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LOCKHEED-GEORGIA SUPERCRITICAL AIRFOIL (lg10sc-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: LOCKHEED-GEORGIA SUPERCRITICAL AIRFOIL (lg10sc-il)
Reynolds number: 100,000
Max Cl/Cd: 39.07 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-lg10sc-il-100000-n5.txt
Download as CSV file: xf-lg10sc-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: LOCKHEED-GEORGIA SUPERCRITICAL AIRFOIL          
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.4351   0.09603   0.09115  -0.0166   1.0000   0.0301
  -9.750  -0.5551   0.09957   0.09447  -0.0106   1.0000   0.0309
  -9.500  -0.5529   0.09579   0.09073  -0.0114   1.0000   0.0299
  -9.000  -0.5865   0.07661   0.07147  -0.0278   1.0000   0.0251
  -8.750  -0.5923   0.07315   0.06800  -0.0279   1.0000   0.0248
  -8.500  -0.5985   0.06945   0.06425  -0.0279   1.0000   0.0246
  -8.250  -0.6028   0.06553   0.06024  -0.0278   1.0000   0.0243
  -8.000  -0.6057   0.06152   0.05609  -0.0273   1.0000   0.0240
  -7.750  -0.6065   0.05751   0.05190  -0.0264   1.0000   0.0237
  -7.500  -0.6053   0.05355   0.04771  -0.0251   1.0000   0.0234
  -7.250  -0.6021   0.04969   0.04357  -0.0234   1.0000   0.0234
  -7.000  -0.5969   0.04602   0.03955  -0.0214   1.0000   0.0237
  -6.750  -0.5899   0.04251   0.03559  -0.0190   1.0000   0.0242
  -6.500  -0.5806   0.03933   0.03194  -0.0165   1.0000   0.0247
  -6.250  -0.5683   0.03656   0.02874  -0.0142   1.0000   0.0249
  -6.000  -0.5538   0.03402   0.02583  -0.0121   1.0000   0.0249
  -5.750  -0.5374   0.03170   0.02313  -0.0101   1.0000   0.0250
  -5.500  -0.5195   0.02959   0.02068  -0.0082   1.0000   0.0252
  -5.250  -0.5005   0.02765   0.01854  -0.0067   1.0000   0.0256
  -5.000  -0.4804   0.02606   0.01679  -0.0053   1.0000   0.0262
  -4.750  -0.4596   0.02468   0.01526  -0.0040   1.0000   0.0270
  -4.500  -0.4386   0.02356   0.01404  -0.0026   1.0000   0.0285
  -4.250  -0.4171   0.02256   0.01287  -0.0013   1.0000   0.0308
  -4.000  -0.3959   0.02141   0.01165   0.0000   1.0000   0.0325
  -3.750  -0.3754   0.02043   0.01070   0.0014   1.0000   0.0341
  -3.500  -0.3550   0.01960   0.00985   0.0027   1.0000   0.0362
  -3.250  -0.3344   0.01898   0.00914   0.0041   1.0000   0.0399
  -3.000  -0.3143   0.01826   0.00847   0.0053   1.0000   0.0448
  -2.750  -0.2932   0.01769   0.00781   0.0065   1.0000   0.0502
  -2.500  -0.2660   0.01702   0.00721   0.0063   0.9978   0.0650
  -2.250  -0.2308   0.01581   0.00658   0.0043   0.9921   0.1638
  -2.000  -0.2076   0.01342   0.00651   0.0049   0.9875   0.6616
  -1.750  -0.1701   0.01347   0.00716   0.0058   0.9834   0.8761
  -1.500  -0.0823   0.01420   0.00769  -0.0035   0.9851   0.9690
  -1.250  -0.0148   0.01411   0.00737  -0.0114   0.9727   0.9757
  -1.000   0.0405   0.01396   0.00703  -0.0170   0.9592   0.9815
  -0.750   0.0906   0.01379   0.00673  -0.0216   0.9443   0.9872
  -0.500   0.1376   0.01360   0.00643  -0.0255   0.9263   0.9929
  -0.250   0.1826   0.01339   0.00613  -0.0290   0.9041   0.9981
   0.000   0.2170   0.01320   0.00585  -0.0302   0.8775   1.0000
   0.250   0.2440   0.01304   0.00558  -0.0298   0.8464   1.0000
   0.500   0.2693   0.01292   0.00534  -0.0290   0.8112   1.0000
   0.750   0.2933   0.01284   0.00511  -0.0278   0.7718   1.0000
   1.000   0.3165   0.01283   0.00491  -0.0265   0.7258   1.0000
   1.250   0.3395   0.01290   0.00474  -0.0252   0.6731   1.0000
   1.500   0.3620   0.01306   0.00462  -0.0238   0.6151   1.0000
   1.750   0.3837   0.01332   0.00456  -0.0225   0.5532   1.0000
   2.000   0.4052   0.01365   0.00457  -0.0212   0.4951   1.0000
   2.250   0.4266   0.01401   0.00463  -0.0201   0.4450   1.0000
   2.500   0.4481   0.01437   0.00475  -0.0190   0.4047   1.0000
   2.750   0.4698   0.01473   0.00491  -0.0179   0.3730   1.0000
   3.000   0.4916   0.01508   0.00509  -0.0169   0.3476   1.0000
   3.250   0.5137   0.01542   0.00531  -0.0160   0.3266   1.0000
   3.500   0.5358   0.01576   0.00554  -0.0150   0.3090   1.0000
   3.750   0.5580   0.01611   0.00582  -0.0140   0.2938   1.0000
   4.000   0.5802   0.01647   0.00610  -0.0131   0.2805   1.0000
   4.250   0.6024   0.01685   0.00640  -0.0121   0.2690   1.0000
   4.500   0.6249   0.01721   0.00673  -0.0112   0.2579   1.0000
   4.750   0.6474   0.01759   0.00711  -0.0103   0.2478   1.0000
   5.000   0.6695   0.01802   0.00747  -0.0094   0.2391   1.0000
   5.250   0.6924   0.01841   0.00790  -0.0085   0.2302   1.0000
   5.500   0.7148   0.01887   0.00834  -0.0077   0.2228   1.0000
   5.750   0.7377   0.01929   0.00881  -0.0068   0.2146   1.0000
   6.000   0.7603   0.01978   0.00928  -0.0060   0.2078   1.0000
   6.250   0.7835   0.02025   0.00983  -0.0053   0.2009   1.0000
   6.500   0.8060   0.02079   0.01035  -0.0045   0.1952   1.0000
   6.750   0.8293   0.02129   0.01098  -0.0038   0.1884   1.0000
   7.000   0.8521   0.02181   0.01153  -0.0031   0.1825   1.0000
   7.250   0.8750   0.02242   0.01223  -0.0024   0.1772   1.0000
   7.500   0.8980   0.02302   0.01295  -0.0017   0.1717   1.0000
   7.750   0.9206   0.02362   0.01356  -0.0010   0.1669   1.0000
   8.000   0.9432   0.02429   0.01441  -0.0003   0.1614   1.0000
   8.250   0.9655   0.02495   0.01520   0.0004   0.1563   1.0000
   8.500   0.9878   0.02565   0.01591   0.0011   0.1524   1.0000
   8.750   1.0094   0.02643   0.01695   0.0019   0.1471   1.0000
   9.000   1.0306   0.02710   0.01775   0.0027   0.1418   1.0000
   9.250   1.0513   0.02776   0.01848   0.0035   0.1368   1.0000
   9.500   1.0707   0.02842   0.01941   0.0045   0.1300   1.0000
   9.750   1.0900   0.02893   0.01992   0.0054   0.1246   1.0000
  10.000   1.1083   0.02976   0.02108   0.0065   0.1181   1.0000
  10.250   1.1262   0.03036   0.02177   0.0076   0.1127   1.0000
  10.500   1.1428   0.03125   0.02293   0.0088   0.1064   1.0000
  10.750   1.1585   0.03193   0.02372   0.0100   0.1004   1.0000
  11.000   1.1728   0.03292   0.02496   0.0114   0.0939   1.0000
  11.250   1.1855   0.03372   0.02586   0.0129   0.0878   1.0000
  11.500   1.1964   0.03497   0.02737   0.0145   0.0812   1.0000
  11.750   1.2045   0.03603   0.02851   0.0163   0.0757   1.0000
  12.000   1.2092   0.03758   0.03030   0.0184   0.0700   1.0000
  12.250   1.2106   0.03906   0.03189   0.0206   0.0657   1.0000
  12.500   1.2095   0.04106   0.03405   0.0225   0.0618   1.0000
  12.750   1.2068   0.04334   0.03653   0.0239   0.0581   1.0000
  13.000   1.2014   0.04594   0.03923   0.0247   0.0556   1.0000
  13.250   1.1932   0.04923   0.04264   0.0248   0.0535   1.0000
  13.500   1.1825   0.05331   0.04697   0.0240   0.0516   1.0000
  13.750   1.1690   0.05818   0.05206   0.0221   0.0501   1.0000
  14.000   1.1525   0.06404   0.05811   0.0190   0.0491   1.0000
  14.250   1.1324   0.07107   0.06532   0.0148   0.0485   1.0000
  14.500   1.1080   0.07933   0.07376   0.0099   0.0483   1.0000
  14.750   1.0774   0.08906   0.08367   0.0043   0.0485   1.0000
  15.000   1.0339   0.10168   0.09649  -0.0027   0.0494   1.0000
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