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GOE 777 AIRFOIL (goe777-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 777 AIRFOIL (goe777-il)
Reynolds number: 1,000,000
Max Cl/Cd: 109.02 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe777-il-1000000.txt
Download as CSV file: xf-goe777-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 777 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0143   0.08039   0.07688  -0.0642   1.0000   0.0261
 -19.500  -1.0290   0.07477   0.07118  -0.0675   1.0000   0.0263
 -19.250  -1.0417   0.06945   0.06577  -0.0706   1.0000   0.0265
 -19.000  -1.0528   0.06441   0.06064  -0.0735   1.0000   0.0266
 -18.750  -1.0610   0.05979   0.05594  -0.0762   1.0000   0.0268
 -18.500  -1.0673   0.05556   0.05163  -0.0786   1.0000   0.0269
 -18.250  -1.0715   0.05174   0.04774  -0.0806   1.0000   0.0271
 -18.000  -1.0735   0.04834   0.04426  -0.0823   1.0000   0.0273
 -17.750  -1.0740   0.04522   0.04107  -0.0838   1.0000   0.0276
 -17.500  -1.0726   0.04242   0.03820  -0.0849   1.0000   0.0278
 -17.250  -1.0730   0.04021   0.03565  -0.0849   0.8664   0.0280
 -17.000  -1.0701   0.03818   0.03325  -0.0850   0.7859   0.0283
 -16.750  -1.0640   0.03620   0.03103  -0.0855   0.7456   0.0285
 -16.500  -1.0562   0.03436   0.02901  -0.0859   0.7182   0.0287
 -16.250  -1.0469   0.03269   0.02718  -0.0862   0.6961   0.0289
 -16.000  -1.0360   0.03121   0.02555  -0.0863   0.6757   0.0291
 -15.750  -1.0294   0.02942   0.02363  -0.0863   0.6570   0.0294
 -15.500  -1.0254   0.02753   0.02162  -0.0860   0.6394   0.0297
 -15.250  -1.0166   0.02612   0.02011  -0.0856   0.6218   0.0301
 -14.750  -0.9915   0.02404   0.01784  -0.0842   0.5935   0.0307
 -14.500  -0.9771   0.02320   0.01690  -0.0833   0.5824   0.0310
 -14.250  -0.9619   0.02243   0.01606  -0.0824   0.5753   0.0314
 -14.000  -0.9457   0.02175   0.01530  -0.0813   0.5681   0.0318
 -13.750  -0.9285   0.02116   0.01463  -0.0802   0.5613   0.0322
 -13.500  -0.9099   0.02062   0.01403  -0.0791   0.5574   0.0326
 -13.250  -0.8904   0.02017   0.01351  -0.0780   0.5533   0.0329
 -13.000  -0.8802   0.01940   0.01268  -0.0757   0.5497   0.0335
 -12.750  -0.8657   0.01885   0.01209  -0.0738   0.5458   0.0340
 -12.500  -0.8461   0.01840   0.01159  -0.0726   0.5414   0.0345
 -12.250  -0.8249   0.01798   0.01114  -0.0716   0.5396   0.0350
 -12.000  -0.8028   0.01758   0.01071  -0.0707   0.5377   0.0355
 -11.750  -0.7800   0.01721   0.01030  -0.0698   0.5357   0.0361
 -11.500  -0.7563   0.01689   0.00993  -0.0690   0.5334   0.0366
 -11.250  -0.7336   0.01649   0.00949  -0.0681   0.5312   0.0373
 -11.000  -0.7116   0.01603   0.00901  -0.0672   0.5291   0.0382
 -10.750  -0.6877   0.01571   0.00866  -0.0664   0.5268   0.0390
 -10.500  -0.6630   0.01543   0.00834  -0.0658   0.5242   0.0398
 -10.250  -0.6380   0.01519   0.00805  -0.0652   0.5214   0.0406
 -10.000  -0.6128   0.01491   0.00774  -0.0646   0.5200   0.0414
  -9.750  -0.5884   0.01454   0.00737  -0.0639   0.5191   0.0427
  -9.500  -0.5626   0.01426   0.00710  -0.0634   0.5179   0.0440
  -9.250  -0.5361   0.01404   0.00685  -0.0629   0.5165   0.0454
  -9.000  -0.5104   0.01375   0.00657  -0.0624   0.5150   0.0472
  -8.750  -0.4839   0.01352   0.00634  -0.0620   0.5136   0.0491
  -8.500  -0.4571   0.01331   0.00612  -0.0616   0.5123   0.0513
  -8.250  -0.4302   0.01311   0.00594  -0.0613   0.5109   0.0541
  -8.000  -0.4029   0.01295   0.00577  -0.0610   0.5095   0.0570
  -7.750  -0.3751   0.01283   0.00566  -0.0607   0.5081   0.0603
  -7.500  -0.3474   0.01271   0.00554  -0.0605   0.5062   0.0633
  -7.250  -0.3193   0.01266   0.00547  -0.0604   0.5037   0.0662
  -7.000  -0.2916   0.01263   0.00540  -0.0601   0.5007   0.0687
  -6.750  -0.2635   0.01249   0.00529  -0.0600   0.4998   0.0711
  -6.500  -0.2347   0.01240   0.00519  -0.0599   0.4989   0.0734
  -6.250  -0.2063   0.01226   0.00505  -0.0598   0.4976   0.0753
  -6.000  -0.1785   0.01209   0.00489  -0.0597   0.4960   0.0777
  -5.750  -0.1499   0.01199   0.00480  -0.0596   0.4946   0.0798
  -5.500  -0.1211   0.01193   0.00471  -0.0596   0.4933   0.0815
  -5.250  -0.0934   0.01175   0.00453  -0.0594   0.4920   0.0837
  -5.000  -0.0653   0.01161   0.00440  -0.0593   0.4903   0.0857
  -4.750  -0.0369   0.01150   0.00428  -0.0592   0.4883   0.0877
  -4.500  -0.0083   0.01144   0.00418  -0.0592   0.4861   0.0894
  -4.250   0.0195   0.01135   0.00407  -0.0590   0.4839   0.0918
  -4.000   0.0474   0.01130   0.00402  -0.0589   0.4816   0.0943
  -3.750   0.0760   0.01121   0.00393  -0.0589   0.4806   0.0966
  -3.500   0.1051   0.01113   0.00385  -0.0590   0.4798   0.0988
  -3.250   0.1334   0.01097   0.00373  -0.0589   0.4788   0.1037
  -3.000   0.1621   0.01086   0.00364  -0.0590   0.4776   0.1081
  -2.750   0.1905   0.01072   0.00354  -0.0590   0.4761   0.1151
  -2.500   0.2187   0.01055   0.00344  -0.0589   0.4744   0.1295
  -2.250   0.2430   0.01002   0.00326  -0.0584   0.4728   0.2199
  -2.000   0.2688   0.00964   0.00317  -0.0581   0.4712   0.2988
  -1.750   0.2963   0.00944   0.00311  -0.0580   0.4696   0.3439
  -1.500   0.3239   0.00928   0.00307  -0.0580   0.4678   0.3850
  -1.250   0.3509   0.00910   0.00304  -0.0578   0.4656   0.4334
  -1.000   0.3764   0.00889   0.00308  -0.0574   0.4630   0.5170
  -0.750   0.4042   0.00876   0.00311  -0.0574   0.4617   0.5703
  -0.500   0.4333   0.00871   0.00312  -0.0575   0.4604   0.5962
  -0.250   0.4625   0.00866   0.00314  -0.0576   0.4587   0.6137
   0.000   0.4918   0.00864   0.00314  -0.0578   0.4566   0.6274
   0.250   0.5212   0.00862   0.00314  -0.0581   0.4543   0.6400
   0.500   0.5504   0.00861   0.00314  -0.0582   0.4517   0.6508
   0.750   0.5793   0.00863   0.00315  -0.0584   0.4489   0.6622
   1.000   0.6078   0.00869   0.00320  -0.0585   0.4454   0.6728
   1.250   0.6371   0.00868   0.00323  -0.0588   0.4433   0.6828
   1.500   0.6668   0.00868   0.00325  -0.0591   0.4408   0.6915
   1.750   0.6958   0.00865   0.00327  -0.0593   0.4376   0.7026
   2.250   0.7525   0.00869   0.00333  -0.0595   0.4296   0.7289
   2.500   0.7810   0.00870   0.00338  -0.0597   0.4257   0.7439
   2.750   0.8093   0.00868   0.00343  -0.0598   0.4208   0.7639
   3.000   0.8366   0.00870   0.00349  -0.0597   0.4146   0.7866
   3.250   0.8636   0.00873   0.00358  -0.0596   0.4081   0.8099
   3.500   0.8899   0.00878   0.00367  -0.0594   0.3993   0.8372
   3.750   0.9153   0.00886   0.00380  -0.0590   0.3899   0.8678
   4.000   0.9389   0.00901   0.00397  -0.0582   0.3789   0.9017
   4.250   0.9659   0.00918   0.00418  -0.0581   0.3688   0.9370
   4.500   0.9989   0.00947   0.00443  -0.0594   0.3593   0.9614
   4.750   1.0334   0.00978   0.00469  -0.0612   0.3511   0.9753
   5.000   1.0685   0.01006   0.00493  -0.0631   0.3448   0.9841
   5.250   1.1038   0.01032   0.00515  -0.0650   0.3400   0.9907
   5.500   1.1406   0.01063   0.00541  -0.0673   0.3351   0.9943
   5.750   1.1775   0.01093   0.00568  -0.0697   0.3307   0.9977
   6.000   1.2134   0.01113   0.00588  -0.0718   0.3282   1.0000
   6.250   1.2303   0.01131   0.00605  -0.0700   0.3258   1.0000
   6.500   1.2468   0.01152   0.00625  -0.0681   0.3234   1.0000
   6.750   1.2627   0.01176   0.00648  -0.0662   0.3210   1.0000
   7.000   1.2770   0.01204   0.00675  -0.0640   0.3183   1.0000
   7.250   1.2898   0.01238   0.00707  -0.0615   0.3155   1.0000
   7.500   1.3074   0.01257   0.00728  -0.0599   0.3145   1.0000
   7.750   1.3253   0.01278   0.00752  -0.0585   0.3132   1.0000
   8.000   1.3439   0.01304   0.00779  -0.0573   0.3119   1.0000
   8.250   1.3628   0.01333   0.00810  -0.0562   0.3103   1.0000
   8.500   1.3812   0.01368   0.00847  -0.0551   0.3086   1.0000
   8.750   1.3989   0.01409   0.00888  -0.0541   0.3069   1.0000
   9.000   1.4156   0.01457   0.00938  -0.0530   0.3051   1.0000
   9.250   1.4312   0.01515   0.00996  -0.0519   0.3033   1.0000
   9.500   1.4450   0.01585   0.01066  -0.0506   0.3009   1.0000
   9.750   1.4620   0.01645   0.01129  -0.0499   0.2994   1.0000
  10.000   1.4818   0.01693   0.01181  -0.0496   0.2983   1.0000
  10.250   1.5006   0.01749   0.01242  -0.0492   0.2971   1.0000
  10.500   1.5187   0.01812   0.01309  -0.0489   0.2957   1.0000
  10.750   1.5358   0.01884   0.01384  -0.0485   0.2944   1.0000
  11.000   1.5520   0.01964   0.01468  -0.0481   0.2928   1.0000
  11.250   1.5667   0.02058   0.01564  -0.0477   0.2911   1.0000
  11.500   1.5792   0.02171   0.01680  -0.0473   0.2892   1.0000
  11.750   1.5889   0.02305   0.01814  -0.0466   0.2868   1.0000
  12.000   1.5986   0.02437   0.01947  -0.0460   0.2842   1.0000
  12.250   1.6140   0.02541   0.02058  -0.0460   0.2832   1.0000
  12.500   1.6285   0.02651   0.02174  -0.0459   0.2818   1.0000
  12.750   1.6414   0.02771   0.02300  -0.0458   0.2804   1.0000
  13.000   1.6529   0.02904   0.02437  -0.0455   0.2788   1.0000
  13.250   1.6636   0.03041   0.02578  -0.0453   0.2771   1.0000
  13.500   1.6714   0.03204   0.02746  -0.0450   0.2754   1.0000
  13.750   1.6772   0.03381   0.02925  -0.0445   0.2735   1.0000
  14.000   1.6824   0.03557   0.03103  -0.0440   0.2715   1.0000
  14.250   1.6898   0.03711   0.03258  -0.0435   0.2692   1.0000
  14.500   1.6988   0.03877   0.03432  -0.0434   0.2681   1.0000
  14.750   1.7064   0.04057   0.03619  -0.0434   0.2665   1.0000
  15.000   1.7140   0.04233   0.03802  -0.0433   0.2645   1.0000
  15.250   1.7194   0.04433   0.04007  -0.0432   0.2623   1.0000
  15.500   1.7239   0.04639   0.04216  -0.0431   0.2600   1.0000
  15.750   1.7231   0.04894   0.04472  -0.0428   0.2570   1.0000
  16.000   1.7280   0.05088   0.04668  -0.0426   0.2543   1.0000
  16.250   1.7329   0.05302   0.04891  -0.0426   0.2524   1.0000
  16.500   1.7387   0.05503   0.05099  -0.0427   0.2500   1.0000
  16.750   1.7432   0.05715   0.05315  -0.0427   0.2472   1.0000
  17.000   1.7403   0.06001   0.05603  -0.0426   0.2440   1.0000
  17.250   1.7401   0.06253   0.05856  -0.0424   0.2406   1.0000
  17.500   1.7444   0.06475   0.06087  -0.0426   0.2381   1.0000
  17.750   1.7466   0.06716   0.06333  -0.0427   0.2344   1.0000
  18.000   1.7449   0.06996   0.06613  -0.0427   0.2301   1.0000
  18.250   1.7388   0.07323   0.06945  -0.0427   0.2262   1.0000
  18.500   1.7419   0.07554   0.07182  -0.0429   0.2217   1.0000
  18.750   1.7315   0.07935   0.07564  -0.0430   0.2159   1.0000
  19.000   1.7271   0.08253   0.07884  -0.0432   0.2099   1.0000
  19.250   1.7103   0.08710   0.08342  -0.0433   0.2022   1.0000
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