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HAM-STD HS1-430 AIRFOIL (hs1430-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: HAM-STD HS1-430 AIRFOIL (hs1430-il)
Reynolds number: 1,000,000
Max Cl/Cd: 29.16 at α=10.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hs1430-il-1000000.txt
Download as CSV file: xf-hs1430-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HAM-STD HS1-430 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  -1.1461   0.05031   0.04522  -0.1368   0.9781   0.1062
 -19.500  -1.1404   0.04806   0.04293  -0.1373   0.9770   0.1074
 -19.250  -1.1325   0.04609   0.04091  -0.1378   0.9759   0.1086
 -19.000  -1.1230   0.04449   0.03927  -0.1378   0.9747   0.1098
 -18.750  -1.1151   0.04288   0.03760  -0.1375   0.9728   0.1107
 -18.500  -1.1035   0.04152   0.03619  -0.1374   0.9709   0.1117
 -18.250  -1.1019   0.03937   0.03402  -0.1369   0.9692   0.1133
 -18.000  -1.0931   0.03779   0.03242  -0.1366   0.9676   0.1148
 -17.750  -1.0822   0.03636   0.03097  -0.1363   0.9660   0.1161
 -17.500  -1.0705   0.03503   0.02959  -0.1360   0.9644   0.1174
 -17.250  -1.0554   0.03393   0.02845  -0.1357   0.9621   0.1186
 -17.000  -1.0414   0.03293   0.02741  -0.1352   0.9596   0.1197
 -16.750  -1.0279   0.03190   0.02633  -0.1346   0.9564   0.1206
 -16.500  -1.0189   0.03056   0.02498  -0.1337   0.9538   0.1225
 -16.250  -1.0073   0.02938   0.02378  -0.1329   0.9511   0.1241
 -16.000  -0.9919   0.02842   0.02280  -0.1323   0.9486   0.1256
 -15.750  -0.9757   0.02762   0.02198  -0.1318   0.9461   0.1271
 -15.500  -0.9592   0.02684   0.02116  -0.1312   0.9432   0.1284
 -15.250  -0.9406   0.02617   0.02046  -0.1308   0.9404   0.1295
 -15.000  -0.9249   0.02533   0.01959  -0.1301   0.9379   0.1310
 -14.750  -0.9106   0.02444   0.01868  -0.1292   0.9353   0.1327
 -14.500  -0.8936   0.02379   0.01804  -0.1284   0.9316   0.1343
 -14.250  -0.8753   0.02320   0.01743  -0.1278   0.9275   0.1359
 -14.000  -0.8560   0.02262   0.01682  -0.1272   0.9237   0.1374
 -13.750  -0.8350   0.02214   0.01630  -0.1268   0.9196   0.1388
 -13.500  -0.8128   0.02171   0.01582  -0.1266   0.9164   0.1398
 -13.250  -0.7966   0.02101   0.01508  -0.1255   0.9131   0.1415
 -13.000  -0.7794   0.02046   0.01455  -0.1245   0.9085   0.1432
 -12.750  -0.7598   0.02000   0.01408  -0.1237   0.9012   0.1447
 -12.500  -0.7397   0.01960   0.01366  -0.1230   0.8883   0.1462
 -12.250  -0.7194   0.01921   0.01317  -0.1221   0.8690   0.1477
 -12.000  -0.7010   0.01898   0.01273  -0.1207   0.8277   0.1489
 -11.750  -0.6856   0.01898   0.01243  -0.1187   0.7745   0.1499
 -11.500  -0.6681   0.01890   0.01217  -0.1171   0.7429   0.1506
 -11.250  -0.6575   0.01848   0.01164  -0.1145   0.7173   0.1526
 -11.000  -0.6422   0.01818   0.01126  -0.1127   0.6978   0.1544
 -10.750  -0.6247   0.01791   0.01092  -0.1112   0.6826   0.1559
 -10.500  -0.6076   0.01770   0.01063  -0.1095   0.6672   0.1574
 -10.250  -0.5905   0.01751   0.01034  -0.1078   0.6480   0.1587
 -10.000  -0.5717   0.01733   0.01009  -0.1064   0.6346   0.1600
  -9.750  -0.5529   0.01720   0.00987  -0.1049   0.6187   0.1611
  -9.500  -0.5351   0.01707   0.00964  -0.1032   0.6015   0.1621
  -9.250  -0.5242   0.01681   0.00931  -0.1002   0.5807   0.1643
  -9.000  -0.5351   0.01759   0.00936  -0.0927   0.4054   0.1655
  -8.750  -0.5387   0.01809   0.00936  -0.0866   0.2633   0.1668
  -8.500  -0.5273   0.01798   0.00919  -0.0835   0.2465   0.1683
  -8.250  -0.5146   0.01783   0.00902  -0.0805   0.2415   0.1698
  -8.000  -0.5041   0.01770   0.00887  -0.0771   0.2387   0.1714
  -7.750  -0.4977   0.01759   0.00872  -0.0727   0.2368   0.1726
  -7.500  -0.4925   0.01748   0.00859  -0.0679   0.2354   0.1738
  -7.250  -0.4865   0.01737   0.00849  -0.0634   0.2343   0.1758
  -7.000  -0.4760   0.01730   0.00843  -0.0598   0.2332   0.1778
  -6.750  -0.4626   0.01726   0.00839  -0.0568   0.2321   0.1798
  -6.500  -0.4464   0.01723   0.00836  -0.0544   0.2313   0.1818
  -6.250  -0.4281   0.01721   0.00833  -0.0524   0.2305   0.1838
  -6.000  -0.4085   0.01720   0.00830  -0.0508   0.2300   0.1853
  -5.750  -0.3894   0.01714   0.00825  -0.0490   0.2296   0.1875
  -5.500  -0.3689   0.01712   0.00823  -0.0475   0.2293   0.1897
  -5.250  -0.3481   0.01713   0.00824  -0.0461   0.2289   0.1919
  -5.000  -0.3268   0.01716   0.00826  -0.0448   0.2285   0.1941
  -4.750  -0.3048   0.01720   0.00829  -0.0437   0.2281   0.1961
  -4.500  -0.2818   0.01727   0.00833  -0.0427   0.2277   0.1976
  -4.250  -0.2596   0.01728   0.00833  -0.0416   0.2275   0.1993
  -4.000  -0.2389   0.01719   0.00827  -0.0403   0.2272   0.2025
  -3.750  -0.2168   0.01719   0.00828  -0.0392   0.2270   0.2048
  -3.500  -0.1944   0.01722   0.00831  -0.0382   0.2268   0.2070
  -3.250  -0.1717   0.01727   0.00836  -0.0372   0.2266   0.2090
  -3.000  -0.1485   0.01733   0.00841  -0.0364   0.2264   0.2108
  -2.750  -0.1248   0.01741   0.00847  -0.0357   0.2262   0.2121
  -2.500  -0.1014   0.01746   0.00852  -0.0349   0.2260   0.2136
  -2.250  -0.0791   0.01744   0.00850  -0.0339   0.2258   0.2168
  -2.000  -0.0565   0.01747   0.00856  -0.0330   0.2256   0.2193
  -1.750  -0.0336   0.01754   0.00864  -0.0322   0.2253   0.2215
  -1.500  -0.0103   0.01763   0.00873  -0.0314   0.2250   0.2235
  -1.250   0.0134   0.01773   0.00883  -0.0307   0.2247   0.2252
  -1.000   0.0371   0.01785   0.00894  -0.0301   0.2244   0.2267
  -0.750   0.0606   0.01797   0.00905  -0.0294   0.2242   0.2279
  -0.500   0.0840   0.01811   0.00919  -0.0287   0.2240   0.2288
  -0.250   0.1074   0.01825   0.00932  -0.0280   0.2238   0.2298
   0.000   0.1305   0.01835   0.00942  -0.0273   0.2236   0.2324
   0.250   0.1538   0.01846   0.00955  -0.0266   0.2234   0.2349
   0.500   0.1768   0.01861   0.00971  -0.0259   0.2231   0.2372
   0.750   0.1999   0.01877   0.00988  -0.0252   0.2230   0.2392
   1.000   0.2228   0.01894   0.01007  -0.0245   0.2227   0.2410
   1.250   0.2458   0.01914   0.01027  -0.0239   0.2226   0.2428
   1.500   0.2685   0.01935   0.01049  -0.0231   0.2224   0.2443
   1.750   0.2911   0.01958   0.01072  -0.0224   0.2221   0.2457
   2.000   0.3140   0.01981   0.01095  -0.0218   0.2219   0.2469
   2.250   0.3366   0.02006   0.01121  -0.0211   0.2217   0.2480
   2.500   0.3585   0.02033   0.01148  -0.0204   0.2214   0.2498
   2.750   0.3805   0.02059   0.01176  -0.0196   0.2212   0.2542
   3.000   0.4031   0.02082   0.01204  -0.0190   0.2211   0.2588
   3.250   0.4258   0.02107   0.01232  -0.0184   0.2209   0.2634
   3.500   0.4481   0.02135   0.01264  -0.0178   0.2208   0.2682
   3.750   0.4704   0.02162   0.01295  -0.0172   0.2206   0.2784
   4.000   0.4928   0.02187   0.01328  -0.0167   0.2205   0.2931
   4.250   0.5142   0.02204   0.01365  -0.0161   0.2203   0.3410
   4.500   0.5348   0.02195   0.01405  -0.0154   0.2201   0.4716
   4.750   0.5552   0.02187   0.01451  -0.0147   0.2199   0.6156
   5.000   0.5769   0.02208   0.01496  -0.0141   0.2197   0.6762
   5.250   0.5985   0.02239   0.01542  -0.0135   0.2195   0.7145
   5.500   0.6195   0.02275   0.01592  -0.0128   0.2193   0.7479
   5.750   0.6405   0.02306   0.01644  -0.0120   0.2191   0.7929
   6.000   0.6586   0.02336   0.01710  -0.0104   0.2188   0.8792
   6.250   0.6761   0.02389   0.01775  -0.0087   0.2185   0.9167
   6.500   0.6944   0.02447   0.01836  -0.0074   0.2181   0.9341
   6.750   0.7131   0.02503   0.01894  -0.0062   0.2177   0.9466
   7.000   0.7324   0.02562   0.01954  -0.0052   0.2173   0.9545
   7.250   0.7501   0.02627   0.02021  -0.0040   0.2170   0.9632
   7.500   0.7681   0.02691   0.02085  -0.0028   0.2167   0.9705
   7.750   0.7909   0.02761   0.02156  -0.0027   0.2163   0.9765
   8.000   0.8142   0.02836   0.02230  -0.0029   0.2157   0.9813
   8.250   0.8362   0.02920   0.02314  -0.0029   0.2152   0.9858
   8.500   0.8591   0.03011   0.02403  -0.0032   0.2143   0.9886
   8.750   0.8885   0.03112   0.02502  -0.0050   0.2134   0.9898
   9.000   0.9182   0.03203   0.02592  -0.0068   0.2129   0.9908
   9.250   0.9471   0.03286   0.02677  -0.0084   0.2125   0.9917
   9.500   0.9751   0.03369   0.02761  -0.0098   0.2121   0.9927
   9.750   1.0023   0.03451   0.02843  -0.0111   0.2117   0.9937
  10.000   1.0310   0.03536   0.02930  -0.0127   0.2112   0.9949
  10.250   1.0587   0.03631   0.03025  -0.0142   0.2106   0.9962
  10.500   1.0843   0.03728   0.03124  -0.0154   0.2101   0.9973
  10.750   1.1094   0.03823   0.03219  -0.0164   0.2094   0.9984
  11.000   1.1347   0.03919   0.03315  -0.0175   0.2088   0.9993
  11.250   1.1586   0.04017   0.03412  -0.0184   0.2080   1.0000
  11.500   1.1671   0.04099   0.03494  -0.0163   0.2074   1.0000
  11.750   1.1757   0.04172   0.03568  -0.0141   0.2068   1.0000
  12.000   1.1853   0.04239   0.03634  -0.0121   0.2062   1.0000
  12.250   1.1962   0.04299   0.03691  -0.0102   0.2055   1.0000
  12.500   1.2058   0.04376   0.03773  -0.0084   0.2051   1.0000
  12.750   1.2156   0.04457   0.03858  -0.0067   0.2047   1.0000
  13.000   1.2272   0.04531   0.03936  -0.0052   0.2042   1.0000
  13.250   1.2396   0.04607   0.04014  -0.0040   0.2036   1.0000
  13.500   1.2510   0.04697   0.04107  -0.0027   0.2029   1.0000
  13.750   1.2631   0.04793   0.04205  -0.0017   0.2021   1.0000
  14.000   1.2771   0.04885   0.04299  -0.0009   0.2013   1.0000
  14.250   1.2916   0.04982   0.04395  -0.0004   0.2002   1.0000
  14.500   1.3066   0.05078   0.04492   0.0001   0.1994   1.0000
  14.750   1.3208   0.05183   0.04596   0.0006   0.1987   1.0000
  15.000   1.3346   0.05310   0.04728   0.0009   0.1979   1.0000
  15.250   1.3503   0.05426   0.04850   0.0009   0.1971   1.0000
  15.500   1.3663   0.05542   0.04971   0.0009   0.1958   1.0000
  15.750   1.3799   0.05680   0.05114   0.0010   0.1944   1.0000
  16.000   1.3943   0.05816   0.05253   0.0010   0.1926   1.0000
  16.250   1.4098   0.05928   0.05368   0.0011   0.1922   1.0000
  16.500   1.4270   0.06034   0.05479   0.0009   0.1907   1.0000
  16.750   1.4449   0.06132   0.05585   0.0006   0.1871   1.0000
  17.000   1.4605   0.06246   0.05706   0.0006   0.1814   1.0000
  17.250   1.4818   0.06354   0.05811  -0.0004   0.1764   1.0000
  17.500   1.4996   0.06464   0.05920  -0.0009   0.1747   1.0000
  17.750   1.5118   0.06623   0.06074  -0.0010   0.1722   1.0000
  18.000   1.5161   0.06848   0.06299  -0.0006   0.1711   1.0000
  18.250   1.5195   0.07076   0.06527  -0.0001   0.1696   1.0000
  18.500   1.5193   0.07341   0.06792   0.0005   0.1684   1.0000
  18.750   1.5199   0.07598   0.07052   0.0009   0.1671   1.0000
  19.000   1.5241   0.07819   0.07276   0.0012   0.1661   1.0000
  19.250   1.5206   0.08118   0.07579   0.0017   0.1647   1.0000
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