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WORTMANN FX 08-S-176 AIRFOIL (fx08s176-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 08-S-176 AIRFOIL (fx08s176-il)
Reynolds number: 100,000
Max Cl/Cd: 20.42 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx08s176-il-100000-n5.txt
Download as CSV file: xf-fx08s176-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 08-S-176 AIRFOIL                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.1087   0.12474   0.11825  -0.0811   0.6495   0.0490
 -11.750  -0.1067   0.12170   0.11522  -0.0833   0.6486   0.0492
 -11.500  -0.1081   0.11858   0.11215  -0.0861   0.6477   0.0494
 -11.250  -0.1064   0.11511   0.10872  -0.0883   0.6466   0.0495
 -11.000  -0.0884   0.11005   0.10367  -0.0869   0.6451   0.0505
 -10.750  -0.0778   0.10670   0.10032  -0.0871   0.6436   0.0512
 -10.500  -0.0735   0.10332   0.09697  -0.0884   0.6424   0.0514
 -10.000  -0.0680   0.09452   0.08818  -0.0917   0.6400   0.0369
  -9.750  -0.0650   0.09098   0.08466  -0.0928   0.6387   0.0355
  -9.500  -0.0649   0.08721   0.08091  -0.0946   0.6377   0.0346
  -9.250  -0.0667   0.08324   0.07698  -0.0967   0.6368   0.0343
  -9.000  -0.0704   0.07898   0.07276  -0.0993   0.6359   0.0341
  -8.750  -0.0778   0.07422   0.06804  -0.1029   0.6350   0.0338
  -8.500  -0.0878   0.06999   0.06379  -0.1053   0.6342   0.0342
  -8.250  -0.1038   0.06608   0.05987  -0.1058   0.6333   0.0331
  -8.000  -0.1197   0.06291   0.05666  -0.1047   0.6322   0.0327
  -7.750  -0.1267   0.05997   0.05364  -0.1038   0.6309   0.0329
  -7.500  -0.1320   0.05680   0.05032  -0.1025   0.6295   0.0328
  -7.250  -0.1351   0.05343   0.04674  -0.1009   0.6280   0.0326
  -7.000  -0.1347   0.05011   0.04314  -0.0991   0.6265   0.0323
  -6.750  -0.1299   0.04714   0.03988  -0.0973   0.6250   0.0323
  -6.500  -0.1217   0.04442   0.03680  -0.0956   0.6237   0.0326
  -6.250  -0.1092   0.04235   0.03443  -0.0942   0.6225   0.0337
  -6.000  -0.0949   0.04035   0.03205  -0.0927   0.6214   0.0355
  -5.750  -0.0788   0.03817   0.02940  -0.0913   0.6204   0.0368
  -5.500  -0.0600   0.03614   0.02691  -0.0900   0.6195   0.0374
  -5.250  -0.0410   0.03457   0.02500  -0.0888   0.6178   0.0380
  -5.000  -0.0207   0.03327   0.02343  -0.0878   0.6159   0.0392
  -4.750   0.0000   0.03254   0.02269  -0.0873   0.6139   0.0414
  -4.500   0.0226   0.03182   0.02183  -0.0867   0.6121   0.0435
  -4.250   0.0466   0.03090   0.02071  -0.0861   0.6105   0.0448
  -4.000   0.0711   0.03010   0.01974  -0.0856   0.6092   0.0464
  -3.750   0.0957   0.02943   0.01892  -0.0850   0.6079   0.0481
  -3.500   0.1198   0.02883   0.01824  -0.0845   0.6067   0.0502
  -3.250   0.1431   0.02842   0.01786  -0.0840   0.6056   0.0545
  -3.000   0.1644   0.02821   0.01760  -0.0832   0.6040   0.0588
  -2.750   0.1804   0.02829   0.01768  -0.0816   0.6012   0.0620
  -2.500   0.1969   0.02816   0.01761  -0.0803   0.5990   0.0671
  -2.250   0.2158   0.02817   0.01755  -0.0792   0.5971   0.0757
  -2.000   0.2353   0.02803   0.01747  -0.0781   0.5954   0.0922
  -1.750   0.2559   0.02778   0.01740  -0.0773   0.5938   0.1295
  -1.500   0.2633   0.02610   0.01733  -0.0747   0.5924   0.4915
  -1.250   0.2656   0.02678   0.01902  -0.0659   0.5912   0.8207
  -1.000   0.2752   0.02764   0.01977  -0.0616   0.5894   0.8640
  -0.750   0.2715   0.02910   0.02132  -0.0571   0.5848   0.8840
  -0.500   0.2932   0.02990   0.02201  -0.0553   0.5820   0.9123
  -0.250   0.3289   0.03034   0.02227  -0.0565   0.5801   0.9324
   0.000   0.3928   0.03064   0.02232  -0.0632   0.5789   0.9464
   0.250   0.4620   0.03071   0.02215  -0.0712   0.5778   0.9547
   0.500   0.4871   0.03079   0.02208  -0.0711   0.5765   0.9599
   1.000   0.5099   0.03326   0.02459  -0.0699   0.5669   0.9717
   1.250   0.5388   0.03342   0.02465  -0.0709   0.5647   0.9748
   1.500   0.5726   0.03335   0.02446  -0.0724   0.5632   0.9773
   1.750   0.6063   0.03321   0.02419  -0.0736   0.5619   0.9799
   2.250   0.6226   0.03610   0.02716  -0.0722   0.5502   0.9916
   2.500   0.6539   0.03600   0.02698  -0.0731   0.5486   0.9943
   2.750   0.6901   0.03577   0.02667  -0.0748   0.5475   0.9967
   3.000   0.7272   0.03561   0.02644  -0.0767   0.5465   0.9996
   3.500   0.6455   0.03940   0.03034  -0.0590   0.5324   1.0000
   4.500   0.5330   0.04788   0.03888  -0.0378   0.4978   1.0000
   4.750   0.5502   0.04844   0.03940  -0.0373   0.4945   1.0000
   5.000   0.5741   0.04861   0.03953  -0.0371   0.4927   1.0000
   5.250   0.6001   0.04866   0.03954  -0.0372   0.4913   1.0000
   5.750   0.6141   0.05156   0.04245  -0.0358   0.4790   1.0000
   6.000   0.6112   0.05392   0.04483  -0.0349   0.4703   1.0000
   6.250   0.6310   0.05459   0.04549  -0.0350   0.4673   1.0000
   6.500   0.6554   0.05489   0.04578  -0.0351   0.4653   1.0000
   6.750   0.6814   0.05506   0.04595  -0.0354   0.4640   1.0000
   7.250   0.6952   0.05868   0.04964  -0.0348   0.4518   1.0000
   8.250   0.7566   0.06340   0.05449  -0.0349   0.4369   1.0000
   8.750   0.7650   0.06816   0.05936  -0.0347   0.4253   1.0000
   9.000   0.7886   0.06856   0.05980  -0.0349   0.4236   1.0000
   9.250   0.8134   0.06885   0.06016  -0.0352   0.4224   1.0000
   9.750   0.8152   0.07468   0.06613  -0.0352   0.4105   1.0000
  10.000   0.8387   0.07509   0.06661  -0.0354   0.4090   1.0000
  10.500   0.8411   0.08107   0.07274  -0.0357   0.3975   1.0000
  11.000   0.8766   0.08325   0.07511  -0.0362   0.3926   1.0000
  11.500   0.8905   0.08790   0.07995  -0.0367   0.3823   1.0000
  11.750   0.9138   0.08824   0.08040  -0.0369   0.3807   1.0000
  14.750   1.0715   0.10123   0.09483  -0.0385   0.2781   1.0000
  15.000   1.0613   0.10631   0.10004  -0.0397   0.2608   1.0000
  15.250   1.0958   0.10270   0.09531  -0.0382   0.1451   1.0000
  15.500   1.0723   0.10936   0.10153  -0.0395   0.0959   1.0000
  15.750   1.0517   0.11585   0.10763  -0.0410   0.0538   1.0000
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