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NASA SC(2)-0714 AIRFOIL (sc20714-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0714 AIRFOIL (sc20714-il)
Reynolds number: 1,000,000
Max Cl/Cd: 79.99 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20714-il-1000000-n5.txt
Download as CSV file: xf-sc20714-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.2574   0.07089   0.06684  -0.0687   1.0000   0.0193
 -19.500  -1.2653   0.06638   0.06222  -0.0708   1.0000   0.0194
 -19.250  -1.2703   0.06238   0.05813  -0.0726   1.0000   0.0196
 -19.000  -1.2730   0.05881   0.05447  -0.0741   1.0000   0.0197
 -18.750  -1.2740   0.05560   0.05117  -0.0753   1.0000   0.0199
 -18.500  -1.2734   0.05269   0.04818  -0.0763   1.0000   0.0200
 -18.250  -1.2713   0.05005   0.04546  -0.0770   1.0000   0.0202
 -18.000  -1.2683   0.04761   0.04295  -0.0776   1.0000   0.0203
 -17.750  -1.2643   0.04542   0.04067  -0.0779   1.0000   0.0205
 -17.500  -1.2595   0.04339   0.03858  -0.0780   1.0000   0.0206
 -17.250  -1.2549   0.04148   0.03660  -0.0779   1.0000   0.0207
 -17.000  -1.2526   0.03950   0.03456  -0.0776   1.0000   0.0209
 -16.750  -1.2504   0.03766   0.03267  -0.0769   1.0000   0.0212
 -16.500  -1.2473   0.03605   0.03102  -0.0760   1.0000   0.0214
 -16.250  -1.2442   0.03463   0.02955  -0.0748   1.0000   0.0216
 -16.000  -1.2419   0.03334   0.02822  -0.0731   1.0000   0.0218
 -15.750  -1.2404   0.03218   0.02702  -0.0711   1.0000   0.0220
 -15.500  -1.2314   0.03098   0.02579  -0.0705   0.9995   0.0223
 -15.250  -1.2144   0.02975   0.02451  -0.0713   0.9986   0.0226
 -15.000  -1.1959   0.02861   0.02332  -0.0721   0.9974   0.0229
 -14.750  -1.1765   0.02750   0.02217  -0.0731   0.9960   0.0232
 -14.500  -1.1557   0.02648   0.02110  -0.0741   0.9948   0.0236
 -14.250  -1.1340   0.02552   0.02010  -0.0752   0.9937   0.0239
 -14.000  -1.1117   0.02460   0.01913  -0.0763   0.9928   0.0242
 -13.750  -1.0945   0.02373   0.01823  -0.0763   0.9904   0.0245
 -13.500  -1.0756   0.02282   0.01730  -0.0767   0.9881   0.0250
 -13.250  -1.0546   0.02199   0.01645  -0.0773   0.9861   0.0255
 -13.000  -1.0313   0.02123   0.01568  -0.0782   0.9845   0.0261
 -12.750  -1.0051   0.02052   0.01494  -0.0795   0.9834   0.0268
 -12.500  -0.9778   0.01984   0.01424  -0.0810   0.9825   0.0274
 -12.250  -0.9498   0.01919   0.01356  -0.0825   0.9815   0.0279
 -12.000  -0.9249   0.01859   0.01293  -0.0834   0.9796   0.0284
 -11.750  -0.9012   0.01797   0.01231  -0.0840   0.9769   0.0292
 -11.500  -0.8745   0.01740   0.01173  -0.0850   0.9749   0.0300
 -11.250  -0.8462   0.01686   0.01119  -0.0863   0.9733   0.0308
 -11.000  -0.8169   0.01636   0.01068  -0.0877   0.9719   0.0317
 -10.750  -0.7870   0.01590   0.01019  -0.0892   0.9705   0.0325
 -10.500  -0.7566   0.01538   0.00967  -0.0908   0.9693   0.0336
 -10.250  -0.7255   0.01491   0.00921  -0.0924   0.9682   0.0349
 -10.000  -0.6970   0.01450   0.00880  -0.0935   0.9662   0.0359
  -9.750  -0.6683   0.01413   0.00841  -0.0944   0.9639   0.0369
  -9.500  -0.6384   0.01374   0.00801  -0.0957   0.9620   0.0379
  -9.250  -0.6076   0.01332   0.00762  -0.0971   0.9603   0.0393
  -9.000  -0.5763   0.01295   0.00725  -0.0986   0.9586   0.0407
  -8.750  -0.5445   0.01262   0.00691  -0.1000   0.9571   0.0421
  -8.500  -0.5122   0.01227   0.00656  -0.1016   0.9557   0.0436
  -8.250  -0.4794   0.01192   0.00623  -0.1033   0.9545   0.0454
  -8.000  -0.4465   0.01161   0.00593  -0.1049   0.9533   0.0472
  -7.750  -0.4152   0.01135   0.00566  -0.1062   0.9515   0.0487
  -7.500  -0.3833   0.01104   0.00539  -0.1076   0.9496   0.0515
  -7.250  -0.3512   0.01078   0.00515  -0.1089   0.9477   0.0543
  -7.000  -0.3188   0.01052   0.00491  -0.1103   0.9459   0.0575
  -6.750  -0.2864   0.01028   0.00469  -0.1117   0.9440   0.0610
  -6.500  -0.2538   0.01004   0.00447  -0.1130   0.9421   0.0648
  -6.250  -0.2208   0.00980   0.00426  -0.1144   0.9403   0.0697
  -6.000  -0.1875   0.00957   0.00406  -0.1159   0.9387   0.0758
  -5.750  -0.1545   0.00934   0.00389  -0.1173   0.9371   0.0835
  -5.500  -0.1222   0.00915   0.00374  -0.1185   0.9349   0.0916
  -5.250  -0.0893   0.00893   0.00358  -0.1199   0.9326   0.1011
  -5.000  -0.0562   0.00872   0.00343  -0.1213   0.9304   0.1122
  -4.750  -0.0225   0.00849   0.00328  -0.1228   0.9284   0.1300
  -4.500   0.0117   0.00824   0.00313  -0.1245   0.9265   0.1511
  -4.250   0.0467   0.00796   0.00297  -0.1264   0.9246   0.1810
  -4.000   0.0821   0.00768   0.00281  -0.1283   0.9224   0.2135
  -3.500   0.1568   0.00683   0.00242  -0.1334   0.9123   0.3381
  -3.250   0.1977   0.00624   0.00213  -0.1369   0.9047   0.4352
  -3.000   0.2362   0.00577   0.00198  -0.1396   0.8923   0.5321
  -2.750   0.2669   0.00573   0.00194  -0.1400   0.8769   0.5547
  -2.500   0.2971   0.00574   0.00192  -0.1403   0.8634   0.5668
  -2.250   0.3266   0.00579   0.00191  -0.1404   0.8408   0.5801
  -2.000   0.3545   0.00595   0.00193  -0.1401   0.8002   0.5920
  -1.750   0.3804   0.00629   0.00198  -0.1395   0.7352   0.6014
  -1.500   0.4031   0.00695   0.00218  -0.1383   0.6269   0.6073
  -1.250   0.4257   0.00772   0.00241  -0.1372   0.5021   0.6110
  -1.000   0.4504   0.00835   0.00261  -0.1367   0.4049   0.6158
  -0.750   0.4767   0.00879   0.00279  -0.1363   0.3360   0.6210
  -0.500   0.5033   0.00919   0.00296  -0.1361   0.2793   0.6242
  -0.250   0.5307   0.00951   0.00310  -0.1359   0.2367   0.6261
   0.000   0.5579   0.00985   0.00325  -0.1358   0.1945   0.6280
   0.250   0.5857   0.01011   0.00338  -0.1357   0.1651   0.6300
   0.500   0.6135   0.01037   0.00351  -0.1356   0.1428   0.6318
   0.750   0.6417   0.01059   0.00364  -0.1356   0.1258   0.6331
   1.000   0.6696   0.01082   0.00377  -0.1355   0.1085   0.6339
   1.250   0.6977   0.01102   0.00390  -0.1355   0.0977   0.6348
   1.500   0.7258   0.01121   0.00405  -0.1354   0.0893   0.6361
   1.750   0.7540   0.01138   0.00419  -0.1354   0.0822   0.6375
   2.000   0.7818   0.01158   0.00435  -0.1352   0.0752   0.6389
   2.250   0.8094   0.01180   0.00452  -0.1351   0.0689   0.6401
   2.500   0.8372   0.01199   0.00469  -0.1350   0.0643   0.6412
   2.750   0.8648   0.01220   0.00487  -0.1348   0.0606   0.6423
   3.000   0.8925   0.01239   0.00505  -0.1346   0.0576   0.6434
   3.250   0.9199   0.01261   0.00524  -0.1344   0.0544   0.6446
   3.500   0.9473   0.01281   0.00543  -0.1342   0.0524   0.6457
   3.750   0.9746   0.01302   0.00563  -0.1340   0.0504   0.6469
   4.000   1.0016   0.01326   0.00583  -0.1337   0.0484   0.6480
   4.250   1.0286   0.01349   0.00605  -0.1334   0.0469   0.6491
   4.500   1.0555   0.01371   0.00628  -0.1330   0.0454   0.6501
   4.750   1.0821   0.01396   0.00651  -0.1327   0.0438   0.6511
   5.000   1.1084   0.01423   0.00676  -0.1322   0.0423   0.6521
   5.250   1.1347   0.01448   0.00702  -0.1318   0.0412   0.6534
   5.500   1.1610   0.01471   0.00727  -0.1314   0.0402   0.6549
   5.750   1.1870   0.01497   0.00754  -0.1309   0.0390   0.6562
   6.000   1.2127   0.01525   0.00783  -0.1304   0.0377   0.6575
   6.250   1.2378   0.01557   0.00815  -0.1297   0.0364   0.6587
   6.500   1.2634   0.01583   0.00843  -0.1292   0.0355   0.6600
   6.750   1.2886   0.01611   0.00873  -0.1285   0.0342   0.6613
   7.000   1.3134   0.01642   0.00904  -0.1279   0.0329   0.6626
   7.250   1.3376   0.01677   0.00938  -0.1271   0.0316   0.6639
   7.500   1.3620   0.01708   0.00972  -0.1263   0.0308   0.6652
   7.750   1.3860   0.01741   0.01007  -0.1255   0.0298   0.6665
   8.000   1.4095   0.01776   0.01043  -0.1245   0.0288   0.6677
   8.250   1.4325   0.01815   0.01081  -0.1235   0.0279   0.6690
   8.500   1.4551   0.01855   0.01123  -0.1225   0.0272   0.6703
   8.750   1.4774   0.01893   0.01164  -0.1213   0.0266   0.6717
   9.000   1.4991   0.01932   0.01207  -0.1201   0.0260   0.6735
   9.250   1.5202   0.01974   0.01252  -0.1188   0.0253   0.6751
   9.500   1.5407   0.02018   0.01299  -0.1173   0.0247   0.6767
   9.750   1.5602   0.02066   0.01349  -0.1157   0.0241   0.6782
  10.000   1.5787   0.02119   0.01405  -0.1140   0.0235   0.6799
  10.250   1.5971   0.02166   0.01457  -0.1122   0.0232   0.6815
  10.500   1.6124   0.02214   0.01510  -0.1098   0.0229   0.6832
  10.750   1.6287   0.02267   0.01568  -0.1077   0.0226   0.6848
  11.000   1.6451   0.02324   0.01629  -0.1056   0.0223   0.6864
  11.250   1.6615   0.02383   0.01693  -0.1036   0.0220   0.6878
  11.500   1.6772   0.02447   0.01761  -0.1016   0.0217   0.6891
  11.750   1.6926   0.02514   0.01833  -0.0995   0.0214   0.6907
  12.000   1.7074   0.02585   0.01910  -0.0974   0.0211   0.6928
  12.250   1.7214   0.02661   0.01992  -0.0953   0.0208   0.6949
  12.500   1.7344   0.02745   0.02081  -0.0930   0.0205   0.6970
  12.750   1.7464   0.02837   0.02180  -0.0907   0.0202   0.6989
  13.000   1.7572   0.02937   0.02286  -0.0883   0.0200   0.7008
  13.250   1.7693   0.03027   0.02384  -0.0861   0.0198   0.7027
  13.500   1.7810   0.03122   0.02487  -0.0839   0.0197   0.7046
  13.750   1.7918   0.03225   0.02596  -0.0818   0.0196   0.7063
  14.000   1.8017   0.03335   0.02714  -0.0795   0.0194   0.7079
  14.250   1.8113   0.03450   0.02836  -0.0774   0.0192   0.7093
  14.500   1.8198   0.03575   0.02970  -0.0753   0.0191   0.7113
  14.750   1.8281   0.03705   0.03108  -0.0732   0.0188   0.7133
  15.000   1.8351   0.03847   0.03260  -0.0711   0.0187   0.7154
  15.250   1.8409   0.04003   0.03424  -0.0691   0.0185   0.7174
  15.500   1.8459   0.04171   0.03601  -0.0671   0.0183   0.7195
  15.750   1.8497   0.04355   0.03794  -0.0653   0.0182   0.7217
  16.000   1.8523   0.04554   0.04002  -0.0635   0.0180   0.7238
  16.250   1.8535   0.04773   0.04230  -0.0619   0.0179   0.7258
  16.500   1.8535   0.05015   0.04482  -0.0604   0.0178   0.7275
  17.000   1.8497   0.05580   0.05068  -0.0583   0.0175   0.7308
  17.250   1.8452   0.05913   0.05412  -0.0577   0.0174   0.7326
  17.500   1.8383   0.06296   0.05807  -0.0575   0.0173   0.7343
  17.750   1.8294   0.06729   0.06253  -0.0578   0.0172   0.7360
  18.000   1.8178   0.07226   0.06764  -0.0587   0.0171   0.7376
  18.250   1.8023   0.07808   0.07361  -0.0604   0.0170   0.7391
  18.500   1.7829   0.08484   0.08053  -0.0629   0.0170   0.7403
  18.750   1.7594   0.09266   0.08852  -0.0664   0.0169   0.7414
  19.000   1.7294   0.10198   0.09802  -0.0712   0.0169   0.7422
  19.250   1.6939   0.11256   0.10881  -0.0770   0.0169   0.7428
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