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HAM-STD HS1-708 AIRFOIL (hs1708-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HAM-STD HS1-708 AIRFOIL (hs1708-il)
Reynolds number: 1,000,000
Max Cl/Cd: 116.99 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hs1708-il-1000000-n5.txt
Download as CSV file: xf-hs1708-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HAM-STD HS1-708 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
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.4592   0.05794   0.05561  -0.0842   0.8830   0.0049
  -9.750  -0.4557   0.03122   0.02811  -0.1212   0.8691   0.0047
  -9.500  -0.4337   0.02123   0.01751  -0.1294   0.8629   0.0047
  -9.250  -0.4076   0.01872   0.01471  -0.1311   0.8578   0.0047
  -9.000  -0.3804   0.01714   0.01291  -0.1322   0.8531   0.0048
  -8.750  -0.3529   0.01593   0.01152  -0.1330   0.8484   0.0048
  -8.500  -0.3252   0.01494   0.01034  -0.1337   0.8443   0.0049
  -8.250  -0.2971   0.01409   0.00934  -0.1342   0.8409   0.0049
  -8.000  -0.2687   0.01336   0.00848  -0.1347   0.8374   0.0050
  -7.750  -0.2403   0.01271   0.00769  -0.1352   0.8341   0.0051
  -7.500  -0.2118   0.01215   0.00700  -0.1356   0.8310   0.0052
  -7.250  -0.1831   0.01165   0.00638  -0.1359   0.8282   0.0053
  -7.000  -0.1543   0.01120   0.00584  -0.1363   0.8254   0.0054
  -6.750  -0.1254   0.01079   0.00534  -0.1366   0.8225   0.0056
  -6.500  -0.0965   0.01043   0.00489  -0.1369   0.8195   0.0058
  -6.250  -0.0676   0.01011   0.00449  -0.1372   0.8169   0.0060
  -6.000  -0.0386   0.00980   0.00410  -0.1375   0.8145   0.0064
  -5.750  -0.0095   0.00951   0.00376  -0.1378   0.8124   0.0069
  -5.500   0.0196   0.00926   0.00347  -0.1381   0.8100   0.0077
  -5.250   0.0487   0.00904   0.00320  -0.1383   0.8076   0.0087
  -5.000   0.0778   0.00879   0.00293  -0.1386   0.8051   0.0110
  -4.750   0.1069   0.00852   0.00267  -0.1389   0.8027   0.0177
  -4.500   0.1359   0.00834   0.00249  -0.1391   0.8004   0.0224
  -4.250   0.1650   0.00820   0.00233  -0.1394   0.7985   0.0260
  -4.000   0.1942   0.00803   0.00219  -0.1397   0.7961   0.0309
  -3.750   0.2233   0.00789   0.00206  -0.1399   0.7929   0.0368
  -3.500   0.2521   0.00778   0.00195  -0.1401   0.7884   0.0434
  -3.250   0.2809   0.00767   0.00184  -0.1403   0.7835   0.0492
  -3.000   0.3099   0.00758   0.00174  -0.1405   0.7783   0.0535
  -2.750   0.3388   0.00751   0.00165  -0.1406   0.7737   0.0578
  -2.500   0.3677   0.00743   0.00158  -0.1408   0.7696   0.0646
  -2.250   0.3967   0.00732   0.00152  -0.1410   0.7650   0.0752
  -2.000   0.4256   0.00725   0.00145  -0.1412   0.7598   0.0835
  -1.750   0.4544   0.00720   0.00140  -0.1414   0.7549   0.0921
  -1.500   0.4834   0.00713   0.00136  -0.1416   0.7495   0.1016
  -1.250   0.5121   0.00709   0.00133  -0.1417   0.7433   0.1123
  -1.000   0.5410   0.00705   0.00131  -0.1419   0.7386   0.1222
  -0.750   0.5699   0.00701   0.00130  -0.1421   0.7335   0.1318
  -0.500   0.5986   0.00700   0.00129  -0.1422   0.7278   0.1395
  -0.250   0.6274   0.00698   0.00130  -0.1424   0.7215   0.1492
   0.000   0.6558   0.00698   0.00130  -0.1425   0.7128   0.1586
   0.250   0.6844   0.00699   0.00131  -0.1426   0.7031   0.1657
   0.500   0.7128   0.00700   0.00133  -0.1427   0.6929   0.1754
   0.750   0.7410   0.00703   0.00135  -0.1427   0.6795   0.1827
   1.000   0.7685   0.00712   0.00139  -0.1426   0.6557   0.1924
   1.250   0.7943   0.00737   0.00147  -0.1422   0.6102   0.2020
   1.500   0.8194   0.00773   0.00162  -0.1417   0.5604   0.2111
   1.750   0.8450   0.00804   0.00180  -0.1414   0.5214   0.2223
   2.000   0.8711   0.00830   0.00195  -0.1411   0.4881   0.2351
   2.250   0.8971   0.00855   0.00211  -0.1408   0.4556   0.2491
   2.750   0.9487   0.00903   0.00249  -0.1403   0.3914   0.3262
   3.250   0.9932   0.00849   0.00302  -0.1385   0.3285   1.0000
   3.500   1.0191   0.00877   0.00320  -0.1382   0.3081   1.0000
   3.750   1.0447   0.00907   0.00339  -0.1379   0.2880   1.0000
   4.000   1.0701   0.00936   0.00358  -0.1375   0.2653   1.0000
   4.250   1.0951   0.00970   0.00380  -0.1370   0.2418   1.0000
   4.500   1.1194   0.01009   0.00405  -0.1365   0.2148   1.0000
   4.750   1.1439   0.01045   0.00430  -0.1360   0.1922   1.0000
   5.000   1.1675   0.01087   0.00460  -0.1353   0.1670   1.0000
   5.250   1.1906   0.01134   0.00493  -0.1345   0.1413   1.0000
   5.500   1.2126   0.01190   0.00532  -0.1336   0.1107   1.0000
   5.750   1.2336   0.01254   0.00578  -0.1325   0.0788   1.0000
   6.000   1.2560   0.01302   0.00617  -0.1316   0.0621   1.0000
   6.250   1.2794   0.01340   0.00651  -0.1309   0.0539   1.0000
   6.500   1.3025   0.01379   0.00686  -0.1301   0.0472   1.0000
   6.750   1.3260   0.01413   0.00720  -0.1294   0.0427   1.0000
   7.000   1.3487   0.01451   0.00757  -0.1286   0.0384   1.0000
   7.250   1.3713   0.01489   0.00794  -0.1277   0.0348   1.0000
   7.500   1.3942   0.01522   0.00829  -0.1269   0.0333   1.0000
   7.750   1.4164   0.01559   0.00867  -0.1260   0.0313   1.0000
   8.000   1.4377   0.01601   0.00911  -0.1249   0.0291   1.0000
   8.250   1.4582   0.01648   0.00958  -0.1237   0.0264   1.0000
   8.500   1.4792   0.01685   0.00998  -0.1226   0.0256   1.0000
   8.750   1.4996   0.01724   0.01042  -0.1214   0.0247   1.0000
   9.000   1.5191   0.01767   0.01088  -0.1200   0.0237   1.0000
   9.250   1.5375   0.01814   0.01138  -0.1185   0.0225   1.0000
   9.500   1.5537   0.01865   0.01191  -0.1165   0.0213   1.0000
   9.750   1.5684   0.01925   0.01253  -0.1143   0.0197   1.0000
  10.000   1.5843   0.01979   0.01311  -0.1124   0.0188   1.0000
  10.250   1.6010   0.02028   0.01365  -0.1107   0.0179   1.0000
  10.500   1.6167   0.02086   0.01426  -0.1089   0.0169   1.0000
  10.750   1.6316   0.02150   0.01493  -0.1070   0.0158   1.0000
  11.000   1.6456   0.02222   0.01569  -0.1050   0.0149   1.0000
  11.250   1.6587   0.02302   0.01653  -0.1030   0.0139   1.0000
  11.500   1.6726   0.02377   0.01734  -0.1012   0.0134   1.0000
  11.750   1.6863   0.02454   0.01817  -0.0994   0.0128   1.0000
  12.000   1.6993   0.02538   0.01906  -0.0976   0.0121   1.0000
  12.250   1.7114   0.02630   0.02002  -0.0957   0.0113   1.0000
  12.500   1.7224   0.02732   0.02108  -0.0938   0.0104   1.0000
  12.750   1.7324   0.02845   0.02226  -0.0918   0.0096   1.0000
  13.000   1.7431   0.02954   0.02343  -0.0900   0.0092   1.0000
  13.250   1.7530   0.03070   0.02467  -0.0882   0.0087   1.0000
  13.500   1.7619   0.03197   0.02600  -0.0864   0.0081   1.0000
  13.750   1.7697   0.03337   0.02746  -0.0846   0.0075   1.0000
  14.000   1.7761   0.03491   0.02905  -0.0828   0.0068   1.0000
  14.250   1.7823   0.03649   0.03071  -0.0810   0.0063   1.0000
  14.500   1.7878   0.03816   0.03246  -0.0793   0.0058   1.0000
  14.750   1.7918   0.04002   0.03439  -0.0776   0.0052   1.0000
  15.000   1.7938   0.04211   0.03655  -0.0758   0.0046   1.0000
  15.250   1.7950   0.04429   0.03884  -0.0742   0.0042   1.0000
  15.500   1.7961   0.04658   0.04122  -0.0727   0.0039   1.0000
  15.750   1.7962   0.04907   0.04380  -0.0714   0.0036   1.0000
  16.000   1.7948   0.05181   0.04663  -0.0702   0.0033   1.0000
  16.250   1.7917   0.05481   0.04974  -0.0691   0.0031   1.0000
  16.500   1.7875   0.05809   0.05312  -0.0683   0.0028   1.0000
  16.750   1.7828   0.06157   0.05671  -0.0677   0.0027   1.0000
  17.000   1.7783   0.06517   0.06044  -0.0674   0.0026   1.0000
  17.250   1.7725   0.06909   0.06448  -0.0674   0.0025   1.0000
  17.500   1.7648   0.07339   0.06890  -0.0677   0.0024   1.0000
  17.750   1.7560   0.07805   0.07369  -0.0683   0.0023   1.0000
  18.000   1.7456   0.08311   0.07887  -0.0693   0.0023   1.0000
  18.250   1.7337   0.08857   0.08447  -0.0706   0.0022   1.0000
  18.500   1.7197   0.09445   0.09049  -0.0723   0.0022   1.0000
  18.750   1.7045   0.10068   0.09686  -0.0743   0.0021   1.0000
  19.000   1.6878   0.10732   0.10364  -0.0768   0.0021   1.0000
  19.250   1.6702   0.11429   0.11074  -0.0796   0.0020   1.0000
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