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NACA CYH (nacacyh-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA CYH (nacacyh-il)
Reynolds number: 500,000
Max Cl/Cd: 86.96 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-nacacyh-il-500000-n5.txt
Download as CSV file: xf-nacacyh-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA CYH                                        
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.9907   0.04498   0.04197  -0.0615   1.0000   0.0174
 -14.250  -1.0095   0.04039   0.03715  -0.0627   1.0000   0.0175
 -14.000  -1.0112   0.03829   0.03495  -0.0615   1.0000   0.0176
 -13.750  -1.0057   0.03697   0.03355  -0.0599   1.0000   0.0178
 -13.500  -0.9933   0.03611   0.03263  -0.0585   1.0000   0.0181
 -13.250  -0.9777   0.03538   0.03187  -0.0574   1.0000   0.0183
 -13.000  -0.9617   0.03462   0.03105  -0.0563   1.0000   0.0186
 -12.750  -0.9468   0.03363   0.02997  -0.0552   1.0000   0.0190
 -12.500  -0.9330   0.03239   0.02859  -0.0540   1.0000   0.0194
 -12.250  -0.9200   0.03091   0.02694  -0.0527   1.0000   0.0199
 -12.000  -0.9070   0.02931   0.02513  -0.0513   1.0000   0.0204
 -11.750  -0.8924   0.02784   0.02342  -0.0498   1.0000   0.0210
 -11.500  -0.8754   0.02669   0.02206  -0.0485   1.0000   0.0214
 -11.250  -0.8566   0.02583   0.02102  -0.0472   1.0000   0.0217
 -11.000  -0.8417   0.02437   0.01945  -0.0456   1.0000   0.0222
 -10.750  -0.8154   0.02356   0.01858  -0.0458   0.9918   0.0226
 -10.500  -0.7854   0.02292   0.01787  -0.0466   0.9787   0.0231
 -10.250  -0.7555   0.02228   0.01714  -0.0473   0.9631   0.0236
 -10.000  -0.7277   0.02155   0.01628  -0.0475   0.9444   0.0242
  -9.750  -0.7039   0.02078   0.01535  -0.0467   0.9202   0.0247
  -9.500  -0.6818   0.02013   0.01451  -0.0455   0.8941   0.0252
  -9.250  -0.6596   0.01954   0.01372  -0.0443   0.8695   0.0258
  -9.000  -0.6367   0.01896   0.01293  -0.0432   0.8488   0.0262
  -8.750  -0.6130   0.01836   0.01215  -0.0423   0.8315   0.0266
  -8.500  -0.5886   0.01785   0.01146  -0.0415   0.8170   0.0268
  -8.250  -0.5640   0.01729   0.01075  -0.0407   0.8043   0.0272
  -8.000  -0.5406   0.01628   0.00960  -0.0399   0.7934   0.0278
  -7.750  -0.5157   0.01567   0.00889  -0.0393   0.7838   0.0283
  -7.500  -0.4902   0.01516   0.00830  -0.0387   0.7747   0.0287
  -7.250  -0.4644   0.01471   0.00776  -0.0382   0.7667   0.0291
  -7.000  -0.4384   0.01428   0.00725  -0.0377   0.7590   0.0295
  -6.750  -0.4122   0.01388   0.00678  -0.0372   0.7523   0.0300
  -6.500  -0.3858   0.01352   0.00635  -0.0368   0.7452   0.0305
  -6.250  -0.3593   0.01320   0.00596  -0.0363   0.7390   0.0312
  -6.000  -0.3325   0.01286   0.00556  -0.0360   0.7330   0.0317
  -5.750  -0.3058   0.01255   0.00518  -0.0355   0.7260   0.0321
  -5.500  -0.2790   0.01226   0.00483  -0.0352   0.7187   0.0326
  -5.250  -0.2521   0.01199   0.00449  -0.0348   0.7111   0.0330
  -5.000  -0.2250   0.01176   0.00420  -0.0345   0.7042   0.0333
  -4.750  -0.1979   0.01150   0.00390  -0.0342   0.6968   0.0338
  -4.500  -0.1711   0.01122   0.00356  -0.0338   0.6901   0.0347
  -4.250  -0.1437   0.01098   0.00330  -0.0336   0.6833   0.0357
  -4.000  -0.1164   0.01081   0.00308  -0.0333   0.6760   0.0368
  -3.750  -0.0888   0.01063   0.00288  -0.0331   0.6681   0.0383
  -3.500  -0.0613   0.01050   0.00270  -0.0329   0.6599   0.0401
  -3.250  -0.0336   0.01034   0.00253  -0.0327   0.6517   0.0426
  -3.000  -0.0061   0.01019   0.00238  -0.0325   0.6444   0.0481
  -2.750   0.0213   0.00999   0.00226  -0.0323   0.6371   0.0650
  -2.500   0.0488   0.00985   0.00215  -0.0322   0.6293   0.0826
  -2.250   0.0764   0.00971   0.00205  -0.0320   0.6213   0.0991
  -2.000   0.1036   0.00955   0.00196  -0.0319   0.6134   0.1263
  -1.750   0.1306   0.00933   0.00189  -0.0317   0.6053   0.1700
  -1.500   0.1574   0.00915   0.00183  -0.0316   0.5970   0.2195
  -1.250   0.1844   0.00896   0.00180  -0.0314   0.5875   0.2693
  -1.000   0.2109   0.00876   0.00176  -0.0312   0.5776   0.3289
  -0.750   0.2364   0.00849   0.00172  -0.0309   0.5666   0.4136
  -0.500   0.2609   0.00811   0.00169  -0.0304   0.5556   0.5263
  -0.250   0.2737   0.00710   0.00179  -0.0268   0.5463   0.8578
   0.000   0.3006   0.00715   0.00191  -0.0262   0.5348   0.9122
   0.250   0.3315   0.00727   0.00201  -0.0265   0.5221   0.9355
   0.500   0.3634   0.00741   0.00209  -0.0272   0.5086   0.9509
   0.750   0.3963   0.00759   0.00219  -0.0282   0.4930   0.9632
   1.000   0.4280   0.00776   0.00227  -0.0290   0.4755   0.9712
   1.250   0.4634   0.00794   0.00235  -0.0307   0.4567   0.9751
   1.500   0.4992   0.00812   0.00244  -0.0325   0.4371   0.9785
   1.750   0.5314   0.00831   0.00253  -0.0336   0.4175   0.9828
   2.000   0.5668   0.00851   0.00264  -0.0355   0.3985   0.9855
   2.750   0.6657   0.00913   0.00300  -0.0397   0.3512   0.9929
   3.000   0.6960   0.00934   0.00313  -0.0405   0.3373   0.9944
   3.250   0.7273   0.00951   0.00326  -0.0416   0.3266   0.9957
   3.500   0.7580   0.00971   0.00340  -0.0426   0.3177   0.9972
   3.750   0.7887   0.00987   0.00354  -0.0435   0.3078   0.9986
   4.000   0.8191   0.01005   0.00370  -0.0445   0.2999   0.9999
   4.250   0.8433   0.01019   0.00384  -0.0440   0.2939   1.0000
   4.500   0.8662   0.01037   0.00401  -0.0433   0.2877   1.0000
   4.750   0.8894   0.01051   0.00417  -0.0427   0.2812   1.0000
   5.000   0.9121   0.01070   0.00434  -0.0419   0.2737   1.0000
   5.250   0.9350   0.01087   0.00452  -0.0412   0.2674   1.0000
   5.500   0.9576   0.01105   0.00470  -0.0405   0.2595   1.0000
   5.750   0.9800   0.01127   0.00491  -0.0398   0.2483   1.0000
   6.000   1.0012   0.01157   0.00513  -0.0389   0.2297   1.0000
   6.250   1.0209   0.01200   0.00542  -0.0378   0.2008   1.0000
   6.500   1.0392   0.01254   0.00580  -0.0365   0.1726   1.0000
   6.750   1.0577   0.01306   0.00622  -0.0353   0.1522   1.0000
   7.000   1.0766   0.01355   0.00663  -0.0341   0.1348   1.0000
   7.250   1.0954   0.01407   0.00707  -0.0330   0.1185   1.0000
   7.500   1.1145   0.01457   0.00751  -0.0319   0.1052   1.0000
   7.750   1.1341   0.01505   0.00796  -0.0310   0.0951   1.0000
   8.000   1.1532   0.01558   0.00844  -0.0300   0.0849   1.0000
   8.250   1.1721   0.01612   0.00895  -0.0290   0.0766   1.0000
   8.500   1.1920   0.01658   0.00941  -0.0282   0.0698   1.0000
   8.750   1.2106   0.01712   0.00995  -0.0273   0.0626   1.0000
   9.000   1.2279   0.01775   0.01053  -0.0262   0.0529   1.0000
   9.250   1.2397   0.01871   0.01136  -0.0244   0.0327   1.0000
   9.500   1.2442   0.01999   0.01253  -0.0216   0.0177   1.0000
   9.750   1.2557   0.02077   0.01336  -0.0198   0.0156   1.0000
  10.000   1.2676   0.02159   0.01424  -0.0182   0.0144   1.0000
  10.250   1.2785   0.02254   0.01526  -0.0167   0.0135   1.0000
  10.500   1.2886   0.02362   0.01641  -0.0153   0.0127   1.0000
  10.750   1.3006   0.02462   0.01749  -0.0144   0.0123   1.0000
  11.000   1.3115   0.02577   0.01872  -0.0135   0.0118   1.0000
  11.250   1.3214   0.02705   0.02009  -0.0127   0.0113   1.0000
  11.500   1.3302   0.02850   0.02163  -0.0120   0.0109   1.0000
  11.750   1.3375   0.03015   0.02337  -0.0115   0.0104   1.0000
  12.000   1.3426   0.03207   0.02537  -0.0110   0.0101   1.0000
  12.250   1.3445   0.03438   0.02777  -0.0105   0.0097   1.0000
  12.500   1.3496   0.03643   0.02992  -0.0103   0.0095   1.0000
  12.750   1.3537   0.03863   0.03222  -0.0102   0.0093   1.0000
  13.000   1.3561   0.04105   0.03474  -0.0102   0.0091   1.0000
  13.250   1.3572   0.04368   0.03747  -0.0103   0.0089   1.0000
  13.500   1.3567   0.04654   0.04044  -0.0105   0.0087   1.0000
  13.750   1.3546   0.04967   0.04368  -0.0109   0.0086   1.0000
  14.000   1.3512   0.05305   0.04717  -0.0114   0.0084   1.0000
  14.250   1.3468   0.05667   0.05089  -0.0121   0.0083   1.0000
  14.500   1.3414   0.06056   0.05490  -0.0130   0.0082   1.0000
  14.750   1.3351   0.06472   0.05917  -0.0141   0.0081   1.0000
  15.000   1.3277   0.06915   0.06371  -0.0153   0.0080   1.0000
  15.250   1.3192   0.07385   0.06852  -0.0168   0.0079   1.0000
  15.500   1.3100   0.07880   0.07358  -0.0184   0.0078   1.0000
  15.750   1.2998   0.08393   0.07882  -0.0201   0.0077   1.0000
  16.000   1.2888   0.08931   0.08431  -0.0219   0.0076   1.0000
  16.250   1.2775   0.09479   0.08990  -0.0239   0.0076   1.0000
  16.500   1.2659   0.10038   0.09559  -0.0259   0.0075   1.0000
  16.750   1.2539   0.10610   0.10141  -0.0281   0.0074   1.0000
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