2.000   0.8926   0.01115   0.00511  -0.2651   0.6612   0.1541
  -1.750   0.9217   0.01119   0.00507  -0.2650   0.6544   0.1591
  -1.500   0.9510   0.01120   0.00504  -0.2650   0.6480   0.1640
  -1.250   0.9798   0.01122   0.00509  -0.2649   0.6417   0.1690
  -1.000   1.0084   0.01130   0.00509  -0.2646   0.6349   0.1736
  -0.500   1.0654   0.01140   0.00520  -0.2642   0.6219   0.1842
  -0.250   1.0936   0.01150   0.00522  -0.2639   0.6150   0.1882
   0.000   1.1220   0.01152   0.00523  -0.2638   0.6085   0.1934
   0.250   1.1502   0.01159   0.00532  -0.2635   0.6024   0.1979
   0.500   1.1781   0.01168   0.00537  -0.2632   0.5956   0.2023
   0.750   1.2060   0.01174   0.00537  -0.2629   0.5888   0.2067
   1.000   1.2338   0.01181   0.00547  -0.2626   0.5825   0.2112
   1.250   1.2612   0.01191   0.00557  -0.2622   0.5755   0.2155
   1.500   1.2877   0.01207   0.00565  -0.2616   0.5681   0.2195
   1.750   1.3152   0.01212   0.00569  -0.2612   0.5604   0.2240
   2.000   1.3415   0.01222   0.00580  -0.2607   0.5516   0.2284
   2.250   1.3670   0.01241   0.00594  -0.2599   0.5431   0.2327
   2.500   1.3933   0.01253   0.00606  -0.2593   0.5347   0.2370
   2.750   1.4181   0.01274   0.00618  -0.2585   0.5260   0.2405
   3.000   1.4444   0.01282   0.00630  -0.2579   0.5174   0.2460
   3.250   1.4682   0.01304   0.00649  -0.2569   0.5069   0.2503
   3.500   1.4923   0.01324   0.00667  -0.2559   0.4959   0.2550
   3.750   1.5137   0.01356   0.00688  -0.2545   0.4829   0.2586
   4.000   1.5366   0.01375   0.00706  -0.2534   0.4681   0.2638
   4.250   1.5569   0.01407   0.00734  -0.2518   0.4521   0.2686
   4.500   1.5752   0.01447   0.00766  -0.2498   0.4350   0.2731
   4.750   1.5903   0.01491   0.00801  -0.2473   0.4182   0.2773
   5.000   1.6026   0.01543   0.00841  -0.2443   0.4029   0.2808
   5.250   1.6184   0.01585   0.00882  -0.2421   0.3905   0.2868
   5.500   1.6329   0.01638   0.00930  -0.2396   0.3808   0.2917
   5.750   1.6490   0.01687   0.00976  -0.2375   0.3730   0.2968
   6.000   1.6628   0.01748   0.01031  -0.2350   0.3661   0.3013
   6.250   1.6809   0.01791   0.01079  -0.2333   0.3609   0.3079
   6.500   1.6978   0.01843   0.01131  -0.2314   0.3555   0.3139
   6.750   1.7121   0.01908   0.01194  -0.2291   0.3501   0.3197
   7.000   1.7256   0.01982   0.01263  -0.2268   0.3450   0.3245
   7.250   1.7450   0.02024   0.01314  -0.2255   0.3420   0.3317
   7.500   1.7624   0.02079   0.01373  -0.2238   0.3385   0.3385
   7.750   1.7785   0.02144   0.01439  -0.2220   0.3349   0.3447
   8.000   1.7937   0.02215   0.01512  -0.2202   0.3315   0.3513
   8.250   1.8077   0.02298   0.01595  -0.2182   0.3279   0.3575
   8.500   1.8237   0.02372   0.01671  -0.2165   0.3249   0.3641
   8.750   1.8416   0.02431   0.01737  -0.2151   0.3223   0.3709
   9.000   1.8583   0.02497   0.01811  -0.2136   0.3192   0.3781
   9.250   1.8731   0.02579   0.01895  -0.2119   0.3156   0.3851
   9.500   1.8868   0.02671   0.01987  -0.2102   0.3120   0.3914
   9.750   1.8990   0.02778   0.02096  -0.2083   0.3079   0.3979
  10.000   1.9145   0.02861   0.02185  -0.2069   0.3049   0.4052
  10.250   1.9304   0.02940   0.02272  -0.2055   0.3018   0.4127
  10.500   1.9447   0.03033   0.02373  -0.2040   0.2982   0.4205
  10.750   1.9575   0.03141   0.02482  -0.2024   0.2944   0.4281
  11.000   1.9679   0.03271   0.02614  -0.2006   0.2902   0.4353
  11.250   1.9806   0.03386   0.02735  -0.1991   0.2865   0.4440
  11.500   1.9954   0.03483   0.02841  -0.1979   0.2829   0.4534
  11.750   2.0077   0.03604   0.02971  -0.1965   0.2785   0.4633
  12.000   2.0175   0.03750   0.03119  -0.1949   0.2738   0.4734
  12.250   2.0258   0.03915   0.03288  -0.1933   0.2690   0.4851
  12.500   2.0399   0.04032   0.03417  -0.1923   0.2642   0.4999
  12.750   2.0502   0.04186   0.03578  -0.1910   0.2584   0.5172
  13.000   2.0547   0.04402   0.03797  -0.1894   0.2523   0.5391
  13.250   2.0680   0.04541   0.03951  -0.1885   0.2455   0.5853
  13.500   2.0699   0.04740   0.04181  -0.1868   0.2378   1.0000
  13.750   2.0771   0.04941   0.04383  -0.1855   0.2295   1.0000
  14.000   2.0766   0.05232   0.04671  -0.1840   0.2206   1.0000
  14.250   2.0810   0.05473   0.04912  -0.1828   0.2119   1.0000
  14.500   2.0790   0.05797   0.05233  -0.1815   0.2040   1.0000
  14.750   2.0808   0.06081   0.05518  -0.1804   0.1973   1.0000
  15.000   2.0778   0.06431   0.05865  -0.1793   0.1911   1.0000
  15.250   2.0802   0.06718   0.06156  -0.1784   0.1866   1.0000
  15.500   2.0809   0.07033   0.06473  -0.1776   0.1822   1.0000
  15.750   2.0773   0.07410   0.06850  -0.1768   0.1779   1.0000
  16.000   2.0805   0.07699   0.07144  -0.1761   0.1744   1.0000
  16.250   2.0826   0.08008   0.07460  -0.1756   0.1711   1.0000
  16.500   2.0824   0.08350   0.07804  -0.1751   0.1677   1.0000
  16.750   2.0783   0.08753   0.08208  -0.1748   0.1641   1.0000
  17.000   2.0813   0.09056   0.08518  -0.1744   0.1612   1.0000
  17.250   2.0843   0.09361   0.08832  -0.1742   0.1583   1.0000
  17.500   2.0843   0.09712   0.09188  -0.1741   0.1552   1.0000
  17.750   2.0810   0.10112   0.09590  -0.1741   0.1520   1.0000
  18.000   2.0802   0.10476   0.09958  -0.1742   0.1489   1.0000
  18.250   2.0842   0.10772   0.10264  -0.1743   0.1461   1.0000
  18.500   2.0832   0.11142   0.10642  -0.1746   0.1428   1.0000
  18.750   2.0799   0.11545   0.11046  -0.1751   0.1394   1.0000
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