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GOE 244 (MVA PR.4) AIRFOIL (goe244-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 244 (MVA PR.4) AIRFOIL (goe244-il)
Reynolds number: 200,000
Max Cl/Cd: 64.27 at α=0.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe244-il-200000-n5.txt
Download as CSV file: xf-goe244-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 244 (MVA PR.4) 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.750   0.2824   0.09891   0.09445  -0.1284   0.8290   0.0457
  -9.500   0.2920   0.09676   0.09231  -0.1294   0.8216   0.0472
  -9.250   0.2875   0.09400   0.08952  -0.1332   0.8151   0.0487
  -9.000   0.3033   0.09154   0.08702  -0.1329   0.8089   0.0490
  -8.750   0.3168   0.08950   0.08498  -0.1329   0.8010   0.0495
  -8.500   0.3289   0.08743   0.08288  -0.1334   0.7947   0.0502
  -8.250   0.3398   0.08533   0.08076  -0.1343   0.7886   0.0512
  -8.000   0.3485   0.08313   0.07856  -0.1356   0.7816   0.0525
  -7.750   0.3443   0.07991   0.07530  -0.1401   0.7753   0.0539
  -7.500   0.3569   0.07767   0.07305  -0.1403   0.7689   0.0541
  -7.250   0.3712   0.07588   0.07126  -0.1400   0.7614   0.0545
  -7.000   0.3844   0.07396   0.06929  -0.1403   0.7551   0.0551
  -6.750   0.3951   0.07204   0.06738  -0.1409   0.7481   0.0559
  -6.250   0.3905   0.06257   0.05783  -0.1481   0.7348   0.0441
  -5.750   0.4717   0.02845   0.02253  -0.2169   0.7215   0.0349
  -5.500   0.5263   0.02527   0.01878  -0.2272   0.7161   0.0350
  -5.250   0.5679   0.02350   0.01664  -0.2324   0.7095   0.0353
  -5.000   0.6010   0.02252   0.01557  -0.2344   0.7025   0.0358
  -4.750   0.6356   0.02170   0.01459  -0.2364   0.6962   0.0364
  -4.500   0.6680   0.02092   0.01367  -0.2381   0.6887   0.0369
  -4.250   0.7016   0.02015   0.01271  -0.2397   0.6816   0.0371
  -4.000   0.7347   0.01950   0.01190  -0.2410   0.6751   0.0373
  -3.750   0.7652   0.01899   0.01129  -0.2418   0.6673   0.0376
  -3.500   0.7966   0.01855   0.01071  -0.2426   0.6595   0.0380
  -3.250   0.8263   0.01820   0.01029  -0.2431   0.6510   0.0383
  -3.000   0.8562   0.01791   0.00990  -0.2436   0.6418   0.0388
  -2.750   0.8856   0.01768   0.00960  -0.2440   0.6326   0.0392
  -2.500   0.9150   0.01747   0.00933  -0.2445   0.6227   0.0397
  -2.250   0.9445   0.01731   0.00914  -0.2450   0.6129   0.0404
  -2.000   0.9733   0.01721   0.00897  -0.2453   0.6020   0.0414
  -1.750   1.0013   0.01716   0.00885  -0.2455   0.5905   0.0430
  -1.500   1.0287   0.01715   0.00873  -0.2456   0.5782   0.0445
  -1.250   1.0549   0.01718   0.00866  -0.2454   0.5637   0.0460
  -1.000   1.0797   0.01727   0.00864  -0.2449   0.5477   0.0476
  -0.750   1.1030   0.01742   0.00867  -0.2442   0.5300   0.0497
  -0.500   1.1245   0.01764   0.00877  -0.2431   0.5112   0.0534
  -0.250   1.1445   0.01792   0.00895  -0.2418   0.4931   0.0624
   0.000   1.1629   0.01824   0.00915  -0.2402   0.4773   0.0788
   0.250   1.1823   0.01845   0.00936  -0.2391   0.4640   0.1165
   0.500   1.2018   0.01870   0.00979  -0.2381   0.4524   0.2265
   0.750   1.2208   0.01913   0.01016  -0.2367   0.4430   0.2486
   1.000   1.2401   0.01959   0.01055  -0.2354   0.4344   0.2659
   1.250   1.2594   0.02007   0.01098  -0.2341   0.4273   0.2823
   1.500   1.2805   0.02048   0.01139  -0.2332   0.4207   0.3037
   1.750   1.3004   0.02095   0.01185  -0.2320   0.4146   0.3245
   2.000   1.3194   0.02148   0.01236  -0.2308   0.4094   0.3475
   2.250   1.3409   0.02189   0.01282  -0.2299   0.4045   0.3739
   2.500   1.3610   0.02237   0.01332  -0.2288   0.3995   0.3976
   2.750   1.3802   0.02291   0.01384  -0.2276   0.3949   0.4177
   3.000   1.3988   0.02351   0.01437  -0.2263   0.3908   0.4355
   3.250   1.4190   0.02401   0.01488  -0.2252   0.3873   0.4524
   3.500   1.4395   0.02449   0.01538  -0.2242   0.3838   0.4678
   3.750   1.4595   0.02501   0.01590  -0.2232   0.3804   0.4816
   4.000   1.4790   0.02557   0.01643  -0.2221   0.3772   0.4932
   4.250   1.4981   0.02615   0.01698  -0.2209   0.3742   0.5025
   4.500   1.5173   0.02675   0.01753  -0.2198   0.3715   0.5119
   4.750   1.5374   0.02731   0.01806  -0.2189   0.3690   0.5202
   5.000   1.5575   0.02783   0.01863  -0.2180   0.3666   0.5283
   5.250   1.5772   0.02839   0.01922  -0.2170   0.3642   0.5368
   5.500   1.5964   0.02896   0.01984  -0.2160   0.3617   0.5445
   5.750   1.6153   0.02957   0.02045  -0.2150   0.3594   0.5533
   6.000   1.6341   0.03019   0.02109  -0.2140   0.3571   0.5612
   6.250   1.6525   0.03083   0.02173  -0.2129   0.3548   0.5703
   6.500   1.6711   0.03148   0.02236  -0.2119   0.3525   0.5793
   6.750   1.6902   0.03211   0.02297  -0.2109   0.3500   0.5897
   7.000   1.7060   0.03286   0.02382  -0.2097   0.3475   0.6005
   7.250   1.7216   0.03362   0.02466  -0.2084   0.3447   0.6128
   7.500   1.7365   0.03443   0.02555  -0.2070   0.3417   0.6239
   7.750   1.7510   0.03527   0.02643  -0.2057   0.3387   0.6341
   8.000   1.7659   0.03609   0.02728  -0.2044   0.3359   0.6429
   8.500   1.7985   0.03764   0.02879  -0.2021   0.3309   0.6659
   8.750   1.8124   0.03856   0.02985  -0.2009   0.3290   0.6793
   9.000   1.8264   0.03948   0.03089  -0.1996   0.3268   0.6969
   9.250   1.8398   0.04043   0.03197  -0.1983   0.3245   0.7236
   9.500   1.8527   0.04130   0.03303  -0.1970   0.3223   0.7909
   9.750   1.8609   0.04226   0.03409  -0.1950   0.3198   1.0000
  10.000   1.8727   0.04342   0.03525  -0.1938   0.3171   1.0000
  10.250   1.8857   0.04449   0.03630  -0.1926   0.3147   1.0000
  10.500   1.9012   0.04539   0.03716  -0.1916   0.3126   1.0000
  10.750   1.9121   0.04669   0.03857  -0.1904   0.3107   1.0000
  11.000   1.9214   0.04813   0.04012  -0.1891   0.3084   1.0000
  11.250   1.9299   0.04965   0.04173  -0.1877   0.3056   1.0000
  11.500   1.9372   0.05128   0.04344  -0.1864   0.3026   1.0000
  11.750   1.9456   0.05282   0.04503  -0.1852   0.2997   1.0000
  12.000   1.9547   0.05429   0.04652  -0.1840   0.2970   1.0000
  12.250   1.9661   0.05556   0.04776  -0.1829   0.2946   1.0000
  12.500   1.9715   0.05752   0.04987  -0.1817   0.2922   1.0000
  12.750   1.9760   0.05958   0.05208  -0.1805   0.2894   1.0000
  13.000   1.9807   0.06164   0.05425  -0.1793   0.2865   1.0000
  13.250   1.9847   0.06378   0.05648  -0.1782   0.2833   1.0000
  13.500   1.9894   0.06583   0.05855  -0.1772   0.2799   1.0000
  13.750   1.9928   0.06807   0.06084  -0.1761   0.2765   1.0000
  14.000   1.9900   0.07118   0.06414  -0.1751   0.2720   1.0000
  14.250   1.9879   0.07420   0.06726  -0.1741   0.2671   1.0000
  14.500   1.9869   0.07705   0.07013  -0.1733   0.2625   1.0000
  14.750   1.9819   0.08057   0.07380  -0.1725   0.2574   1.0000
  15.000   1.9754   0.08432   0.07768  -0.1718   0.2515   1.0000
  15.250   1.9695   0.08798   0.08137  -0.1712   0.2458   1.0000
  15.500   1.9581   0.09255   0.08611  -0.1707   0.2385   1.0000
  15.750   1.9458   0.09721   0.09082  -0.1704   0.2310   1.0000
  16.000   1.9300   0.10248   0.09621  -0.1703   0.2218   1.0000
  16.250   1.9121   0.10809   0.10189  -0.1704   0.2120   1.0000
  16.500   1.8908   0.11431   0.10813  -0.1709   0.2017   1.0000
  16.750   1.8673   0.12095   0.11480  -0.1717   0.1919   1.0000
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