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GOE 601 AIRFOIL (goe601-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 601 AIRFOIL (goe601-il)
Reynolds number: 200,000
Max Cl/Cd: 69.85 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe601-il-200000.txt
Download as CSV file: xf-goe601-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 601 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.5895   0.09504   0.09091  -0.0707   1.0000   0.0543
 -14.250  -0.6383   0.08309   0.07890  -0.0770   1.0000   0.0533
 -14.000  -0.7040   0.07084   0.06644  -0.0840   1.0000   0.0522
 -13.750  -0.7542   0.06282   0.05820  -0.0874   1.0000   0.0516
 -13.500  -0.7955   0.05709   0.05225  -0.0882   1.0000   0.0511
 -13.250  -0.8310   0.05283   0.04778  -0.0871   1.0000   0.0508
 -13.000  -0.8582   0.04995   0.04474  -0.0844   1.0000   0.0509
 -12.750  -0.8838   0.04772   0.04236  -0.0806   1.0000   0.0509
 -12.500  -0.9092   0.04600   0.04051  -0.0755   1.0000   0.0510
 -12.250  -0.9375   0.04476   0.03916  -0.0690   1.0000   0.0510
 -12.000  -0.9670   0.04402   0.03834  -0.0614   1.0000   0.0510
 -11.750  -0.9884   0.04297   0.03717  -0.0553   1.0000   0.0512
 -11.500  -0.9752   0.04054   0.03443  -0.0558   0.9956   0.0520
 -11.250  -0.9563   0.03819   0.03174  -0.0568   0.9902   0.0530
 -11.000  -0.9357   0.03636   0.02952  -0.0577   0.9846   0.0542
 -10.750  -0.9076   0.03410   0.02712  -0.0595   0.9818   0.0555
 -10.500  -0.8838   0.03277   0.02576  -0.0599   0.9760   0.0566
 -10.250  -0.8539   0.03151   0.02440  -0.0615   0.9720   0.0581
 -10.000  -0.8213   0.03034   0.02307  -0.0634   0.9694   0.0600
  -9.750  -0.8032   0.02936   0.02191  -0.0624   0.9622   0.0614
  -9.500  -0.7731   0.02800   0.02044  -0.0637   0.9587   0.0630
  -9.250  -0.7388   0.02695   0.01944  -0.0657   0.9562   0.0650
  -9.000  -0.7199   0.02628   0.01873  -0.0646   0.9495   0.0670
  -8.750  -0.6924   0.02554   0.01788  -0.0651   0.9450   0.0696
  -8.500  -0.6603   0.02453   0.01685  -0.0666   0.9422   0.0724
  -8.250  -0.6249   0.02381   0.01615  -0.0687   0.9401   0.0761
  -8.000  -0.6155   0.02341   0.01568  -0.0655   0.9311   0.0789
  -7.750  -0.5856   0.02269   0.01498  -0.0664   0.9278   0.0838
  -7.500  -0.5502   0.02217   0.01437  -0.0682   0.9255   0.0915
  -7.250  -0.5402   0.02163   0.01392  -0.0652   0.9176   0.0982
  -7.000  -0.5158   0.02086   0.01317  -0.0651   0.9133   0.1118
  -6.750  -0.4856   0.02001   0.01234  -0.0661   0.9106   0.1289
  -6.500  -0.4512   0.01923   0.01159  -0.0678   0.9089   0.1446
  -6.250  -0.4482   0.01904   0.01141  -0.0633   0.8993   0.1523
  -6.000  -0.4173   0.01849   0.01090  -0.0642   0.8963   0.1655
  -5.750  -0.3824   0.01789   0.01038  -0.0659   0.8944   0.1821
  -5.500  -0.3462   0.01728   0.00990  -0.0679   0.8929   0.2088
  -5.250  -0.3453   0.01720   0.00994  -0.0628   0.8830   0.2319
  -5.000  -0.3149   0.01664   0.00959  -0.0636   0.8802   0.2858
  -4.750  -0.2817   0.01610   0.00923  -0.0648   0.8781   0.3339
  -4.500  -0.2475   0.01566   0.00893  -0.0661   0.8765   0.3773
  -4.250  -0.2449   0.01583   0.00919  -0.0613   0.8667   0.4009
  -4.000  -0.2126   0.01563   0.00904  -0.0620   0.8639   0.4347
  -3.750  -0.1771   0.01544   0.00884  -0.0633   0.8619   0.4612
  -3.500  -0.1399   0.01523   0.00859  -0.0650   0.8602   0.4835
  -3.250  -0.1344   0.01550   0.00888  -0.0607   0.8508   0.4982
  -3.000  -0.1023   0.01533   0.00869  -0.0613   0.8477   0.5179
  -2.750  -0.0672   0.01511   0.00848  -0.0625   0.8455   0.5374
  -2.500  -0.0299   0.01486   0.00825  -0.0642   0.8436   0.5563
  -2.250  -0.0219   0.01507   0.00852  -0.0603   0.8343   0.5692
  -2.000   0.0132   0.01479   0.00826  -0.0614   0.8306   0.5850
  -1.750   0.0540   0.01441   0.00788  -0.0635   0.8276   0.6023
  -1.500   0.0718   0.01446   0.00798  -0.0614   0.8198   0.6166
  -1.250   0.1021   0.01428   0.00781  -0.0615   0.8143   0.6321
  -1.000   0.1387   0.01404   0.00757  -0.0629   0.8108   0.6480
  -0.500   0.1861   0.01397   0.00758  -0.0608   0.7974   0.6801
  -0.250   0.2206   0.01376   0.00739  -0.0618   0.7932   0.6996
   0.000   0.2424   0.01375   0.00746  -0.0603   0.7862   0.7176
   0.250   0.2682   0.01363   0.00741  -0.0596   0.7793   0.7368
   0.500   0.3040   0.01339   0.00723  -0.0607   0.7747   0.7587
   0.750   0.3226   0.01339   0.00736  -0.0585   0.7663   0.7823
   1.000   0.3534   0.01320   0.00723  -0.0586   0.7596   0.8100
   1.250   0.3883   0.01309   0.00719  -0.0595   0.7536   0.8365
   1.500   0.4151   0.01311   0.00731  -0.0589   0.7455   0.8655
   1.750   0.4625   0.01305   0.00726  -0.0622   0.7400   0.8890
   2.000   0.5017   0.01316   0.00743  -0.0642   0.7316   0.9112
   2.250   0.5501   0.01316   0.00740  -0.0678   0.7241   0.9271
   2.500   0.5947   0.01323   0.00748  -0.0709   0.7153   0.9402
   2.750   0.6402   0.01318   0.00740  -0.0742   0.7062   0.9509
   3.000   0.6860   0.01318   0.00742  -0.0777   0.6946   0.9592
   3.250   0.7298   0.01312   0.00734  -0.0808   0.6834   0.9696
   3.500   0.7764   0.01303   0.00722  -0.0845   0.6701   0.9782
   3.750   0.8206   0.01295   0.00713  -0.0878   0.6526   0.9870
   4.000   0.8642   0.01287   0.00706  -0.0912   0.6307   0.9960
   4.250   0.8917   0.01281   0.00692  -0.0914   0.6068   1.0000
   4.500   0.8976   0.01285   0.00686  -0.0872   0.5811   1.0000
   4.750   0.9012   0.01299   0.00683  -0.0825   0.5484   1.0000
   5.000   0.9014   0.01325   0.00689  -0.0772   0.5104   1.0000
   5.250   0.8986   0.01364   0.00703  -0.0713   0.4719   1.0000
   5.500   0.8965   0.01408   0.00724  -0.0655   0.4397   1.0000
   5.750   0.8962   0.01454   0.00750  -0.0602   0.4144   1.0000
   6.000   0.8977   0.01496   0.00777  -0.0552   0.3958   1.0000
   6.250   0.9011   0.01538   0.00805  -0.0506   0.3806   1.0000
   6.500   0.9082   0.01583   0.00837  -0.0468   0.3684   1.0000
   6.750   0.9187   0.01623   0.00872  -0.0437   0.3570   1.0000
   7.000   0.9308   0.01666   0.00909  -0.0409   0.3467   1.0000
   7.250   0.9442   0.01713   0.00947  -0.0385   0.3373   1.0000
   7.500   0.9589   0.01753   0.00989  -0.0362   0.3288   1.0000
   7.750   0.9743   0.01800   0.01029  -0.0342   0.3206   1.0000
   8.000   0.9895   0.01842   0.01073  -0.0322   0.3128   1.0000
   8.250   1.0038   0.01886   0.01116  -0.0300   0.3047   1.0000
   8.500   1.0202   0.01931   0.01162  -0.0282   0.2977   1.0000
   8.750   1.0332   0.01972   0.01207  -0.0259   0.2901   1.0000
   9.000   1.0480   0.02022   0.01254  -0.0240   0.2825   1.0000
   9.250   1.0584   0.02062   0.01305  -0.0214   0.2742   1.0000
   9.500   1.0679   0.02115   0.01356  -0.0188   0.2647   1.0000
   9.750   1.0765   0.02164   0.01412  -0.0161   0.2545   1.0000
  10.000   1.0868   0.02218   0.01473  -0.0138   0.2446   1.0000
  10.250   1.0948   0.02285   0.01540  -0.0113   0.2332   1.0000
  10.500   1.1022   0.02357   0.01617  -0.0089   0.2170   1.0000
  10.750   1.1069   0.02454   0.01710  -0.0064   0.1903   1.0000
  11.000   1.1039   0.02618   0.01846  -0.0034   0.1402   1.0000
  11.250   1.0910   0.02873   0.02054   0.0002   0.0878   1.0000
  11.500   1.0888   0.03071   0.02241   0.0027   0.0741   1.0000
  11.750   1.0903   0.03248   0.02417   0.0047   0.0682   1.0000
  12.000   1.0926   0.03423   0.02597   0.0065   0.0648   1.0000
  12.250   1.0962   0.03592   0.02775   0.0081   0.0623   1.0000
  12.500   1.0974   0.03787   0.02975   0.0096   0.0602   1.0000
  12.750   1.0955   0.04014   0.03205   0.0111   0.0585   1.0000
  13.000   1.0957   0.04230   0.03427   0.0124   0.0571   1.0000
  13.250   1.0993   0.04425   0.03631   0.0135   0.0559   1.0000
  13.500   1.1022   0.04632   0.03845   0.0144   0.0546   1.0000
  13.750   1.1048   0.04845   0.04064   0.0152   0.0534   1.0000
  14.000   1.1074   0.05063   0.04285   0.0160   0.0524   1.0000
  14.250   1.1104   0.05277   0.04500   0.0168   0.0515   1.0000
  14.500   1.1156   0.05469   0.04688   0.0178   0.0505   1.0000
  14.750   1.1231   0.05648   0.04873   0.0185   0.0496   1.0000
  15.000   1.1312   0.05825   0.05059   0.0191   0.0488   1.0000
  15.250   1.1397   0.05999   0.05241   0.0197   0.0480   1.0000
  15.500   1.1479   0.06180   0.05427   0.0202   0.0469   1.0000
  15.750   1.1583   0.06338   0.05589   0.0208   0.0461   1.0000
  16.000   1.1699   0.06484   0.05737   0.0214   0.0453   1.0000
  16.250   1.1840   0.06608   0.05861   0.0222   0.0446   1.0000
  16.500   1.2088   0.06662   0.05909   0.0235   0.0433   1.0000
  16.750   1.2130   0.06894   0.06157   0.0237   0.0430   1.0000
  17.000   1.2146   0.07161   0.06442   0.0238   0.0425   1.0000
  17.250   1.2156   0.07438   0.06735   0.0238   0.0420   1.0000
  17.500   1.2171   0.07720   0.07034   0.0237   0.0415   1.0000
  17.750   1.2184   0.08012   0.07343   0.0236   0.0412   1.0000
  18.000   1.2166   0.08341   0.07688   0.0233   0.0407   1.0000
  18.250   1.2140   0.08688   0.08051   0.0227   0.0404   1.0000
  18.500   1.2105   0.09046   0.08424   0.0219   0.0400   1.0000
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