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UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT (ua79sfm-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT (ua79sfm-il)
Reynolds number: 200,000
Max Cl/Cd: 80.03 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ua79sfm-il-200000-n5.txt
Download as CSV file: xf-ua79sfm-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.2105   0.09407   0.09079  -0.0715  -0.0011   4.4574
 -12.000  -0.2018   0.09140   0.08813  -0.0717  -0.0012   4.4573
 -11.750  -0.2058   0.08614   0.08289  -0.0747  -0.0014   4.4571
 -11.500  -0.1968   0.08281   0.07955  -0.0757  -0.0015   4.4569
 -11.250  -0.1933   0.07843   0.07518  -0.0781  -0.0015   4.4569
 -11.000  -0.2195   0.06348   0.06024  -0.0856  -0.0016   4.4481
 -10.750  -0.2421   0.06133   0.05813  -0.0845  -0.0016   4.4480
 -10.500  -0.2604   0.05694   0.05369  -0.0875  -0.0014   4.4478
 -10.250  -0.2806   0.05308   0.04974  -0.0904  -0.0012   4.4476
 -10.000  -0.2992   0.04989   0.04644  -0.0926  -0.0010   4.4473
  -9.750  -0.3243   0.04803   0.04450  -0.0921  -0.0007   4.4472
  -9.500  -0.3482   0.04657   0.04296  -0.0900  -0.0002   4.4471
  -9.250  -0.3577   0.04361   0.03982  -0.0898  -0.0001   4.4466
  -9.000  -0.3722   0.03756   0.03321  -0.0893   0.0000   4.4435
  -8.750  -0.3827   0.03630   0.03183  -0.0858  -0.0001   4.4430
  -8.500  -0.3798   0.03443   0.02981  -0.0843  -0.0003   4.4426
  -8.250  -0.3707   0.03217   0.02732  -0.0835  -0.0004   4.4421
  -8.000  -0.3581   0.02989   0.02475  -0.0828  -0.0004   4.4413
  -7.750  -0.3430   0.02774   0.02229  -0.0821  -0.0004   4.4405
  -7.500  -0.3504   0.02697   0.02139  -0.0779  -0.0002   4.4400
  -7.250  -0.3361   0.02532   0.01946  -0.0766   0.0001   4.4393
  -7.000  -0.3171   0.02378   0.01763  -0.0756   0.0004   4.4385
  -6.750  -0.2949   0.02252   0.01610  -0.0751   0.0007   4.4379
  -6.500  -0.2893   0.02190   0.01539  -0.0724   0.0026   4.4376
  -6.250  -0.2745   0.02118   0.01457  -0.0709   0.0039   4.4375
  -6.000  -0.2555   0.02045   0.01375  -0.0701   0.0048   4.4374
  -5.750  -0.2349   0.01975   0.01298  -0.0694   0.0056   4.4374
  -5.500  -0.2136   0.01912   0.01228  -0.0690   0.0063   4.4376
  -5.250  -0.2147   0.01889   0.01205  -0.0656   0.0108   4.4377
  -5.000  -0.1985   0.01840   0.01152  -0.0645   0.0128   4.4379
  -4.750  -0.1791   0.01793   0.01099  -0.0638   0.0142   4.4383
  -4.500  -0.1580   0.01752   0.01050  -0.0633   0.0152   4.4389
  -4.250  -0.1543   0.01735   0.01032  -0.0605   0.0202   4.4393
  -4.000  -0.1393   0.01708   0.00998  -0.0592   0.0232   4.4400
  -3.750  -0.1191   0.01680   0.00962  -0.0585   0.0249   4.4410
  -3.500  -0.0973   0.01654   0.00929  -0.0580   0.0262   4.4425
  -3.250  -0.0809   0.01637   0.00907  -0.0568   0.0287   4.4441
  -3.000  -0.0755   0.01622   0.00891  -0.0542   0.0352   4.4460
  -2.500  -0.0427   0.01433   0.00843  -0.0529   0.0388   3.6549
  -2.250  -0.0020   0.01451   0.00964  -0.0530   0.0390   2.5538
  -2.000   0.0259   0.01557   0.01074  -0.0514   0.0456   2.3430
  -1.750   0.0567   0.01627   0.01135  -0.0509   0.0484   2.2384
  -1.500   0.0963   0.01687   0.01186  -0.0514   0.0496   2.1967
  -1.250   0.1198   0.01690   0.01179  -0.0511   0.0517   2.1656
  -1.000   0.1342   0.01694   0.01180  -0.0495   0.0601   2.1503
  -0.750   0.1584   0.01693   0.01171  -0.0490   0.0650   2.1355
  -0.500   0.1867   0.01690   0.01162  -0.0490   0.0677   2.1153
  -0.250   0.2146   0.01689   0.01154  -0.0491   0.0698   2.0917
   0.000   0.2235   0.01708   0.01173  -0.0469   0.0836   2.0702
   0.250   0.2490   0.01696   0.01156  -0.0467   0.0877   2.0594
   0.500   0.2754   0.01681   0.01136  -0.0467   0.0907   2.0469
   0.750   0.3026   0.01665   0.01117  -0.0467   0.0929   2.0328
   1.000   0.3104   0.01685   0.01139  -0.0444   0.1109   2.0183
   1.250   0.3356   0.01676   0.01128  -0.0443   0.1149   2.0054
   1.500   0.3577   0.01650   0.01100  -0.0439   0.1183   2.0009
   1.750   0.3578   0.01653   0.01104  -0.0412   0.1389   2.0009
   2.000   0.3747   0.01621   0.01070  -0.0403   0.1448   2.0009
   2.250   0.3943   0.01583   0.01029  -0.0398   0.1487   2.0009
   2.500   0.3943   0.01580   0.01028  -0.0369   0.1725   2.0009
   2.750   0.4135   0.01537   0.00983  -0.0362   0.1782   2.0009
   3.000   0.4343   0.01491   0.00936  -0.0357   0.1819   2.0009
   3.250   0.4325   0.01497   0.00946  -0.0327   0.2086   2.0009
   3.500   0.4521   0.01455   0.00904  -0.0319   0.2132   2.0009
   3.750   0.4522   0.01461   0.00911  -0.0291   0.2403   2.0009
   4.000   0.4714   0.01417   0.00868  -0.0283   0.2461   2.0009
   4.250   0.4744   0.01414   0.00867  -0.0258   0.2740   2.0009
   4.500   0.4936   0.01364   0.00820  -0.0249   0.2817   2.0009
   4.750   0.4989   0.01356   0.00815  -0.0226   0.3096   2.0009
   5.000   0.5171   0.01311   0.00772  -0.0216   0.3197   2.0009
   5.250   0.5382   0.01262   0.00726  -0.0209   0.3260   2.0009
   5.500   0.5420   0.01265   0.00732  -0.0185   0.3583   2.0009
   5.750   0.5628   0.01219   0.00690  -0.0178   0.3670   2.0009
   6.000   0.5712   0.01212   0.00687  -0.0159   0.3943   2.0009
   6.250   0.5888   0.01177   0.00656  -0.0148   0.4102   2.0009
   6.500   0.6121   0.01128   0.00611  -0.0143   0.4194   2.0009
   6.750   0.6169   0.01132   0.00621  -0.0120   0.4555   2.0009
   7.250   0.6464   0.01085   0.00585  -0.0094   0.5060   2.0009
   7.500   0.6711   0.01034   0.00539  -0.0089   0.5240   2.0009
   7.750   0.6783   0.01030   0.00541  -0.0069   0.5677   2.0009
   8.000   0.6992   0.00968   0.00476  -0.0058   0.6436   2.0009
   8.250   0.7155   0.00894   0.00357  -0.0039   0.9692   2.0009
   8.500   0.7086   0.00917   0.00347  -0.0003   1.2648   2.0009
   8.750   0.6943   0.00968   0.00369   0.0037   1.5464   2.0009
   9.000   0.6786   0.01032   0.00406   0.0075   1.8491   2.0009
   9.250   0.6644   0.01100   0.00450   0.0109   2.1797   2.0009
   9.500   0.6493   0.01181   0.00502   0.0142   2.5846   2.0009
   9.750   0.6283   0.01294   0.00572   0.0176   3.2479   2.0009
  10.000   0.6090   0.01411   0.00655   0.0206   4.1282   2.0009
  10.250   0.6080   0.01455   0.00704   0.0226   4.2096   2.0009
  10.500   0.6104   0.01485   0.00743   0.0243   4.2211   2.0009
  10.750   0.6114   0.01522   0.00789   0.0260   4.2331   2.0009
  11.000   0.6134   0.01554   0.00832   0.0276   4.2376   2.0009
  11.250   0.6149   0.01589   0.00878   0.0292   4.2418   2.0009
  11.500   0.6158   0.01628   0.00928   0.0308   4.2456   2.0009
  11.750   0.6164   0.01669   0.00980   0.0323   4.2483   2.0009
  12.000   0.6159   0.01718   0.01040   0.0338   4.2517   2.0009
  12.250   0.6151   0.01768   0.01102   0.0352   4.2542   2.0009
  12.500   0.6137   0.01824   0.01169   0.0365   4.2559   2.0009
  12.750   0.6110   0.01888   0.01245   0.0378   4.2576   2.0009
  13.000   0.6090   0.01950   0.01318   0.0390   4.2584   2.0009
  13.250   0.6068   0.02015   0.01394   0.0401   4.2590   2.0009
  13.500   0.6039   0.02087   0.01478   0.0411   4.2598   2.0009
  13.750   0.6003   0.02165   0.01567   0.0420   4.2600   2.0009
  14.000   0.5960   0.02249   0.01663   0.0428   4.2609   2.0009
  14.250   0.5918   0.02334   0.01759   0.0436   4.2609   2.0009
  14.500   0.5869   0.02428   0.01864   0.0442   4.2615   2.0009
  14.750   0.5821   0.02525   0.01970   0.0448   4.2619   2.0009
  15.000   0.5777   0.02622   0.02078   0.0452   4.2618   2.0009
  15.250   0.5734   0.02719   0.02184   0.0456   4.2621   2.0009
  15.500   0.5697   0.02813   0.02286   0.0460   4.2621   2.0009
  15.750   0.5669   0.02903   0.02383   0.0464   4.2625   2.0009
  16.000   0.5650   0.02987   0.02474   0.0468   4.2626   2.0009
  16.250   0.5645   0.03060   0.02553   0.0472   4.2628   2.0009
  16.500   0.5652   0.03123   0.02622   0.0477   4.2626   2.0009
  16.750   0.5671   0.03176   0.02680   0.0483   4.2626   2.0009
  17.000   0.5701   0.03224   0.02734   0.0489   4.2626   2.0009
  17.250   0.5741   0.03265   0.02780   0.0496   4.2625   2.0009
  17.500   0.5779   0.03311   0.02833   0.0502   4.2621   2.0009
  17.750   0.5820   0.03358   0.02888   0.0508   4.2617   2.0009
  18.000   0.5848   0.03420   0.02958   0.0513   4.2613   2.0009
  18.250   0.5870   0.03491   0.03038   0.0517   4.2610   2.0009
  18.500   0.5888   0.03572   0.03129   0.0520   4.2605   2.0009
  18.750   0.5886   0.03664   0.03231   0.0522   4.2600   2.0009
  19.000   0.5872   0.03772   0.03349   0.0522   4.2596   2.0009
  19.250   0.5855   0.03886   0.03474   0.0522   4.2590   2.0009
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