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TH 25816 HALE AIRFOIL (th25816-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: TH 25816 HALE AIRFOIL (th25816-il)
Reynolds number: 1,000,000
Max Cl/Cd: 74.91 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-th25816-il-1000000.txt
Download as CSV file: xf-th25816-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: TH 25816 HALE 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  -0.3244   0.07344   0.06986  -0.2284   0.9506   0.0143
 -19.500  -0.3981   0.07341   0.06977  -0.2121   0.9428   0.0141
 -19.250  -0.4029   0.07017   0.06645  -0.2132   0.9419   0.0142
 -19.000  -0.4045   0.06691   0.06310  -0.2149   0.9412   0.0143
 -18.750  -0.4103   0.06304   0.05907  -0.2166   0.9407   0.0143
 -18.500  -0.4057   0.06016   0.05610  -0.2186   0.9404   0.0144
 -18.250  -0.4033   0.05715   0.05297  -0.2203   0.9400   0.0144
 -18.000  -0.3909   0.05498   0.05076  -0.2227   0.9396   0.0146
 -17.750  -0.3851   0.05223   0.04787  -0.2244   0.9393   0.0145
 -17.500  -0.3754   0.04983   0.04537  -0.2261   0.9391   0.0146
 -17.250  -0.3604   0.04794   0.04341  -0.2283   0.9388   0.0147
 -17.000  -0.3464   0.04600   0.04139  -0.2301   0.9386   0.0148
 -16.750  -0.3315   0.04424   0.03955  -0.2317   0.9383   0.0149
 -16.500  -0.3153   0.04260   0.03784  -0.2334   0.9379   0.0152
 -16.250  -0.2979   0.04100   0.03616  -0.2351   0.9376   0.0153
 -16.000  -0.2781   0.03956   0.03466  -0.2370   0.9372   0.0155
 -15.750  -0.2590   0.03818   0.03321  -0.2386   0.9368   0.0157
 -15.500  -0.2859   0.03801   0.03301  -0.2294   0.9312   0.0157
 -15.250  -0.2771   0.03692   0.03187  -0.2285   0.9292   0.0160
 -15.000  -0.2579   0.03585   0.03075  -0.2293   0.9283   0.0159
 -14.750  -0.2388   0.03468   0.02952  -0.2305   0.9275   0.0161
 -14.500  -0.2168   0.03356   0.02834  -0.2319   0.9268   0.0163
 -14.250  -0.1948   0.03243   0.02714  -0.2336   0.9261   0.0165
 -14.000  -0.1709   0.03139   0.02606  -0.2353   0.9255   0.0166
 -13.750  -0.1491   0.03030   0.02494  -0.2362   0.9249   0.0169
 -13.500  -0.1263   0.02921   0.02382  -0.2377   0.9242   0.0170
 -13.250  -0.1039   0.02813   0.02271  -0.2393   0.9235   0.0172
 -13.000  -0.0812   0.02714   0.02171  -0.2409   0.9225   0.0177
 -12.750  -0.1056   0.02679   0.02135  -0.2316   0.9159   0.0177
 -12.500  -0.0877   0.02589   0.02043  -0.2318   0.9141   0.0179
 -12.250  -0.0660   0.02492   0.01942  -0.2328   0.9126   0.0182
 -12.000  -0.0429   0.02398   0.01845  -0.2341   0.9112   0.0186
 -11.750  -0.0191   0.02312   0.01754  -0.2355   0.9098   0.0188
 -11.500  -0.0397   0.02276   0.01717  -0.2268   0.9017   0.0190
 -11.250  -0.0220   0.02203   0.01640  -0.2266   0.8985   0.0193
 -11.000  -0.0351   0.02159   0.01593  -0.2195   0.8891   0.0194
 -10.750  -0.0126   0.02086   0.01515  -0.2202   0.8844   0.0197
 -10.500  -0.0165   0.02037   0.01459  -0.2151   0.8728   0.0199
 -10.250   0.0025   0.01982   0.01398  -0.2149   0.8643   0.0201
 -10.000   0.0180   0.01896   0.01300  -0.2146   0.8550   0.0207
  -9.750   0.0253   0.01851   0.01246  -0.2118   0.8438   0.0211
  -9.500   0.0304   0.01816   0.01204  -0.2085   0.8340   0.0216
  -9.000   0.0398   0.01758   0.01132  -0.2016   0.8183   0.0224
  -8.750   0.0486   0.01728   0.01096  -0.1990   0.8120   0.0230
  -8.500   0.0521   0.01705   0.01069  -0.1951   0.8066   0.0235
  -8.000   0.0623   0.01651   0.01005  -0.1881   0.7966   0.0247
  -7.750   0.0696   0.01621   0.00973  -0.1852   0.7923   0.0258
  -7.500   0.0641   0.01601   0.00952  -0.1793   0.7877   0.0271
  -7.250   0.0698   0.01581   0.00929  -0.1758   0.7836   0.0279
  -7.000   0.0797   0.01552   0.00897  -0.1733   0.7799   0.0306
  -6.750   0.0854   0.01509   0.00860  -0.1702   0.7763   0.0458
  -6.500   0.0722   0.01475   0.00836  -0.1630   0.7727   0.0655
  -6.250   0.0574   0.01424   0.00800  -0.1557   0.7689   0.1012
  -6.000   0.0519   0.01379   0.00765  -0.1502   0.7652   0.1324
  -5.750   0.0473   0.01305   0.00711  -0.1454   0.7612   0.1909
  -5.500   0.0285   0.01268   0.00686  -0.1369   0.7580   0.2186
  -5.250   0.0041   0.01222   0.00654  -0.1274   0.7543   0.2565
  -5.000  -0.0147   0.01179   0.00622  -0.1189   0.7509   0.2883
  -4.750  -0.0394   0.01121   0.00577  -0.1093   0.7472   0.3314
  -4.500  -0.0581   0.01068   0.00533  -0.1007   0.7436   0.3677
  -4.250  -0.0870   0.00999   0.00492  -0.0901   0.7406   0.4328
  -4.000  -0.0957   0.00921   0.00451  -0.0836   0.7375   0.5215
  -3.750  -0.0837   0.00880   0.00432  -0.0811   0.7349   0.5836
  -3.500  -0.0614   0.00867   0.00425  -0.0806   0.7326   0.6122
  -3.250  -0.0340   0.00861   0.00418  -0.0811   0.7306   0.6308
  -3.000  -0.0016   0.00855   0.00412  -0.0826   0.7284   0.6451
  -2.750   0.0246   0.00854   0.00413  -0.0828   0.7264   0.6603
  -2.500   0.0426   0.00859   0.00423  -0.0812   0.7245   0.6765
  -2.250   0.0634   0.00865   0.00431  -0.0802   0.7223   0.6904
  -2.000   0.0869   0.00871   0.00436  -0.0798   0.7201   0.6969
  -1.750   0.1112   0.00875   0.00436  -0.0796   0.7178   0.7006
  -1.500   0.1366   0.00877   0.00436  -0.0796   0.7157   0.7053
  -1.250   0.1661   0.00878   0.00436  -0.0805   0.7136   0.7090
  -1.000   0.2005   0.00880   0.00433  -0.0824   0.7115   0.7132
  -0.750   0.2270   0.00885   0.00436  -0.0827   0.7096   0.7161
  -0.500   0.2445   0.00895   0.00445  -0.0812   0.7076   0.7186
  -0.250   0.2652   0.00901   0.00451  -0.0802   0.7055   0.7216
   0.000   0.2877   0.00905   0.00458  -0.0797   0.7031   0.7245
   0.250   0.3117   0.00910   0.00462  -0.0795   0.7009   0.7274
   0.500   0.3376   0.00915   0.00465  -0.0797   0.6988   0.7301
   0.750   0.3671   0.00918   0.00465  -0.0807   0.6968   0.7328
   1.000   0.4017   0.00920   0.00462  -0.0827   0.6948   0.7352
   1.250   0.4267   0.00927   0.00469  -0.0827   0.6929   0.7379
   1.500   0.4440   0.00937   0.00484  -0.0812   0.6908   0.7414
   1.750   0.4639   0.00947   0.00497  -0.0801   0.6884   0.7445
   2.000   0.4864   0.00956   0.00506  -0.0796   0.6861   0.7476
   2.250   0.5096   0.00965   0.00514  -0.0793   0.6839   0.7506
   2.500   0.5352   0.00973   0.00519  -0.0795   0.6820   0.7534
   2.750   0.5649   0.00975   0.00521  -0.0805   0.6798   0.7563
   3.000   0.6018   0.00975   0.00520  -0.0831   0.6776   0.7591
   3.250   0.6154   0.00994   0.00544  -0.0808   0.6754   0.7627
   3.500   0.6316   0.01011   0.00564  -0.0791   0.6729   0.7664
   3.750   0.6523   0.01025   0.00578  -0.0783   0.6704   0.7698
   4.000   0.6741   0.01036   0.00590  -0.0777   0.6678   0.7730
   4.250   0.6975   0.01045   0.00602  -0.0774   0.6654   0.7762
   4.500   0.7269   0.01050   0.00607  -0.0784   0.6628   0.7791
   4.750   0.7558   0.01059   0.00614  -0.0793   0.6602   0.7822
   5.000   0.7640   0.01089   0.00649  -0.0761   0.6571   0.7861
   5.250   0.7801   0.01110   0.00673  -0.0744   0.6538   0.7895
   5.500   0.7984   0.01128   0.00694  -0.0732   0.6506   0.7930
   5.750   0.8227   0.01140   0.00706  -0.0731   0.6475   0.7960
   6.000   0.8555   0.01142   0.00706  -0.0748   0.6442   0.7988
   6.250   0.8617   0.01183   0.00752  -0.0713   0.6410   0.8026
   6.500   0.8749   0.01215   0.00787  -0.0692   0.6371   0.8056
   6.750   0.8914   0.01239   0.00814  -0.0676   0.6329   0.8089
   7.000   0.9171   0.01249   0.00823  -0.0679   0.6292   0.8115
   7.250   0.9302   0.01286   0.00865  -0.0658   0.6252   0.8147
   7.500   0.9401   0.01331   0.00915  -0.0631   0.6206   0.8182
   7.750   0.9568   0.01363   0.00946  -0.0618   0.6161   0.8212
   8.000   0.9819   0.01375   0.00954  -0.0620   0.6114   0.8234
   8.250   0.9842   0.01442   0.01030  -0.0580   0.6060   0.8268
   8.500   0.9965   0.01488   0.01079  -0.0559   0.6000   0.8293
   8.750   1.0084   0.01536   0.01127  -0.0537   0.5931   0.8320
   9.000   1.0188   0.01595   0.01190  -0.0514   0.5871   0.8349
   9.250   1.0316   0.01645   0.01239  -0.0495   0.5802   0.8377
   9.500   1.0392   0.01718   0.01314  -0.0468   0.5719   0.8401
   9.750   1.0474   0.01784   0.01378  -0.0442   0.5628   0.8429
  10.000   1.0567   0.01854   0.01453  -0.0419   0.5550   0.8452
  10.250   1.0648   0.01928   0.01527  -0.0394   0.5461   0.8475
  10.500   1.0714   0.02014   0.01615  -0.0367   0.5353   0.8499
  10.750   1.0757   0.02110   0.01709  -0.0338   0.5229   0.8525
  11.000   1.0770   0.02223   0.01819  -0.0304   0.5101   0.8550
  11.250   1.0777   0.02344   0.01935  -0.0271   0.4945   0.8571
  11.500   1.0740   0.02484   0.02070  -0.0232   0.4773   0.8594
  11.750   1.0686   0.02636   0.02218  -0.0192   0.4578   0.8616
  12.000   1.0663   0.02779   0.02357  -0.0157   0.4403   0.8636
  12.250   1.0626   0.02937   0.02509  -0.0122   0.4231   0.8655
  12.500   1.0616   0.03086   0.02653  -0.0091   0.4054   0.8676
  12.750   1.0589   0.03249   0.02812  -0.0060   0.3883   0.8697
  13.000   1.0587   0.03403   0.02960  -0.0033   0.3708   0.8716
  13.250   1.0557   0.03580   0.03129  -0.0004   0.3516   0.8733
  13.500   1.0579   0.03730   0.03274   0.0017   0.3358   0.8745
  13.750   1.0571   0.03897   0.03435   0.0042   0.3184   0.8763
  14.000   1.0584   0.04054   0.03586   0.0063   0.3009   0.8780
  14.250   1.0578   0.04228   0.03755   0.0086   0.2838   0.8795
  14.500   1.0607   0.04382   0.03904   0.0104   0.2676   0.8811
  14.750   1.0606   0.04563   0.04078   0.0124   0.2502   0.8826
  15.000   1.0642   0.04721   0.04231   0.0139   0.2350   0.8841
  15.250   1.0665   0.04894   0.04397   0.0155   0.2186   0.8856
  15.500   1.0694   0.05066   0.04563   0.0169   0.2043   0.8870
  15.750   1.0742   0.05227   0.04719   0.0180   0.1906   0.8883
  16.000   1.0766   0.05410   0.04896   0.0193   0.1764   0.8895
  16.250   1.0818   0.05575   0.05056   0.0202   0.1644   0.8905
  16.500   1.0894   0.05718   0.05198   0.0210   0.1544   0.8920
  16.750   1.0926   0.05900   0.05376   0.0220   0.1435   0.8934
  17.000   1.0959   0.06080   0.05552   0.0230   0.1320   0.8947
  17.250   1.1039   0.06228   0.05700   0.0236   0.1247   0.8960
  17.500   1.1084   0.06409   0.05880   0.0243   0.1172   0.8973
  17.750   1.1145   0.06576   0.06046   0.0249   0.1099   0.8987
  18.000   1.1218   0.06737   0.06207   0.0253   0.1041   0.9000
  18.250   1.1276   0.06917   0.06388   0.0257   0.0988   0.9013
  18.500   1.1328   0.07102   0.06572   0.0261   0.0928   0.9025
  18.750   1.1415   0.07258   0.06731   0.0262   0.0885   0.9036
  19.000   1.1451   0.07468   0.06939   0.0265   0.0835   0.9046
  19.250   1.1532   0.07636   0.07111   0.0265   0.0807   0.9054
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