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NASA SC(2)-0012 AIRFOIL (sc20012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA SC(2)-0012 AIRFOIL (sc20012-il)
Reynolds number: 1,000,000
Max Cl/Cd: 72.91 at α=9.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc20012-il-1000000-n5.txt
Download as CSV file: xf-sc20012-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA SC(2)-0012 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
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -1.2070   0.12258   0.11982   0.0093   1.0000   0.0123
 -19.000  -1.2854   0.10350   0.10048  -0.0013   1.0000   0.0122
 -18.750  -1.3482   0.08747   0.08419  -0.0102   1.0000   0.0121
 -18.500  -1.3879   0.07610   0.07260  -0.0168   1.0000   0.0121
 -18.250  -1.4136   0.06778   0.06410  -0.0215   1.0000   0.0121
 -18.000  -1.4317   0.06135   0.05750  -0.0248   1.0000   0.0121
 -17.750  -1.4449   0.05614   0.05215  -0.0269   1.0000   0.0121
 -17.500  -1.4544   0.05185   0.04773  -0.0283   1.0000   0.0122
 -17.250  -1.4614   0.04812   0.04388  -0.0290   1.0000   0.0122
 -17.000  -1.4655   0.04490   0.04054  -0.0294   1.0000   0.0123
 -16.750  -1.4673   0.04207   0.03760  -0.0294   1.0000   0.0123
 -16.500  -1.4671   0.03955   0.03497  -0.0293   1.0000   0.0124
 -16.250  -1.4652   0.03728   0.03260  -0.0289   1.0000   0.0125
 -16.000  -1.4617   0.03525   0.03047  -0.0283   1.0000   0.0125
 -15.750  -1.4568   0.03341   0.02854  -0.0275   1.0000   0.0126
 -15.500  -1.4506   0.03176   0.02679  -0.0267   1.0000   0.0127
 -15.250  -1.4433   0.03026   0.02520  -0.0256   1.0000   0.0127
 -15.000  -1.4349   0.02891   0.02377  -0.0245   1.0000   0.0128
 -14.750  -1.4256   0.02768   0.02245  -0.0232   1.0000   0.0129
 -14.500  -1.4155   0.02657   0.02126  -0.0219   1.0000   0.0129
 -14.250  -1.4044   0.02557   0.02018  -0.0204   1.0000   0.0130
 -14.000  -1.3945   0.02453   0.01906  -0.0186   1.0000   0.0131
 -13.750  -1.3843   0.02355   0.01802  -0.0167   1.0000   0.0133
 -13.500  -1.3730   0.02271   0.01711  -0.0147   1.0000   0.0135
 -13.250  -1.3602   0.02196   0.01631  -0.0127   1.0000   0.0137
 -13.000  -1.3440   0.02126   0.01556  -0.0113   1.0000   0.0139
 -12.750  -1.3262   0.02061   0.01485  -0.0101   1.0000   0.0141
 -12.500  -1.3074   0.01999   0.01419  -0.0091   1.0000   0.0143
 -12.250  -1.2876   0.01940   0.01356  -0.0081   1.0000   0.0145
 -12.000  -1.2671   0.01884   0.01295  -0.0072   1.0000   0.0148
 -11.750  -1.2460   0.01831   0.01238  -0.0064   1.0000   0.0150
 -11.500  -1.2242   0.01781   0.01183  -0.0057   1.0000   0.0153
 -11.250  -1.2020   0.01733   0.01131  -0.0050   1.0000   0.0156
 -11.000  -1.1792   0.01687   0.01082  -0.0044   1.0000   0.0158
 -10.750  -1.1568   0.01636   0.01028  -0.0038   1.0000   0.0163
 -10.500  -1.1337   0.01589   0.00979  -0.0032   1.0000   0.0168
 -10.250  -1.1102   0.01546   0.00934  -0.0027   1.0000   0.0174
 -10.000  -1.0863   0.01505   0.00892  -0.0022   1.0000   0.0181
  -9.750  -1.0620   0.01468   0.00852  -0.0018   1.0000   0.0188
  -9.500  -1.0378   0.01428   0.00811  -0.0013   1.0000   0.0198
  -9.250  -1.0133   0.01390   0.00774  -0.0009   1.0000   0.0209
  -9.000  -0.9844   0.01355   0.00737  -0.0014   0.9880   0.0221
  -8.750  -0.9544   0.01319   0.00701  -0.0022   0.9713   0.0235
  -8.500  -0.9271   0.01289   0.00669  -0.0022   0.9500   0.0252
  -8.250  -0.9030   0.01266   0.00639  -0.0015   0.9250   0.0266
  -8.000  -0.8795   0.01242   0.00611  -0.0007   0.9016   0.0284
  -7.750  -0.8547   0.01223   0.00584  -0.0001   0.8810   0.0301
  -7.500  -0.8293   0.01202   0.00557   0.0004   0.8628   0.0317
  -7.250  -0.8034   0.01181   0.00532   0.0007   0.8469   0.0336
  -7.000  -0.7770   0.01163   0.00508   0.0009   0.8338   0.0352
  -6.750  -0.7504   0.01143   0.00484   0.0011   0.8229   0.0369
  -6.500  -0.7236   0.01123   0.00462   0.0012   0.8133   0.0388
  -6.250  -0.6965   0.01106   0.00441   0.0013   0.8052   0.0407
  -6.000  -0.6692   0.01087   0.00420   0.0014   0.7979   0.0425
  -5.750  -0.6420   0.01068   0.00401   0.0014   0.7911   0.0447
  -5.500  -0.6144   0.01052   0.00382   0.0014   0.7856   0.0466
  -5.250  -0.5867   0.01035   0.00364   0.0014   0.7804   0.0487
  -5.000  -0.5591   0.01016   0.00346   0.0014   0.7754   0.0520
  -4.750  -0.5313   0.01002   0.00331   0.0014   0.7708   0.0548
  -4.500  -0.5034   0.00984   0.00313   0.0014   0.7671   0.0580
  -4.250  -0.4753   0.00967   0.00298   0.0013   0.7635   0.0614
  -4.000  -0.4472   0.00951   0.00283   0.0012   0.7599   0.0655
  -3.750  -0.4192   0.00935   0.00269   0.0012   0.7562   0.0713
  -3.500  -0.3911   0.00919   0.00256   0.0011   0.7524   0.0797
  -3.250  -0.3631   0.00901   0.00243   0.0010   0.7489   0.0916
  -3.000  -0.3348   0.00883   0.00231   0.0009   0.7457   0.1058
  -2.750  -0.3065   0.00866   0.00220   0.0008   0.7423   0.1202
  -2.500  -0.2783   0.00849   0.00210   0.0007   0.7384   0.1370
  -2.250  -0.2504   0.00829   0.00198   0.0006   0.7333   0.1646
  -2.000  -0.2224   0.00805   0.00188   0.0005   0.7282   0.1984
  -1.750  -0.1943   0.00781   0.00177   0.0004   0.7226   0.2351
  -1.500  -0.1665   0.00755   0.00167   0.0003   0.7177   0.2832
  -1.250  -0.1390   0.00723   0.00156   0.0002   0.7125   0.3463
  -1.000  -0.1114   0.00686   0.00145   0.0001   0.7070   0.4164
  -0.750  -0.0842   0.00645   0.00133   0.0001   0.6997   0.5035
  -0.500  -0.0577   0.00600   0.00128   0.0002   0.6923   0.6143
  -0.250  -0.0290   0.00591   0.00130   0.0001   0.6845   0.6532
   0.000   0.0000   0.00590   0.00131   0.0000   0.6741   0.6743
   0.250   0.0290   0.00591   0.00130  -0.0001   0.6527   0.6844
   0.500   0.0577   0.00600   0.00128  -0.0002   0.6153   0.6924
   0.750   0.0842   0.00645   0.00133  -0.0001   0.5024   0.6998
   1.000   0.1114   0.00686   0.00145  -0.0001   0.4168   0.7069
   1.250   0.1390   0.00723   0.00156  -0.0002   0.3463   0.7127
   1.500   0.1665   0.00755   0.00167  -0.0003   0.2831   0.7178
   1.750   0.1943   0.00781   0.00177  -0.0004   0.2347   0.7226
   2.000   0.2224   0.00805   0.00188  -0.0005   0.1986   0.7283
   2.250   0.2503   0.00829   0.00198  -0.0006   0.1644   0.7336
   2.500   0.2782   0.00849   0.00210  -0.0007   0.1367   0.7384
   2.750   0.3065   0.00866   0.00220  -0.0008   0.1202   0.7423
   3.000   0.3348   0.00883   0.00231  -0.0009   0.1058   0.7457
   3.250   0.3631   0.00901   0.00243  -0.0010   0.0917   0.7488
   3.500   0.3911   0.00919   0.00256  -0.0011   0.0797   0.7523
   3.750   0.4192   0.00935   0.00269  -0.0012   0.0712   0.7562
   4.000   0.4472   0.00951   0.00283  -0.0012   0.0655   0.7599
   4.250   0.4753   0.00967   0.00298  -0.0013   0.0614   0.7635
   4.500   0.5034   0.00984   0.00313  -0.0014   0.0580   0.7670
   4.750   0.5313   0.01002   0.00331  -0.0014   0.0548   0.7708
   5.000   0.5591   0.01016   0.00346  -0.0014   0.0521   0.7753
   5.250   0.5867   0.01035   0.00364  -0.0014   0.0487   0.7804
   5.500   0.6144   0.01052   0.00382  -0.0014   0.0466   0.7856
   5.750   0.6420   0.01068   0.00401  -0.0014   0.0447   0.7911
   6.000   0.6692   0.01087   0.00420  -0.0014   0.0425   0.7979
   6.250   0.6965   0.01106   0.00441  -0.0013   0.0406   0.8052
   6.500   0.7236   0.01123   0.00462  -0.0012   0.0388   0.8133
   6.750   0.7504   0.01143   0.00484  -0.0011   0.0369   0.8229
   7.000   0.7770   0.01163   0.00508  -0.0009   0.0352   0.8337
   7.250   0.8034   0.01181   0.00532  -0.0007   0.0336   0.8468
   7.500   0.8293   0.01202   0.00557  -0.0004   0.0317   0.8627
   7.750   0.8547   0.01223   0.00584   0.0001   0.0301   0.8809
   8.000   0.8795   0.01242   0.00611   0.0007   0.0284   0.9016
   8.250   0.9031   0.01266   0.00639   0.0015   0.0266   0.9250
   8.500   0.9271   0.01289   0.00669   0.0022   0.0252   0.9500
   8.750   0.9545   0.01319   0.00701   0.0022   0.0236   0.9713
   9.000   0.9845   0.01355   0.00737   0.0014   0.0221   0.9881
   9.250   1.0134   0.01390   0.00774   0.0009   0.0209   1.0000
   9.500   1.0379   0.01428   0.00811   0.0013   0.0197   1.0000
   9.750   1.0621   0.01468   0.00852   0.0018   0.0188   1.0000
  10.000   1.0864   0.01505   0.00892   0.0022   0.0181   1.0000
  10.250   1.1103   0.01545   0.00934   0.0027   0.0174   1.0000
  10.500   1.1338   0.01589   0.00979   0.0032   0.0168   1.0000
  10.750   1.1568   0.01636   0.01028   0.0038   0.0163   1.0000
  11.000   1.1793   0.01687   0.01082   0.0044   0.0158   1.0000
  11.250   1.2021   0.01733   0.01131   0.0050   0.0156   1.0000
  11.500   1.2244   0.01781   0.01183   0.0057   0.0153   1.0000
  11.750   1.2461   0.01831   0.01238   0.0064   0.0150   1.0000
  12.000   1.2673   0.01884   0.01295   0.0072   0.0148   1.0000
  12.250   1.2878   0.01940   0.01355   0.0081   0.0145   1.0000
  12.500   1.3076   0.01998   0.01418   0.0090   0.0143   1.0000
  12.750   1.3265   0.02061   0.01485   0.0101   0.0141   1.0000
  13.000   1.3444   0.02126   0.01556   0.0112   0.0139   1.0000
  13.250   1.3607   0.02196   0.01630   0.0126   0.0137   1.0000
  13.500   1.3736   0.02270   0.01710   0.0146   0.0135   1.0000
  13.750   1.3848   0.02356   0.01802   0.0166   0.0133   1.0000
  14.000   1.3950   0.02454   0.01907   0.0185   0.0131   1.0000
  14.250   1.4051   0.02557   0.02018   0.0203   0.0130   1.0000
  14.500   1.4163   0.02657   0.02126   0.0217   0.0129   1.0000
  14.750   1.4266   0.02767   0.02244   0.0231   0.0129   1.0000
  15.000   1.4359   0.02890   0.02375   0.0243   0.0128   1.0000
  15.250   1.4444   0.03024   0.02518   0.0255   0.0127   1.0000
  15.500   1.4519   0.03173   0.02676   0.0265   0.0127   1.0000
  15.750   1.4580   0.03338   0.02851   0.0274   0.0126   1.0000
  16.000   1.4630   0.03522   0.03044   0.0281   0.0125   1.0000
  16.250   1.4667   0.03723   0.03256   0.0287   0.0125   1.0000
  16.500   1.4688   0.03949   0.03491   0.0290   0.0124   1.0000
  16.750   1.4689   0.04203   0.03756   0.0292   0.0123   1.0000
  17.000   1.4674   0.04482   0.04046   0.0292   0.0123   1.0000
  17.250   1.4632   0.04807   0.04383   0.0288   0.0122   1.0000
  17.500   1.4566   0.05175   0.04763   0.0280   0.0122   1.0000
  17.750   1.4472   0.05604   0.05205   0.0267   0.0121   1.0000
  18.000   1.4340   0.06124   0.05740   0.0245   0.0121   1.0000
  18.250   1.4164   0.06759   0.06391   0.0213   0.0121   1.0000
  18.500   1.3911   0.07585   0.07235   0.0167   0.0121   1.0000
  18.750   1.3515   0.08722   0.08394   0.0100   0.0121   1.0000
  19.000   1.2890   0.10321   0.10019   0.0011   0.0122   1.0000
  19.250   1.2099   0.12241   0.11965  -0.0095   0.0123   1.0000
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