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NACA 5-H-15 AIRFOIL (n5h15-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 5-H-15 AIRFOIL (n5h15-il)
Reynolds number: 1,000,000
Max Cl/Cd: 85.49 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n5h15-il-1000000-n5.txt
Download as CSV file: xf-n5h15-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 5-H-15 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.1786   0.05079   0.04763  -0.0616   0.7621   0.0133
 -17.500  -1.1946   0.04660   0.04329  -0.0624   0.7593   0.0136
 -17.250  -1.2077   0.04314   0.03967  -0.0621   0.7563   0.0138
 -17.000  -1.2173   0.04030   0.03668  -0.0612   0.7532   0.0139
 -16.750  -1.2240   0.03787   0.03407  -0.0598   0.7502   0.0142
 -16.500  -1.2196   0.03644   0.03258  -0.0586   0.7471   0.0145
 -16.250  -1.2073   0.03569   0.03182  -0.0576   0.7436   0.0148
 -16.000  -1.1990   0.03467   0.03073  -0.0563   0.7399   0.0151
 -15.750  -1.1872   0.03397   0.02998  -0.0552   0.7366   0.0154
 -15.500  -1.1736   0.03340   0.02938  -0.0541   0.7337   0.0158
 -15.250  -1.1656   0.03240   0.02830  -0.0525   0.7306   0.0161
 -15.000  -1.1549   0.03162   0.02745  -0.0510   0.7272   0.0165
 -14.750  -1.1465   0.03066   0.02638  -0.0492   0.7238   0.0168
 -14.500  -1.1377   0.02972   0.02533  -0.0473   0.7206   0.0172
 -14.250  -1.1295   0.02871   0.02420  -0.0453   0.7177   0.0174
 -14.000  -1.1210   0.02771   0.02309  -0.0432   0.7145   0.0176
 -13.750  -1.1095   0.02692   0.02218  -0.0414   0.7107   0.0178
 -13.500  -1.0967   0.02623   0.02139  -0.0396   0.7072   0.0180
 -13.250  -1.0850   0.02557   0.02064  -0.0376   0.7038   0.0183
 -13.000  -1.0736   0.02478   0.01977  -0.0355   0.7007   0.0185
 -12.750  -1.0578   0.02447   0.01943  -0.0339   0.6973   0.0187
 -12.500  -1.0396   0.02447   0.01942  -0.0324   0.6939   0.0190
 -12.250  -1.0239   0.02416   0.01907  -0.0307   0.6908   0.0192
 -12.000  -1.0083   0.02382   0.01867  -0.0289   0.6879   0.0194
 -11.750  -0.9918   0.02360   0.01843  -0.0272   0.6850   0.0196
 -11.500  -0.9753   0.02345   0.01824  -0.0254   0.6819   0.0199
 -11.250  -0.9603   0.02289   0.01758  -0.0234   0.6789   0.0201
 -11.000  -0.9429   0.02254   0.01716  -0.0218   0.6759   0.0204
 -10.750  -0.9243   0.02204   0.01657  -0.0205   0.6731   0.0207
 -10.500  -0.9043   0.02169   0.01616  -0.0194   0.6705   0.0211
 -10.250  -0.8839   0.02130   0.01569  -0.0183   0.6672   0.0215
 -10.000  -0.8637   0.02069   0.01498  -0.0172   0.6637   0.0218
  -9.750  -0.8427   0.02020   0.01438  -0.0163   0.6601   0.0220
  -9.500  -0.8210   0.01984   0.01394  -0.0154   0.6568   0.0222
  -9.250  -0.7989   0.01940   0.01343  -0.0146   0.6543   0.0224
  -9.000  -0.7765   0.01889   0.01283  -0.0138   0.6514   0.0225
  -8.750  -0.7537   0.01843   0.01229  -0.0131   0.6485   0.0226
  -8.500  -0.7311   0.01751   0.01124  -0.0125   0.6456   0.0229
  -8.000  -0.6848   0.01607   0.00965  -0.0114   0.6400   0.0236
  -7.750  -0.6609   0.01559   0.00912  -0.0109   0.6377   0.0238
  -7.500  -0.6367   0.01517   0.00865  -0.0104   0.6352   0.0240
  -7.250  -0.6124   0.01477   0.00820  -0.0099   0.6326   0.0242
  -7.000  -0.5879   0.01439   0.00777  -0.0094   0.6301   0.0244
  -6.750  -0.5634   0.01405   0.00738  -0.0090   0.6275   0.0246
  -6.500  -0.5387   0.01369   0.00699  -0.0085   0.6252   0.0248
  -6.250  -0.5138   0.01334   0.00661  -0.0081   0.6227   0.0250
  -6.000  -0.4890   0.01303   0.00626  -0.0077   0.6202   0.0253
  -5.750  -0.4641   0.01272   0.00592  -0.0072   0.6175   0.0256
  -5.500  -0.4392   0.01243   0.00559  -0.0068   0.6146   0.0259
  -5.250  -0.4141   0.01220   0.00531  -0.0064   0.6116   0.0263
  -5.000  -0.3888   0.01194   0.00503  -0.0060   0.6093   0.0268
  -4.750  -0.3637   0.01167   0.00474  -0.0056   0.6067   0.0270
  -4.500  -0.3383   0.01144   0.00448  -0.0052   0.6037   0.0273
  -4.250  -0.3131   0.01121   0.00422  -0.0048   0.6008   0.0276
  -4.000  -0.2876   0.01101   0.00398  -0.0045   0.5983   0.0278
  -3.750  -0.2620   0.01084   0.00378  -0.0042   0.5959   0.0280
  -3.500  -0.2362   0.01065   0.00358  -0.0039   0.5938   0.0282
  -3.250  -0.2102   0.01047   0.00339  -0.0036   0.5913   0.0283
  -3.000  -0.1844   0.01028   0.00319  -0.0033   0.5886   0.0286
  -2.750  -0.1592   0.01006   0.00294  -0.0029   0.5857   0.0291
  -2.500  -0.1335   0.00989   0.00274  -0.0026   0.5829   0.0298
  -2.250  -0.1075   0.00975   0.00259  -0.0023   0.5801   0.0305
  -2.000  -0.0811   0.00961   0.00246  -0.0021   0.5772   0.0311
  -1.750  -0.0547   0.00949   0.00234  -0.0019   0.5737   0.0319
  -1.500  -0.0283   0.00939   0.00224  -0.0018   0.5697   0.0330
  -1.250  -0.0019   0.00932   0.00214  -0.0016   0.5657   0.0342
  -1.000   0.0250   0.00923   0.00206  -0.0015   0.5621   0.0354
  -0.750   0.0516   0.00914   0.00198  -0.0014   0.5574   0.0374
  -0.500   0.0779   0.00906   0.00191  -0.0012   0.5525   0.0412
  -0.250   0.1045   0.00898   0.00186  -0.0011   0.5480   0.0473
   0.000   0.1308   0.00889   0.00181  -0.0009   0.5421   0.0588
   0.250   0.1565   0.00881   0.00176  -0.0007   0.5358   0.0783
   0.500   0.1801   0.00856   0.00171   0.0000   0.5289   0.1485
   0.750   0.1996   0.00816   0.00164   0.0013   0.5209   0.2725
   1.000   0.2010   0.00699   0.00146   0.0062   0.5130   0.5724
   1.250   0.1956   0.00608   0.00146   0.0134   0.5048   0.8301
   1.500   0.2210   0.00617   0.00154   0.0138   0.4936   0.8498
   1.750   0.2463   0.00629   0.00164   0.0143   0.4832   0.8655
   2.000   0.2727   0.00642   0.00175   0.0145   0.4741   0.8754
   2.250   0.2989   0.00654   0.00185   0.0147   0.4660   0.8840
   2.500   0.3247   0.00669   0.00198   0.0151   0.4597   0.8926
   2.750   0.3506   0.00678   0.00205   0.0153   0.4544   0.8959
   3.000   0.3786   0.00686   0.00211   0.0150   0.4494   0.8976
   3.250   0.4064   0.00695   0.00220   0.0148   0.4453   0.8999
   3.500   0.4342   0.00703   0.00227   0.0146   0.4422   0.9019
   3.750   0.4616   0.00710   0.00235   0.0145   0.4391   0.9037
   4.000   0.4887   0.00719   0.00243   0.0144   0.4355   0.9051
   4.500   0.5415   0.00741   0.00262   0.0144   0.4254   0.9087
   4.750   0.5669   0.00755   0.00273   0.0146   0.4178   0.9101
   5.000   0.5926   0.00767   0.00284   0.0147   0.4122   0.9113
   5.250   0.6187   0.00778   0.00294   0.0147   0.4058   0.9124
   5.500   0.6450   0.00791   0.00306   0.0146   0.4005   0.9137
   5.750   0.6714   0.00802   0.00319   0.0146   0.3931   0.9151
   6.000   0.6959   0.00822   0.00335   0.0148   0.3811   0.9166
   6.250   0.7198   0.00842   0.00352   0.0151   0.3673   0.9181
   6.500   0.7361   0.00891   0.00383   0.0167   0.3192   0.9204
   6.750   0.7249   0.01028   0.00477   0.0227   0.2299   0.9256
   7.000   0.7197   0.01110   0.00542   0.0279   0.1879   0.9306
   7.250   0.7136   0.01219   0.00639   0.0324   0.1519   0.9381
   7.500   0.7065   0.01378   0.00777   0.0361   0.1003   0.9465
   7.750   0.7144   0.01542   0.00923   0.0365   0.0542   0.9534
   8.250   0.7545   0.01781   0.01149   0.0341   0.0150   0.9618
   8.500   0.7826   0.01855   0.01225   0.0322   0.0142   0.9640
   8.750   0.8092   0.01944   0.01316   0.0303   0.0126   0.9661
   9.000   0.8338   0.02041   0.01417   0.0286   0.0114   0.9686
   9.250   0.8572   0.02128   0.01506   0.0274   0.0109   0.9716
   9.500   0.8808   0.02222   0.01603   0.0260   0.0104   0.9737
   9.750   0.9032   0.02320   0.01704   0.0247   0.0098   0.9760
  10.000   0.9233   0.02428   0.01814   0.0238   0.0094   0.9789
  10.250   0.9411   0.02538   0.01928   0.0232   0.0091   0.9827
  10.500   0.9571   0.02674   0.02067   0.0226   0.0085   0.9859
  10.750   0.9750   0.02789   0.02185   0.0219   0.0081   0.9892
  11.000   0.9911   0.02910   0.02310   0.0215   0.0079   0.9927
  11.250   1.0059   0.03047   0.02450   0.0213   0.0078   0.9983
  11.500   1.0231   0.03190   0.02597   0.0204   0.0075   0.9994
  11.750   1.0407   0.03305   0.02713   0.0198   0.0070   1.0000
  12.000   1.0433   0.03452   0.02866   0.0215   0.0072   1.0000
  12.250   1.0501   0.03578   0.02994   0.0228   0.0069   1.0000
  12.500   1.0576   0.03708   0.03126   0.0239   0.0066   1.0000
  12.750   1.0647   0.03847   0.03268   0.0249   0.0064   1.0000
  13.000   1.0698   0.04012   0.03438   0.0259   0.0064   1.0000
  13.250   1.0757   0.04173   0.03603   0.0268   0.0063   1.0000
  13.500   1.0775   0.04378   0.03813   0.0277   0.0060   1.0000
  13.750   1.0832   0.04553   0.03993   0.0284   0.0060   1.0000
  14.000   1.0896   0.04728   0.04173   0.0289   0.0059   1.0000
  14.250   1.1007   0.04858   0.04306   0.0292   0.0057   1.0000
  14.500   1.1054   0.05055   0.04508   0.0297   0.0056   1.0000
  14.750   1.1114   0.05242   0.04701   0.0301   0.0055   1.0000
  15.000   1.1150   0.05459   0.04924   0.0304   0.0055   1.0000
  15.250   1.1211   0.05651   0.05120   0.0307   0.0054   1.0000
  15.500   1.1261   0.05860   0.05336   0.0308   0.0053   1.0000
  15.750   1.1321   0.06059   0.05539   0.0309   0.0052   1.0000
  16.000   1.1394   0.06250   0.05734   0.0309   0.0050   1.0000
  16.250   1.1446   0.06465   0.05954   0.0309   0.0049   1.0000
  16.500   1.1474   0.06712   0.06208   0.0309   0.0049   1.0000
  16.750   1.1527   0.06931   0.06431   0.0308   0.0048   1.0000
  17.000   1.1566   0.07170   0.06676   0.0305   0.0047   1.0000
  17.250   1.1616   0.07398   0.06908   0.0303   0.0046   1.0000
  17.500   1.1627   0.07678   0.07195   0.0300   0.0046   1.0000
  17.750   1.1648   0.07948   0.07470   0.0296   0.0044   1.0000
  18.000   1.1658   0.08234   0.07763   0.0292   0.0045   1.0000
  18.250   1.1652   0.08543   0.08079   0.0287   0.0044   1.0000
  18.500   1.1643   0.08860   0.08403   0.0281   0.0043   1.0000
  18.750   1.1583   0.09247   0.08798   0.0274   0.0042   1.0000
  19.000   1.1574   0.09573   0.09131   0.0266   0.0042   1.0000
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