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NASA SC(2)-0714 AIRFOIL (sc20714-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0714 AIRFOIL (sc20714-il)
Reynolds number: 500,000
Max Cl/Cd: 64.19 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20714-il-500000-n5.txt
Download as CSV file: xf-sc20714-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0714 AIRFOIL                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0323   0.10690   0.10290  -0.0508   1.0000   0.0236
 -19.500  -1.0544   0.09904   0.09488  -0.0551   1.0000   0.0237
 -19.250  -1.0727   0.09207   0.08776  -0.0589   1.0000   0.0238
 -19.000  -1.0876   0.08579   0.08133  -0.0623   1.0000   0.0239
 -18.750  -1.0997   0.08016   0.07557  -0.0652   1.0000   0.0240
 -18.500  -1.1090   0.07512   0.07039  -0.0677   1.0000   0.0241
 -18.250  -1.1161   0.07055   0.06569  -0.0699   1.0000   0.0242
 -18.000  -1.1217   0.06639   0.06142  -0.0718   1.0000   0.0244
 -17.750  -1.1271   0.06242   0.05737  -0.0734   1.0000   0.0246
 -17.500  -1.1304   0.05887   0.05374  -0.0747   1.0000   0.0247
 -17.250  -1.1321   0.05569   0.05048  -0.0758   1.0000   0.0249
 -17.000  -1.1323   0.05283   0.04755  -0.0765   1.0000   0.0252
 -16.750  -1.1314   0.05024   0.04489  -0.0769   1.0000   0.0254
 -16.500  -1.1296   0.04793   0.04251  -0.0770   1.0000   0.0256
 -16.250  -1.1273   0.04581   0.04032  -0.0769   1.0000   0.0258
 -16.000  -1.1248   0.04385   0.03829  -0.0765   1.0000   0.0261
 -15.750  -1.1218   0.04207   0.03645  -0.0759   1.0000   0.0264
 -15.500  -1.1190   0.04042   0.03472  -0.0750   1.0000   0.0266
 -15.250  -1.1164   0.03890   0.03315  -0.0738   1.0000   0.0269
 -15.000  -1.1143   0.03752   0.03170  -0.0723   1.0000   0.0272
 -14.750  -1.1125   0.03623   0.03035  -0.0706   1.0000   0.0275
 -14.500  -1.1109   0.03505   0.02910  -0.0686   1.0000   0.0279
 -14.250  -1.1094   0.03397   0.02796  -0.0663   1.0000   0.0281
 -14.000  -1.1102   0.03285   0.02680  -0.0638   1.0000   0.0284
 -13.750  -1.0963   0.03150   0.02542  -0.0642   0.9988   0.0289
 -13.500  -1.0787   0.03029   0.02418  -0.0650   0.9972   0.0294
 -13.250  -1.0597   0.02921   0.02305  -0.0658   0.9955   0.0299
 -13.000  -1.0396   0.02819   0.02198  -0.0667   0.9940   0.0304
 -12.750  -1.0190   0.02723   0.02097  -0.0675   0.9925   0.0310
 -12.500  -1.0022   0.02633   0.02002  -0.0675   0.9896   0.0316
 -12.250  -0.9831   0.02547   0.01910  -0.0678   0.9868   0.0322
 -12.000  -0.9610   0.02460   0.01817  -0.0686   0.9847   0.0328
 -11.750  -0.9361   0.02367   0.01724  -0.0700   0.9831   0.0335
 -11.500  -0.9089   0.02289   0.01645  -0.0716   0.9819   0.0344
 -11.250  -0.8802   0.02219   0.01571  -0.0733   0.9810   0.0354
 -11.000  -0.8607   0.02157   0.01505  -0.0731   0.9772   0.0364
 -10.750  -0.8350   0.02095   0.01439  -0.0740   0.9749   0.0372
 -10.500  -0.8073   0.02021   0.01363  -0.0755   0.9731   0.0382
 -10.250  -0.7776   0.01955   0.01298  -0.0772   0.9717   0.0393
 -10.000  -0.7467   0.01897   0.01238  -0.0791   0.9707   0.0406
  -9.750  -0.7152   0.01843   0.01181  -0.0809   0.9698   0.0419
  -9.500  -0.6830   0.01788   0.01124  -0.0829   0.9691   0.0433
  -9.250  -0.6502   0.01732   0.01069  -0.0851   0.9685   0.0450
  -9.000  -0.6168   0.01683   0.01020  -0.0872   0.9680   0.0467
  -8.750  -0.5933   0.01644   0.00978  -0.0871   0.9640   0.0481
  -8.500  -0.5629   0.01596   0.00932  -0.0886   0.9620   0.0498
  -8.250  -0.5308   0.01553   0.00890  -0.0903   0.9606   0.0520
  -8.000  -0.4979   0.01514   0.00851  -0.0921   0.9594   0.0544
  -7.750  -0.4644   0.01472   0.00811  -0.0941   0.9583   0.0569
  -7.500  -0.4303   0.01433   0.00773  -0.0960   0.9574   0.0599
  -7.250  -0.3961   0.01400   0.00739  -0.0980   0.9566   0.0629
  -7.000  -0.3612   0.01359   0.00703  -0.1002   0.9558   0.0672
  -6.750  -0.3262   0.01326   0.00671  -0.1022   0.9551   0.0717
  -6.500  -0.2905   0.01289   0.00639  -0.1045   0.9543   0.0778
  -6.250  -0.2546   0.01254   0.00610  -0.1067   0.9536   0.0854
  -6.000  -0.2248   0.01230   0.00588  -0.1076   0.9507   0.0929
  -5.750  -0.1931   0.01202   0.00565  -0.1088   0.9483   0.1024
  -5.500  -0.1593   0.01171   0.00542  -0.1106   0.9466   0.1148
  -5.250  -0.1243   0.01138   0.00519  -0.1126   0.9451   0.1333
  -5.000  -0.0883   0.01102   0.00495  -0.1149   0.9438   0.1579
  -4.750  -0.0509   0.01062   0.00470  -0.1175   0.9427   0.1930
  -4.500  -0.0118   0.01014   0.00444  -0.1207   0.9418   0.2404
  -4.250   0.0316   0.00947   0.00410  -0.1251   0.9413   0.3213
  -4.000   0.0792   0.00864   0.00372  -0.1307   0.9412   0.4346
  -3.750   0.1210   0.00820   0.00368  -0.1343   0.9405   0.5349
  -3.500   0.1547   0.00816   0.00373  -0.1354   0.9391   0.5664
  -3.250   0.1874   0.00816   0.00373  -0.1363   0.9375   0.5805
  -3.000   0.2149   0.00820   0.00381  -0.1361   0.9328   0.5894
  -2.750   0.2465   0.00815   0.00374  -0.1366   0.9279   0.6003
  -2.500   0.2790   0.00807   0.00368  -0.1371   0.9224   0.6101
  -2.250   0.3074   0.00804   0.00363  -0.1368   0.9111   0.6190
  -2.000   0.3365   0.00801   0.00360  -0.1365   0.8982   0.6247
  -1.750   0.3667   0.00800   0.00355  -0.1366   0.8847   0.6311
  -1.500   0.3965   0.00800   0.00349  -0.1366   0.8661   0.6363
  -1.250   0.4252   0.00801   0.00345  -0.1363   0.8411   0.6386
  -1.000   0.4540   0.00807   0.00342  -0.1362   0.8143   0.6405
  -0.750   0.4808   0.00827   0.00338  -0.1355   0.7583   0.6422
  -0.500   0.5004   0.00899   0.00350  -0.1334   0.6361   0.6441
  -0.250   0.5196   0.00987   0.00379  -0.1317   0.5100   0.6466
   0.000   0.5421   0.01061   0.00405  -0.1307   0.4111   0.6490
   0.250   0.5670   0.01116   0.00424  -0.1302   0.3343   0.6507
   0.500   0.5927   0.01165   0.00442  -0.1299   0.2707   0.6519
   0.750   0.6189   0.01206   0.00460  -0.1296   0.2215   0.6531
   1.000   0.6449   0.01244   0.00480  -0.1292   0.1806   0.6542
   1.250   0.6715   0.01276   0.00499  -0.1290   0.1521   0.6552
   1.500   0.6983   0.01305   0.00518  -0.1287   0.1322   0.6563
   1.750   0.7252   0.01334   0.00539  -0.1284   0.1148   0.6576
   2.000   0.7522   0.01362   0.00559  -0.1282   0.1022   0.6590
   2.250   0.7794   0.01386   0.00579  -0.1280   0.0936   0.6602
   2.500   0.8066   0.01411   0.00600  -0.1278   0.0865   0.6614
   3.000   0.8607   0.01463   0.00644  -0.1273   0.0736   0.6639
   3.250   0.8874   0.01491   0.00668  -0.1270   0.0688   0.6652
   3.500   0.9144   0.01516   0.00692  -0.1268   0.0651   0.6665
   3.750   0.9409   0.01546   0.00718  -0.1264   0.0619   0.6678
   4.000   0.9677   0.01572   0.00745  -0.1261   0.0595   0.6690
   4.250   0.9942   0.01600   0.00771  -0.1258   0.0569   0.6702
   4.500   1.0201   0.01632   0.00801  -0.1253   0.0546   0.6715
   4.750   1.0458   0.01661   0.00833  -0.1248   0.0528   0.6728
   5.000   1.0714   0.01690   0.00864  -0.1243   0.0511   0.6741
   5.250   1.0966   0.01722   0.00897  -0.1237   0.0494   0.6753
   5.500   1.1212   0.01759   0.00934  -0.1230   0.0476   0.6765
   5.750   1.1463   0.01792   0.00970  -0.1223   0.0462   0.6777
   6.000   1.1710   0.01825   0.01006  -0.1217   0.0446   0.6790
   6.250   1.1953   0.01862   0.01044  -0.1209   0.0432   0.6804
   6.500   1.2188   0.01906   0.01087  -0.1201   0.0419   0.6818
   6.750   1.2427   0.01944   0.01129  -0.1192   0.0408   0.6832
   7.000   1.2663   0.01983   0.01171  -0.1184   0.0396   0.6847
   7.250   1.2895   0.02024   0.01215  -0.1174   0.0384   0.6861
   7.500   1.3121   0.02068   0.01260  -0.1164   0.0372   0.6876
   7.750   1.3338   0.02119   0.01311  -0.1153   0.0361   0.6890
   8.000   1.3558   0.02160   0.01359  -0.1141   0.0351   0.6905
   8.250   1.3770   0.02204   0.01409  -0.1128   0.0341   0.6921
   8.500   1.3974   0.02251   0.01460  -0.1114   0.0331   0.6935
   8.750   1.4169   0.02302   0.01515  -0.1099   0.0323   0.6949
   9.000   1.4350   0.02361   0.01576  -0.1081   0.0316   0.6964
   9.250   1.4521   0.02414   0.01637  -0.1061   0.0310   0.6979
   9.500   1.4676   0.02470   0.01700  -0.1039   0.0304   0.6995
   9.750   1.4842   0.02531   0.01767  -0.1019   0.0298   0.7011
  10.000   1.5010   0.02595   0.01836  -0.1000   0.0292   0.7028
  10.250   1.5175   0.02662   0.01908  -0.0981   0.0286   0.7045
  10.500   1.5334   0.02733   0.01984  -0.0962   0.0281   0.7062
  10.750   1.5481   0.02814   0.02068  -0.0942   0.0276   0.7078
  11.000   1.5622   0.02899   0.02158  -0.0921   0.0271   0.7094
  11.250   1.5763   0.02981   0.02251  -0.0901   0.0267   0.7112
  11.500   1.5897   0.03069   0.02348  -0.0880   0.0263   0.7129
  11.750   1.6024   0.03162   0.02451  -0.0859   0.0259   0.7147
  12.000   1.6142   0.03262   0.02560  -0.0837   0.0255   0.7165
  12.250   1.6256   0.03367   0.02674  -0.0816   0.0252   0.7183
  12.500   1.6360   0.03480   0.02795  -0.0794   0.0249   0.7201
  12.750   1.6455   0.03601   0.02924  -0.0773   0.0246   0.7219
  13.000   1.6539   0.03732   0.03063  -0.0751   0.0243   0.7238
  13.250   1.6609   0.03879   0.03218  -0.0730   0.0240   0.7257
  13.500   1.6658   0.04046   0.03392  -0.0708   0.0237   0.7274
  13.750   1.6686   0.04235   0.03589  -0.0685   0.0235   0.7290
  14.000   1.6734   0.04412   0.03779  -0.0666   0.0233   0.7305
  14.250   1.6771   0.04605   0.03986  -0.0648   0.0232   0.7322
  14.500   1.6794   0.04816   0.04211  -0.0631   0.0230   0.7338
  14.750   1.6803   0.05047   0.04456  -0.0615   0.0228   0.7356
  15.000   1.6799   0.05303   0.04726  -0.0602   0.0226   0.7376
  15.250   1.6780   0.05586   0.05022  -0.0591   0.0225   0.7396
  15.500   1.6750   0.05896   0.05345  -0.0583   0.0223   0.7415
  15.750   1.6705   0.06242   0.05706  -0.0579   0.0222   0.7434
  16.000   1.6649   0.06625   0.06102  -0.0579   0.0220   0.7452
  16.250   1.6576   0.07054   0.06545  -0.0585   0.0219   0.7467
  16.500   1.6485   0.07532   0.07039  -0.0596   0.0217   0.7480
  16.750   1.6373   0.08069   0.07593  -0.0613   0.0216   0.7492
  17.000   1.6234   0.08679   0.08219  -0.0638   0.0215   0.7504
  17.250   1.6071   0.09361   0.08919  -0.0670   0.0214   0.7515
  17.500   1.5873   0.10133   0.09709  -0.0710   0.0213   0.7525
  17.750   1.5639   0.10993   0.10588  -0.0758   0.0212   0.7534
  18.000   1.5379   0.11932   0.11546  -0.0813   0.0212   0.7541
  18.250   1.5083   0.12971   0.12605  -0.0878   0.0211   0.7547
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