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NASA SC(2)-0614 AIRFOIL (sc20614-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NASA SC(2)-0614 AIRFOIL (sc20614-il)
Reynolds number: 1,000,000
Max Cl/Cd: 77.63 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sc20614-il-1000000.txt
Download as CSV file: xf-sc20614-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0614 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  -1.2076   0.08816   0.08456  -0.0487   1.0000   0.0236
 -19.500  -1.2189   0.08264   0.07893  -0.0516   1.0000   0.0237
 -19.250  -1.2285   0.07753   0.07371  -0.0542   1.0000   0.0238
 -19.000  -1.2358   0.07282   0.06889  -0.0566   1.0000   0.0239
 -18.750  -1.2407   0.06858   0.06454  -0.0586   1.0000   0.0240
 -18.500  -1.2438   0.06471   0.06057  -0.0604   1.0000   0.0241
 -18.250  -1.2448   0.06120   0.05696  -0.0620   1.0000   0.0242
 -18.000  -1.2437   0.05804   0.05372  -0.0633   1.0000   0.0243
 -17.750  -1.2535   0.05385   0.04941  -0.0646   1.0000   0.0246
 -17.500  -1.2575   0.05041   0.04590  -0.0656   1.0000   0.0249
 -17.250  -1.2576   0.04750   0.04293  -0.0664   1.0000   0.0251
 -17.000  -1.2551   0.04497   0.04033  -0.0670   1.0000   0.0254
 -16.750  -1.2508   0.04267   0.03798  -0.0675   1.0000   0.0256
 -16.500  -1.2449   0.04064   0.03589  -0.0678   1.0000   0.0258
 -16.250  -1.2382   0.03875   0.03394  -0.0679   1.0000   0.0260
 -16.000  -1.2309   0.03697   0.03211  -0.0680   1.0000   0.0263
 -15.750  -1.2227   0.03537   0.03045  -0.0679   1.0000   0.0266
 -15.500  -1.2142   0.03384   0.02886  -0.0677   1.0000   0.0268
 -15.250  -1.2049   0.03242   0.02739  -0.0674   1.0000   0.0271
 -15.000  -1.1951   0.03110   0.02601  -0.0670   1.0000   0.0274
 -14.750  -1.1849   0.02987   0.02472  -0.0665   1.0000   0.0277
 -14.500  -1.1744   0.02876   0.02356  -0.0657   1.0000   0.0279
 -14.250  -1.1644   0.02774   0.02249  -0.0647   1.0000   0.0281
 -14.000  -1.1601   0.02654   0.02124  -0.0630   1.0000   0.0284
 -13.750  -1.1614   0.02528   0.01994  -0.0604   1.0000   0.0288
 -13.500  -1.1659   0.02431   0.01896  -0.0568   1.0000   0.0292
 -13.250  -1.1810   0.02358   0.01820  -0.0509   1.0000   0.0294
 -13.000  -1.1858   0.02280   0.01740  -0.0469   1.0000   0.0296
 -12.750  -1.1615   0.02193   0.01651  -0.0481   0.9990   0.0302
 -12.500  -1.1316   0.02114   0.01570  -0.0502   0.9976   0.0310
 -12.250  -1.1011   0.02041   0.01493  -0.0523   0.9962   0.0317
 -12.000  -1.0696   0.01973   0.01421  -0.0545   0.9949   0.0323
 -11.750  -1.0377   0.01884   0.01329  -0.0570   0.9938   0.0331
 -11.500  -1.0050   0.01801   0.01246  -0.0597   0.9930   0.0342
 -11.250  -0.9740   0.01740   0.01184  -0.0615   0.9913   0.0352
 -11.000  -0.9426   0.01685   0.01128  -0.0633   0.9894   0.0363
 -10.750  -0.9098   0.01638   0.01078  -0.0653   0.9878   0.0372
 -10.500  -0.8763   0.01564   0.01006  -0.0678   0.9863   0.0391
 -10.250  -0.8420   0.01519   0.00961  -0.0700   0.9852   0.0408
 -10.000  -0.8072   0.01483   0.00923  -0.0721   0.9843   0.0424
  -9.750  -0.7717   0.01422   0.00865  -0.0747   0.9834   0.0447
  -9.500  -0.7362   0.01384   0.00827  -0.0770   0.9827   0.0469
  -9.250  -0.7005   0.01353   0.00794  -0.0791   0.9821   0.0485
  -9.000  -0.6642   0.01298   0.00743  -0.0818   0.9816   0.0515
  -8.750  -0.6283   0.01265   0.00710  -0.0840   0.9810   0.0538
  -8.500  -0.5964   0.01233   0.00677  -0.0853   0.9787   0.0558
  -8.250  -0.5642   0.01193   0.00641  -0.0868   0.9760   0.0588
  -8.000  -0.5307   0.01166   0.00614  -0.0883   0.9740   0.0612
  -7.750  -0.4966   0.01134   0.00582  -0.0901   0.9722   0.0637
  -7.500  -0.4623   0.01100   0.00551  -0.0919   0.9705   0.0669
  -7.250  -0.4286   0.01075   0.00526  -0.0934   0.9687   0.0696
  -7.000  -0.3958   0.01046   0.00499  -0.0947   0.9663   0.0730
  -6.750  -0.3650   0.01017   0.00474  -0.0957   0.9623   0.0772
  -6.500  -0.3332   0.00993   0.00450  -0.0967   0.9590   0.0815
  -6.250  -0.3008   0.00963   0.00426  -0.0980   0.9561   0.0881
  -6.000  -0.2680   0.00936   0.00403  -0.0993   0.9534   0.0970
  -5.750  -0.2364   0.00909   0.00383  -0.1003   0.9495   0.1092
  -5.500  -0.2041   0.00879   0.00362  -0.1016   0.9454   0.1284
  -5.250  -0.1711   0.00845   0.00340  -0.1030   0.9418   0.1540
  -5.000  -0.1370   0.00807   0.00318  -0.1048   0.9385   0.1911
  -4.750  -0.1024   0.00766   0.00297  -0.1067   0.9347   0.2398
  -4.500  -0.0661   0.00714   0.00273  -0.1091   0.9307   0.3094
  -4.000   0.0107   0.00594   0.00223  -0.1150   0.9238   0.5067
  -3.750   0.0431   0.00582   0.00222  -0.1160   0.9193   0.5432
  -3.500   0.0738   0.00579   0.00221  -0.1164   0.9136   0.5632
  -3.250   0.1039   0.00579   0.00219  -0.1167   0.9072   0.5769
  -3.000   0.1341   0.00578   0.00219  -0.1170   0.9000   0.5855
  -2.750   0.1638   0.00580   0.00216  -0.1171   0.8918   0.5933
  -2.500   0.1934   0.00580   0.00215  -0.1172   0.8812   0.6001
  -2.250   0.2229   0.00585   0.00216  -0.1173   0.8713   0.6074
  -2.000   0.2531   0.00588   0.00216  -0.1175   0.8620   0.6135
  -1.750   0.2825   0.00590   0.00218  -0.1176   0.8509   0.6188
  -1.500   0.3117   0.00597   0.00218  -0.1176   0.8357   0.6234
  -1.250   0.3411   0.00607   0.00220  -0.1176   0.8194   0.6287
  -1.000   0.3705   0.00611   0.00224  -0.1177   0.8047   0.6341
  -0.750   0.3998   0.00619   0.00230  -0.1177   0.7886   0.6384
  -0.500   0.4290   0.00631   0.00234  -0.1177   0.7703   0.6426
  -0.250   0.4580   0.00646   0.00239  -0.1177   0.7480   0.6465
   0.000   0.4862   0.00659   0.00244  -0.1175   0.7150   0.6497
   0.250   0.5131   0.00688   0.00252  -0.1172   0.6561   0.6520
   0.500   0.5357   0.00771   0.00276  -0.1161   0.5200   0.6542
   0.750   0.5602   0.00840   0.00301  -0.1155   0.4176   0.6565
   1.000   0.5858   0.00899   0.00322  -0.1152   0.3343   0.6584
   1.250   0.6117   0.00953   0.00342  -0.1149   0.2603   0.6599
   1.500   0.6386   0.00996   0.00361  -0.1147   0.2108   0.6613
   1.750   0.6659   0.01028   0.00376  -0.1146   0.1734   0.6628
   2.000   0.6932   0.01058   0.00393  -0.1145   0.1461   0.6644
   2.250   0.7209   0.01084   0.00410  -0.1144   0.1261   0.6661
   2.500   0.7482   0.01114   0.00430  -0.1142   0.1063   0.6678
   2.750   0.7756   0.01143   0.00450  -0.1140   0.0921   0.6694
   3.000   0.8033   0.01167   0.00469  -0.1139   0.0835   0.6711
   3.250   0.8311   0.01190   0.00489  -0.1138   0.0772   0.6728
   3.500   0.8585   0.01218   0.00511  -0.1136   0.0718   0.6744
   3.750   0.8865   0.01238   0.00530  -0.1135   0.0688   0.6760
   4.000   0.9141   0.01262   0.00551  -0.1133   0.0657   0.6773
   4.250   0.9410   0.01290   0.00577  -0.1131   0.0624   0.6793
   4.500   0.9687   0.01306   0.00596  -0.1129   0.0607   0.6810
   4.750   0.9959   0.01329   0.00618  -0.1127   0.0585   0.6827
   5.000   1.0224   0.01359   0.00647  -0.1123   0.0561   0.6844
   5.250   1.0491   0.01386   0.00675  -0.1120   0.0544   0.6862
   5.500   1.0760   0.01409   0.00699  -0.1117   0.0529   0.6881
   5.750   1.1026   0.01436   0.00726  -0.1113   0.0511   0.6900
   6.000   1.1280   0.01475   0.00762  -0.1108   0.0490   0.6918
   6.250   1.1543   0.01503   0.00791  -0.1104   0.0477   0.6933
   6.500   1.1806   0.01525   0.00817  -0.1100   0.0462   0.6956
   6.750   1.2063   0.01554   0.00847  -0.1095   0.0446   0.6976
   7.000   1.2302   0.01602   0.00893  -0.1087   0.0425   0.6996
   7.250   1.2563   0.01624   0.00919  -0.1083   0.0414   0.7017
   7.500   1.2817   0.01652   0.00950  -0.1077   0.0400   0.7040
   7.750   1.3063   0.01688   0.00984  -0.1071   0.0386   0.7063
   8.000   1.3292   0.01741   0.01037  -0.1061   0.0371   0.7084
   8.250   1.3540   0.01769   0.01069  -0.1054   0.0362   0.7107
   8.500   1.3781   0.01802   0.01106  -0.1047   0.0352   0.7130
   8.750   1.4015   0.01839   0.01145  -0.1038   0.0343   0.7151
   9.000   1.4238   0.01885   0.01192  -0.1028   0.0333   0.7173
   9.250   1.4440   0.01948   0.01258  -0.1014   0.0323   0.7197
   9.500   1.4667   0.01986   0.01300  -0.1003   0.0318   0.7222
   9.750   1.4886   0.02027   0.01345  -0.0992   0.0311   0.7243
  10.000   1.5098   0.02070   0.01391  -0.0980   0.0305   0.7265
  10.250   1.5298   0.02116   0.01441  -0.0966   0.0299   0.7289
  10.500   1.5483   0.02169   0.01498  -0.0950   0.0293   0.7311
  10.750   1.5643   0.02236   0.01568  -0.0929   0.0287   0.7334
  11.000   1.5745   0.02325   0.01662  -0.0899   0.0281   0.7357
  11.250   1.5889   0.02378   0.01723  -0.0875   0.0279   0.7381
  11.500   1.6040   0.02441   0.01791  -0.0854   0.0276   0.7403
  11.750   1.6189   0.02508   0.01865  -0.0833   0.0273   0.7424
  12.000   1.6334   0.02579   0.01944  -0.0812   0.0269   0.7451
  12.250   1.6469   0.02656   0.02028  -0.0791   0.0266   0.7475
  12.500   1.6599   0.02739   0.02117  -0.0770   0.0263   0.7501
  12.750   1.6725   0.02826   0.02210  -0.0748   0.0260   0.7527
  13.000   1.6840   0.02921   0.02311  -0.0727   0.0257   0.7552
  13.250   1.6948   0.03025   0.02420  -0.0706   0.0254   0.7573
  13.500   1.7035   0.03145   0.02546  -0.0683   0.0251   0.7595
  13.750   1.7093   0.03289   0.02698  -0.0659   0.0247   0.7621
  14.000   1.7092   0.03486   0.02905  -0.0631   0.0243   0.7643
  14.250   1.7142   0.03647   0.03077  -0.0609   0.0241   0.7667
  14.500   1.7220   0.03789   0.03228  -0.0592   0.0240   0.7691
  14.750   1.7287   0.03947   0.03395  -0.0575   0.0238   0.7715
  15.000   1.7341   0.04120   0.03577  -0.0558   0.0237   0.7738
  15.250   1.7381   0.04309   0.03777  -0.0542   0.0235   0.7759
  15.500   1.7406   0.04519   0.03998  -0.0528   0.0234   0.7785
  15.750   1.7420   0.04748   0.04238  -0.0515   0.0232   0.7809
  16.000   1.7421   0.04998   0.04500  -0.0503   0.0230   0.7832
  16.250   1.7408   0.05271   0.04783  -0.0494   0.0229   0.7855
  16.500   1.7386   0.05571   0.05095  -0.0488   0.0227   0.7879
  16.750   1.7345   0.05908   0.05443  -0.0485   0.0226   0.7900
  17.250   1.7223   0.06687   0.06245  -0.0490   0.0223   0.7942
  17.500   1.7135   0.07146   0.06718  -0.0500   0.0222   0.7963
  17.750   1.7025   0.07663   0.07248  -0.0515   0.0221   0.7983
  18.000   1.6891   0.08242   0.07841  -0.0537   0.0220   0.8002
  18.250   1.6730   0.08888   0.08502  -0.0564   0.0220   0.8020
  18.500   1.6543   0.09604   0.09232  -0.0599   0.0219   0.8037
  18.750   1.6330   0.10386   0.10029  -0.0639   0.0218   0.8051
  19.000   1.6088   0.11230   0.10889  -0.0685   0.0218   0.8064
  19.250   1.5833   0.12116   0.11790  -0.0736   0.0217   0.8074
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