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CLARK YM-15 AIRFOIL (clarym15-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: CLARK YM-15 AIRFOIL (clarym15-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.13 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-clarym15-il-1000000-n5.txt
Download as CSV file: xf-clarym15-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: CLARK YM-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
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.8657   0.10974   0.10715  -0.0487   1.0000   0.0216
 -18.250  -0.9050   0.09907   0.09635  -0.0548   1.0000   0.0217
 -18.000  -0.9388   0.08978   0.08692  -0.0602   1.0000   0.0217
 -17.750  -0.9767   0.08034   0.07735  -0.0659   1.0000   0.0218
 -17.500  -1.0139   0.07130   0.06817  -0.0714   1.0000   0.0218
 -17.250  -1.0479   0.06269   0.05942  -0.0768   1.0000   0.0218
 -17.000  -1.0765   0.05458   0.05115  -0.0822   1.0000   0.0219
 -16.750  -1.0958   0.04753   0.04395  -0.0875   1.0000   0.0219
 -16.500  -1.1065   0.04185   0.03812  -0.0921   1.0000   0.0220
 -16.250  -1.1110   0.03751   0.03365  -0.0955   1.0000   0.0221
 -16.000  -1.1119   0.03423   0.03025  -0.0977   1.0000   0.0222
 -15.750  -1.1106   0.03175   0.02766  -0.0987   1.0000   0.0223
 -15.500  -1.1084   0.02980   0.02562  -0.0987   1.0000   0.0224
 -15.250  -1.1073   0.02828   0.02401  -0.0975   1.0000   0.0224
 -15.000  -1.1112   0.02711   0.02277  -0.0946   1.0000   0.0225
 -14.500  -1.0816   0.02420   0.01968  -0.0955   0.9926   0.0230
 -14.250  -1.0636   0.02323   0.01866  -0.0953   0.9870   0.0232
 -14.000  -1.0406   0.02236   0.01773  -0.0958   0.9833   0.0234
 -13.750  -1.0193   0.02159   0.01691  -0.0957   0.9784   0.0236
 -13.500  -0.9971   0.02088   0.01614  -0.0956   0.9731   0.0238
 -13.250  -0.9743   0.02022   0.01541  -0.0954   0.9682   0.0240
 -13.000  -0.9535   0.01963   0.01477  -0.0948   0.9616   0.0242
 -12.750  -0.9309   0.01908   0.01416  -0.0943   0.9558   0.0245
 -12.500  -0.9097   0.01856   0.01359  -0.0936   0.9489   0.0247
 -12.250  -0.8878   0.01804   0.01300  -0.0929   0.9422   0.0249
 -12.000  -0.8658   0.01753   0.01242  -0.0921   0.9353   0.0251
 -11.750  -0.8435   0.01705   0.01187  -0.0914   0.9278   0.0253
 -11.500  -0.8205   0.01659   0.01133  -0.0908   0.9209   0.0255
 -11.250  -0.7972   0.01615   0.01083  -0.0902   0.9129   0.0257
 -11.000  -0.7735   0.01574   0.01034  -0.0896   0.9055   0.0259
 -10.750  -0.7493   0.01535   0.00988  -0.0891   0.8972   0.0260
 -10.500  -0.7248   0.01499   0.00945  -0.0886   0.8892   0.0262
 -10.250  -0.6999   0.01464   0.00904  -0.0882   0.8807   0.0264
 -10.000  -0.6766   0.01414   0.00846  -0.0876   0.8722   0.0268
  -9.750  -0.6521   0.01372   0.00799  -0.0871   0.8631   0.0271
  -9.500  -0.6271   0.01337   0.00757  -0.0866   0.8546   0.0274
  -9.250  -0.6016   0.01305   0.00720  -0.0863   0.8455   0.0277
  -9.000  -0.5759   0.01276   0.00684  -0.0859   0.8372   0.0280
  -8.750  -0.5499   0.01248   0.00651  -0.0856   0.8289   0.0283
  -8.500  -0.5238   0.01222   0.00620  -0.0853   0.8213   0.0286
  -8.250  -0.4973   0.01197   0.00590  -0.0850   0.8137   0.0290
  -8.000  -0.4709   0.01174   0.00561  -0.0847   0.8061   0.0293
  -7.750  -0.4440   0.01150   0.00533  -0.0845   0.7994   0.0296
  -7.500  -0.4172   0.01129   0.00507  -0.0843   0.7922   0.0300
  -7.250  -0.3903   0.01109   0.00482  -0.0841   0.7855   0.0303
  -7.000  -0.3630   0.01090   0.00459  -0.0839   0.7783   0.0305
  -6.500  -0.3094   0.01046   0.00408  -0.0834   0.7628   0.0320
  -6.000  -0.2553   0.01012   0.00367  -0.0830   0.7443   0.0335
  -5.750  -0.2283   0.00999   0.00348  -0.0828   0.7356   0.0343
  -5.500  -0.2006   0.00985   0.00331  -0.0826   0.7272   0.0351
  -5.250  -0.1737   0.00971   0.00313  -0.0824   0.7181   0.0364
  -5.000  -0.1462   0.00956   0.00297  -0.0823   0.7094   0.0383
  -4.750  -0.1190   0.00945   0.00282  -0.0820   0.7009   0.0404
  -4.500  -0.0915   0.00929   0.00267  -0.0819   0.6924   0.0447
  -4.250  -0.0645   0.00916   0.00254  -0.0817   0.6833   0.0519
  -4.000  -0.0371   0.00903   0.00243  -0.0815   0.6740   0.0608
  -3.750  -0.0099   0.00894   0.00233  -0.0813   0.6635   0.0684
  -3.500   0.0173   0.00886   0.00224  -0.0811   0.6517   0.0752
  -3.250   0.0449   0.00879   0.00216  -0.0810   0.6419   0.0803
  -3.000   0.0721   0.00874   0.00208  -0.0808   0.6306   0.0859
  -2.750   0.0994   0.00870   0.00201  -0.0806   0.6177   0.0906
  -2.500   0.1268   0.00864   0.00195  -0.0804   0.6068   0.0974
  -2.250   0.1540   0.00860   0.00189  -0.0802   0.5956   0.1053
  -2.000   0.1809   0.00854   0.00183  -0.0800   0.5833   0.1185
  -1.750   0.2077   0.00843   0.00178  -0.0798   0.5720   0.1424
  -1.500   0.2342   0.00832   0.00175  -0.0795   0.5615   0.1770
  -1.250   0.2611   0.00824   0.00173  -0.0793   0.5505   0.2024
  -1.000   0.2883   0.00821   0.00172  -0.0791   0.5400   0.2215
  -0.750   0.3152   0.00821   0.00172  -0.0789   0.5288   0.2391
  -0.500   0.3424   0.00819   0.00172  -0.0787   0.5173   0.2594
  -0.250   0.3694   0.00819   0.00174  -0.0785   0.5057   0.2788
   0.000   0.3962   0.00823   0.00176  -0.0783   0.4922   0.2949
   0.250   0.4227   0.00827   0.00179  -0.0780   0.4767   0.3127
   0.500   0.4489   0.00830   0.00183  -0.0777   0.4600   0.3396
   0.750   0.4746   0.00828   0.00188  -0.0773   0.4425   0.3828
   1.000   0.4997   0.00827   0.00194  -0.0769   0.4227   0.4385
   1.250   0.5242   0.00824   0.00203  -0.0763   0.4008   0.5067
   1.500   0.5481   0.00820   0.00213  -0.0756   0.3807   0.5863
   1.750   0.5723   0.00817   0.00224  -0.0750   0.3648   0.6604
   2.000   0.5974   0.00818   0.00234  -0.0744   0.3530   0.7115
   2.250   0.6222   0.00821   0.00246  -0.0738   0.3429   0.7595
   2.500   0.6474   0.00821   0.00257  -0.0732   0.3349   0.8054
   2.750   0.6721   0.00828   0.00270  -0.0725   0.3270   0.8424
   3.000   0.6976   0.00832   0.00282  -0.0719   0.3222   0.8740
   3.250   0.7227   0.00839   0.00294  -0.0712   0.3175   0.9054
   3.500   0.7482   0.00850   0.00308  -0.0706   0.3130   0.9310
   3.750   0.7756   0.00863   0.00321  -0.0704   0.3086   0.9501
   4.000   0.8064   0.00876   0.00334  -0.0710   0.3051   0.9680
   4.250   0.8410   0.00893   0.00348  -0.0725   0.2998   0.9817
   4.500   0.8764   0.00916   0.00366  -0.0743   0.2919   0.9904
   5.000   0.9537   0.00957   0.00398  -0.0793   0.2773   1.0000
   5.250   0.9746   0.00969   0.00409  -0.0780   0.2729   1.0000
   5.500   0.9960   0.00981   0.00420  -0.0767   0.2690   1.0000
   5.750   1.0173   0.00995   0.00433  -0.0754   0.2649   1.0000
   6.000   1.0388   0.01012   0.00447  -0.0742   0.2611   1.0000
   6.250   1.0614   0.01027   0.00462  -0.0732   0.2578   1.0000
   6.500   1.0847   0.01041   0.00477  -0.0724   0.2539   1.0000
   6.750   1.1075   0.01059   0.00493  -0.0715   0.2484   1.0000
   7.000   1.1298   0.01081   0.00512  -0.0705   0.2430   1.0000
   7.250   1.1533   0.01097   0.00529  -0.0698   0.2387   1.0000
   7.500   1.1758   0.01119   0.00549  -0.0689   0.2321   1.0000
   7.750   1.1973   0.01143   0.00570  -0.0679   0.2248   1.0000
   8.000   1.2170   0.01173   0.00594  -0.0665   0.2145   1.0000
   8.250   1.2367   0.01202   0.00621  -0.0651   0.2043   1.0000
   8.500   1.2548   0.01241   0.00653  -0.0636   0.1915   1.0000
   8.750   1.2717   0.01287   0.00692  -0.0619   0.1772   1.0000
   9.000   1.2871   0.01343   0.00738  -0.0600   0.1613   1.0000
   9.250   1.3016   0.01406   0.00792  -0.0580   0.1455   1.0000
   9.500   1.3161   0.01470   0.00848  -0.0562   0.1313   1.0000
   9.750   1.3320   0.01528   0.00901  -0.0546   0.1206   1.0000
  10.000   1.3481   0.01587   0.00956  -0.0530   0.1120   1.0000
  10.500   1.3807   0.01704   0.01068  -0.0502   0.0991   1.0000
  10.750   1.3963   0.01768   0.01130  -0.0488   0.0940   1.0000
  11.000   1.4128   0.01828   0.01191  -0.0475   0.0897   1.0000
  11.250   1.4282   0.01896   0.01259  -0.0462   0.0854   1.0000
  11.500   1.4427   0.01971   0.01333  -0.0448   0.0813   1.0000
  11.750   1.4589   0.02037   0.01401  -0.0437   0.0788   1.0000
  12.000   1.4737   0.02112   0.01478  -0.0425   0.0759   1.0000
  12.250   1.4872   0.02199   0.01565  -0.0412   0.0728   1.0000
  12.500   1.5015   0.02282   0.01650  -0.0400   0.0705   1.0000
  12.750   1.5157   0.02366   0.01737  -0.0389   0.0681   1.0000
  13.000   1.5282   0.02465   0.01838  -0.0377   0.0653   1.0000
  13.250   1.5392   0.02577   0.01950  -0.0365   0.0626   1.0000
  13.500   1.5521   0.02676   0.02054  -0.0355   0.0607   1.0000
  13.750   1.5630   0.02793   0.02173  -0.0344   0.0578   1.0000
  14.000   1.5708   0.02937   0.02316  -0.0331   0.0542   1.0000
  14.250   1.5791   0.03080   0.02462  -0.0320   0.0503   1.0000
  14.500   1.5844   0.03250   0.02633  -0.0308   0.0461   1.0000
  14.750   1.5875   0.03446   0.02828  -0.0296   0.0411   1.0000
  15.000   1.5874   0.03677   0.03059  -0.0285   0.0345   1.0000
  15.250   1.5710   0.04070   0.03447  -0.0268   0.0213   1.0000
  15.500   1.5640   0.04393   0.03774  -0.0259   0.0169   1.0000
  15.750   1.5638   0.04661   0.04047  -0.0253   0.0154   1.0000
  16.000   1.5624   0.04946   0.04339  -0.0249   0.0143   1.0000
  16.250   1.5627   0.05221   0.04621  -0.0246   0.0136   1.0000
  16.500   1.5621   0.05514   0.04922  -0.0245   0.0131   1.0000
  16.750   1.5600   0.05831   0.05246  -0.0245   0.0126   1.0000
  17.000   1.5567   0.06168   0.05591  -0.0246   0.0122   1.0000
  17.250   1.5520   0.06527   0.05958  -0.0248   0.0118   1.0000
  17.500   1.5482   0.06883   0.06323  -0.0252   0.0116   1.0000
  17.750   1.5440   0.07250   0.06699  -0.0257   0.0113   1.0000
  18.000   1.5384   0.07640   0.07098  -0.0262   0.0111   1.0000
  18.250   1.5314   0.08052   0.07519  -0.0270   0.0108   1.0000
  18.500   1.5233   0.08487   0.07963  -0.0278   0.0106   1.0000
  18.750   1.5144   0.08940   0.08425  -0.0289   0.0104   1.0000
  19.000   1.5045   0.09412   0.08907  -0.0300   0.0102   1.0000
  19.250   1.4936   0.09902   0.09407  -0.0313   0.0100   1.0000
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