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NASA SC(2)-0714 AIRFOIL (sc20714-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NASA SC(2)-0714 AIRFOIL (sc20714-il)
Reynolds number: 500,000
Max Cl/Cd: 63.05 at α=0.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sc20714-il-500000.txt
Download as CSV file: xf-sc20714-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.9204   0.10182   0.09834  -0.0570   1.0000   0.0315
 -18.000  -0.9840   0.08595   0.08213  -0.0669   1.0000   0.0313
 -17.750  -1.0141   0.07728   0.07322  -0.0719   1.0000   0.0314
 -17.500  -1.0351   0.07070   0.06644  -0.0754   1.0000   0.0315
 -17.250  -1.0510   0.06534   0.06090  -0.0778   1.0000   0.0316
 -17.000  -1.0635   0.06083   0.05622  -0.0795   1.0000   0.0318
 -16.750  -1.0735   0.05697   0.05219  -0.0805   1.0000   0.0320
 -16.500  -1.0816   0.05364   0.04870  -0.0810   1.0000   0.0322
 -16.250  -1.0881   0.05076   0.04568  -0.0810   1.0000   0.0324
 -16.000  -1.0937   0.04827   0.04304  -0.0805   1.0000   0.0325
 -15.750  -1.0983   0.04572   0.04036  -0.0796   1.0000   0.0328
 -15.500  -1.0971   0.04380   0.03840  -0.0784   1.0000   0.0332
 -15.250  -1.0950   0.04225   0.03682  -0.0771   1.0000   0.0335
 -15.000  -1.0931   0.04085   0.03538  -0.0756   1.0000   0.0338
 -14.750  -1.0921   0.03952   0.03401  -0.0738   1.0000   0.0341
 -14.500  -1.0915   0.03827   0.03272  -0.0718   1.0000   0.0344
 -14.250  -1.0917   0.03708   0.03147  -0.0695   1.0000   0.0347
 -14.000  -1.0923   0.03596   0.03029  -0.0670   1.0000   0.0351
 -13.750  -1.0937   0.03488   0.02915  -0.0642   1.0000   0.0354
 -13.500  -1.0957   0.03387   0.02808  -0.0612   1.0000   0.0358
 -13.250  -1.0992   0.03295   0.02708  -0.0578   1.0000   0.0362
 -13.000  -1.1054   0.03211   0.02618  -0.0539   1.0000   0.0365
 -12.750  -1.1138   0.03134   0.02533  -0.0495   1.0000   0.0368
 -12.500  -1.1102   0.03046   0.02436  -0.0472   1.0000   0.0372
 -12.250  -1.1028   0.02936   0.02319  -0.0453   1.0000   0.0377
 -12.000  -1.0797   0.02823   0.02208  -0.0461   0.9988   0.0386
 -11.750  -1.0529   0.02734   0.02118  -0.0476   0.9972   0.0393
 -11.500  -1.0246   0.02649   0.02030  -0.0494   0.9956   0.0402
 -11.250  -0.9951   0.02568   0.01942  -0.0513   0.9942   0.0412
 -11.000  -0.9648   0.02493   0.01860  -0.0532   0.9931   0.0422
 -10.750  -0.9391   0.02411   0.01770  -0.0540   0.9914   0.0430
 -10.500  -0.9143   0.02319   0.01682  -0.0548   0.9894   0.0443
 -10.250  -0.8852   0.02257   0.01621  -0.0564   0.9876   0.0456
 -10.000  -0.8548   0.02199   0.01559  -0.0581   0.9860   0.0470
  -9.750  -0.8231   0.02146   0.01499  -0.0599   0.9847   0.0483
  -9.500  -0.7922   0.02060   0.01416  -0.0617   0.9836   0.0500
  -9.250  -0.7582   0.02005   0.01363  -0.0641   0.9826   0.0517
  -9.000  -0.7232   0.01959   0.01315  -0.0664   0.9818   0.0536
  -8.750  -0.6878   0.01919   0.01270  -0.0688   0.9811   0.0555
  -8.500  -0.6622   0.01846   0.01202  -0.0695   0.9779   0.0577
  -8.250  -0.6306   0.01803   0.01159  -0.0711   0.9758   0.0601
  -8.000  -0.5977   0.01767   0.01120  -0.0729   0.9743   0.0623
  -7.750  -0.5626   0.01701   0.01058  -0.0755   0.9732   0.0653
  -7.500  -0.5272   0.01662   0.01020  -0.0778   0.9721   0.0686
  -7.250  -0.4906   0.01622   0.00979  -0.0804   0.9711   0.0721
  -7.000  -0.4526   0.01573   0.00936  -0.0833   0.9704   0.0768
  -6.750  -0.4148   0.01537   0.00901  -0.0860   0.9697   0.0819
  -6.500  -0.3769   0.01501   0.00870  -0.0888   0.9692   0.0890
  -6.250  -0.3384   0.01461   0.00837  -0.0917   0.9687   0.0982
  -6.000  -0.2992   0.01422   0.00806  -0.0948   0.9682   0.1109
  -5.750  -0.2593   0.01384   0.00779  -0.0980   0.9678   0.1310
  -5.500  -0.2312   0.01342   0.00754  -0.0989   0.9638   0.1594
  -5.250  -0.1894   0.01283   0.00722  -0.1030   0.9632   0.2159
  -5.000  -0.1205   0.01150   0.00658  -0.1139   0.9680   0.3698
  -4.750  -0.0695   0.01065   0.00640  -0.1203   0.9685   0.5271
  -4.500  -0.0322   0.01069   0.00655  -0.1223   0.9678   0.5708
  -4.250  -0.0102   0.01083   0.00671  -0.1210   0.9625   0.5876
  -4.000   0.0227   0.01091   0.00676  -0.1219   0.9602   0.6018
  -3.750   0.0569   0.01101   0.00686  -0.1230   0.9583   0.6135
  -3.500   0.0916   0.01110   0.00697  -0.1242   0.9568   0.6221
  -3.250   0.1273   0.01120   0.00708  -0.1255   0.9556   0.6301
  -3.000   0.1658   0.01120   0.00705  -0.1276   0.9547   0.6360
  -2.750   0.2056   0.01116   0.00706  -0.1296   0.9538   0.6405
  -2.500   0.2278   0.01127   0.00720  -0.1279   0.9464   0.6459
  -2.250   0.2720   0.01105   0.00698  -0.1307   0.9437   0.6537
  -2.000   0.3121   0.01079   0.00680  -0.1319   0.9402   0.6581
  -1.750   0.3423   0.01073   0.00678  -0.1315   0.9343   0.6620
  -1.500   0.3728   0.01061   0.00667  -0.1312   0.9267   0.6671
  -1.250   0.4096   0.01031   0.00632  -0.1326   0.9195   0.6712
  -1.000   0.4364   0.01017   0.00622  -0.1319   0.9111   0.6729
  -0.750   0.4665   0.01001   0.00607  -0.1318   0.9026   0.6743
  -0.500   0.4943   0.00991   0.00597  -0.1312   0.8899   0.6757
  -0.250   0.5225   0.00983   0.00590  -0.1308   0.8757   0.6771
   0.000   0.5513   0.00977   0.00583  -0.1306   0.8584   0.6787
   0.250   0.5807   0.00975   0.00574  -0.1304   0.8362   0.6806
   0.500   0.6088   0.00978   0.00567  -0.1301   0.7995   0.6826
   0.750   0.6343   0.01006   0.00560  -0.1291   0.7227   0.6850
   1.000   0.6514   0.01099   0.00578  -0.1268   0.5786   0.6874
   1.250   0.6702   0.01199   0.00609  -0.1252   0.4407   0.6893
   1.500   0.6914   0.01277   0.00635  -0.1242   0.3325   0.6908
   2.000   0.7365   0.01405   0.00688  -0.1224   0.1819   0.6930
   2.250   0.7611   0.01453   0.00715  -0.1218   0.1447   0.6940
   2.500   0.7869   0.01489   0.00740  -0.1213   0.1224   0.6951
   2.750   0.8129   0.01524   0.00766  -0.1209   0.1069   0.6963
   3.000   0.8390   0.01557   0.00793  -0.1206   0.0965   0.6975
   3.250   0.8649   0.01595   0.00824  -0.1201   0.0885   0.6988
   3.500   0.8918   0.01620   0.00848  -0.1199   0.0831   0.7004
   3.750   0.9175   0.01660   0.00884  -0.1194   0.0783   0.7021
   4.000   0.9446   0.01685   0.00909  -0.1193   0.0749   0.7037
   4.250   0.9710   0.01720   0.00939  -0.1190   0.0714   0.7052
   4.500   0.9969   0.01761   0.00979  -0.1187   0.0685   0.7067
   4.750   1.0238   0.01791   0.01010  -0.1185   0.0661   0.7081
   5.000   1.0500   0.01827   0.01043  -0.1182   0.0637   0.7093
   5.250   1.0728   0.01886   0.01099  -0.1173   0.0612   0.7106
   5.500   1.0984   0.01908   0.01128  -0.1167   0.0594   0.7118
   5.750   1.1231   0.01940   0.01162  -0.1160   0.0572   0.7129
   6.000   1.1466   0.01981   0.01203  -0.1152   0.0553   0.7141
   6.250   1.1680   0.02046   0.01269  -0.1139   0.0534   0.7155
   6.500   1.1920   0.02082   0.01312  -0.1131   0.0518   0.7170
   6.750   1.2154   0.02122   0.01354  -0.1122   0.0501   0.7185
   7.000   1.2378   0.02173   0.01403  -0.1112   0.0485   0.7200
   7.250   1.2584   0.02249   0.01481  -0.1099   0.0470   0.7215
   7.500   1.2816   0.02291   0.01530  -0.1090   0.0456   0.7231
   7.750   1.3040   0.02337   0.01578  -0.1081   0.0442   0.7248
   8.000   1.3254   0.02390   0.01630  -0.1069   0.0430   0.7264
   8.250   1.3437   0.02487   0.01725  -0.1054   0.0418   0.7278
   8.500   1.3639   0.02553   0.01798  -0.1041   0.0410   0.7292
   8.750   1.3832   0.02608   0.01863  -0.1025   0.0401   0.7306
   9.000   1.4007   0.02670   0.01933  -0.1006   0.0392   0.7319
   9.250   1.4152   0.02732   0.02002  -0.0982   0.0385   0.7334
   9.500   1.4297   0.02799   0.02073  -0.0959   0.0378   0.7349
   9.750   1.4451   0.02881   0.02157  -0.0939   0.0371   0.7366
  10.000   1.4601   0.03021   0.02300  -0.0920   0.0363   0.7383
  10.250   1.4756   0.03089   0.02380  -0.0900   0.0358   0.7401
  10.500   1.4908   0.03170   0.02472  -0.0881   0.0352   0.7419
  10.750   1.5052   0.03262   0.02574  -0.0861   0.0346   0.7438
  11.000   1.5190   0.03359   0.02680  -0.0841   0.0340   0.7456
  11.250   1.5321   0.03461   0.02788  -0.0821   0.0335   0.7472
  11.500   1.5443   0.03561   0.02895  -0.0801   0.0331   0.7488
  11.750   1.5552   0.03669   0.03010  -0.0779   0.0327   0.7502
  12.000   1.5653   0.03791   0.03138  -0.0757   0.0323   0.7517
  12.250   1.5737   0.03949   0.03302  -0.0735   0.0319   0.7532
  12.500   1.5796   0.04149   0.03516  -0.0710   0.0315   0.7549
  12.750   1.5850   0.04303   0.03686  -0.0686   0.0313   0.7569
  13.000   1.5892   0.04475   0.03874  -0.0662   0.0310   0.7589
  13.250   1.5921   0.04666   0.04082  -0.0640   0.0307   0.7610
  13.500   1.5937   0.04877   0.04307  -0.0618   0.0304   0.7629
  13.750   1.5940   0.05103   0.04549  -0.0599   0.0302   0.7646
  14.000   1.5930   0.05346   0.04807  -0.0580   0.0299   0.7661
  14.250   1.5903   0.05608   0.05085  -0.0564   0.0296   0.7676
  14.500   1.5865   0.05888   0.05381  -0.0550   0.0294   0.7690
  14.750   1.5820   0.06186   0.05694  -0.0539   0.0291   0.7705
  15.000   1.5763   0.06516   0.06038  -0.0532   0.0289   0.7720
  15.250   1.5697   0.06875   0.06411  -0.0530   0.0287   0.7736
  15.500   1.5630   0.07256   0.06805  -0.0532   0.0285   0.7753
  15.750   1.5530   0.07714   0.07277  -0.0540   0.0284   0.7770
  16.000   1.5431   0.08195   0.07772  -0.0554   0.0282   0.7786
  16.250   1.5292   0.08773   0.08365  -0.0575   0.0282   0.7801
  16.500   1.5144   0.09396   0.09003  -0.0604   0.0280   0.7815
  16.750   1.4935   0.10167   0.09793  -0.0646   0.0280   0.7825
  17.000   1.4674   0.11092   0.10741  -0.0703   0.0279   0.7834
  17.250   1.4167   0.12628   0.12313  -0.0812   0.0280   0.7833
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