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RG 14 10% AIRFOIL (rg1410-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: RG 14 10% AIRFOIL (rg1410-il)
Reynolds number: 500,000
Max Cl/Cd: 82.26 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rg1410-il-500000.txt
Download as CSV file: xf-rg1410-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RG 14 10% 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.7199   0.05362   0.05091  -0.0556   1.0000   0.0153
 -11.000  -0.7365   0.04933   0.04647  -0.0580   1.0000   0.0152
 -10.750  -0.7594   0.04581   0.04279  -0.0570   1.0000   0.0152
 -10.500  -0.7850   0.04291   0.03971  -0.0529   1.0000   0.0152
 -10.250  -0.8025   0.03945   0.03601  -0.0495   1.0000   0.0153
 -10.000  -0.8164   0.03573   0.03199  -0.0460   1.0000   0.0154
  -9.750  -0.8201   0.03279   0.02881  -0.0428   1.0000   0.0157
  -9.500  -0.8136   0.03108   0.02697  -0.0405   1.0000   0.0160
  -9.250  -0.8064   0.02925   0.02495  -0.0380   1.0000   0.0163
  -9.000  -0.7959   0.02779   0.02333  -0.0358   1.0000   0.0167
  -8.750  -0.7846   0.02632   0.02168  -0.0335   1.0000   0.0171
  -8.500  -0.7723   0.02491   0.02008  -0.0313   1.0000   0.0177
  -8.250  -0.7601   0.02326   0.01819  -0.0289   1.0000   0.0182
  -8.000  -0.7450   0.02216   0.01688  -0.0269   1.0000   0.0189
  -7.750  -0.7274   0.02179   0.01634  -0.0251   1.0000   0.0196
  -7.500  -0.7156   0.01917   0.01349  -0.0229   1.0000   0.0206
  -7.250  -0.6982   0.01837   0.01264  -0.0213   1.0000   0.0214
  -7.000  -0.6772   0.01764   0.01183  -0.0203   0.9997   0.0222
  -6.750  -0.6432   0.01674   0.01082  -0.0219   0.9974   0.0233
  -6.500  -0.6081   0.01603   0.01000  -0.0236   0.9951   0.0245
  -6.250  -0.5747   0.01510   0.00894  -0.0250   0.9928   0.0259
  -6.000  -0.5430   0.01405   0.00785  -0.0262   0.9896   0.0275
  -5.750  -0.5082   0.01347   0.00723  -0.0278   0.9867   0.0290
  -5.500  -0.4719   0.01299   0.00671  -0.0297   0.9845   0.0310
  -5.250  -0.4379   0.01254   0.00619  -0.0311   0.9815   0.0327
  -5.000  -0.4069   0.01174   0.00538  -0.0320   0.9770   0.0358
  -4.750  -0.3713   0.01134   0.00496  -0.0336   0.9740   0.0393
  -4.500  -0.3344   0.01082   0.00445  -0.0356   0.9717   0.0471
  -4.250  -0.3025   0.01035   0.00404  -0.0365   0.9670   0.0631
  -4.000  -0.2688   0.00989   0.00370  -0.0378   0.9625   0.0897
  -3.750  -0.2319   0.00946   0.00340  -0.0399   0.9596   0.1206
  -3.500  -0.1939   0.00902   0.00314  -0.0421   0.9574   0.1626
  -3.250  -0.1652   0.00861   0.00291  -0.0424   0.9503   0.2090
  -3.000  -0.1317   0.00814   0.00268  -0.0437   0.9454   0.2707
  -2.750  -0.1018   0.00761   0.00248  -0.0443   0.9387   0.3595
  -2.500  -0.0728   0.00705   0.00228  -0.0447   0.9307   0.4608
  -2.250  -0.0456   0.00659   0.00213  -0.0445   0.9210   0.5502
  -2.000  -0.0186   0.00613   0.00200  -0.0442   0.9111   0.6487
  -1.750   0.0066   0.00585   0.00200  -0.0432   0.8993   0.7344
  -1.500   0.0322   0.00578   0.00201  -0.0422   0.8863   0.7860
  -1.250   0.0583   0.00576   0.00201  -0.0414   0.8729   0.8170
  -1.000   0.0844   0.00577   0.00200  -0.0406   0.8589   0.8396
  -0.750   0.1101   0.00580   0.00200  -0.0397   0.8442   0.8571
  -0.500   0.1356   0.00583   0.00199  -0.0388   0.8288   0.8719
  -0.250   0.1607   0.00588   0.00198  -0.0378   0.8122   0.8852
   0.000   0.1853   0.00595   0.00197  -0.0367   0.7939   0.8977
   0.250   0.2093   0.00600   0.00199  -0.0354   0.7737   0.9091
   0.500   0.2335   0.00607   0.00199  -0.0342   0.7540   0.9195
   0.750   0.2578   0.00615   0.00200  -0.0331   0.7354   0.9295
   1.000   0.2826   0.00624   0.00203  -0.0321   0.7165   0.9390
   1.250   0.3087   0.00634   0.00205  -0.0314   0.6941   0.9478
   1.500   0.3344   0.00646   0.00208  -0.0306   0.6715   0.9571
   1.750   0.3671   0.00659   0.00213  -0.0315   0.6496   0.9624
   2.000   0.3973   0.00673   0.00219  -0.0318   0.6267   0.9694
   2.250   0.4340   0.00690   0.00226  -0.0337   0.6016   0.9736
   2.500   0.4722   0.00707   0.00233  -0.0359   0.5754   0.9771
   2.750   0.5061   0.00726   0.00242  -0.0372   0.5464   0.9818
   3.000   0.5419   0.00747   0.00249  -0.0390   0.5131   0.9852
   3.250   0.5781   0.00767   0.00258  -0.0409   0.4814   0.9884
   3.750   0.6464   0.00811   0.00279  -0.0440   0.4194   0.9955
   4.000   0.6808   0.00835   0.00291  -0.0457   0.3849   0.9986
   4.250   0.7066   0.00859   0.00304  -0.0455   0.3534   1.0000
   4.500   0.7232   0.00883   0.00318  -0.0435   0.3247   1.0000
   4.750   0.7388   0.00912   0.00334  -0.0413   0.2927   1.0000
   5.000   0.7541   0.00946   0.00354  -0.0390   0.2597   1.0000
   5.250   0.7704   0.00984   0.00377  -0.0369   0.2251   1.0000
   5.500   0.7881   0.01025   0.00403  -0.0351   0.1925   1.0000
   5.750   0.8072   0.01067   0.00432  -0.0335   0.1686   1.0000
   6.000   0.8281   0.01105   0.00462  -0.0323   0.1517   1.0000
   6.250   0.8499   0.01141   0.00495  -0.0313   0.1373   1.0000
   6.500   0.8722   0.01178   0.00527  -0.0303   0.1227   1.0000
   6.750   0.8948   0.01215   0.00560  -0.0295   0.1087   1.0000
   7.000   0.9172   0.01255   0.00595  -0.0286   0.0960   1.0000
   7.250   0.9394   0.01298   0.00636  -0.0277   0.0852   1.0000
   7.500   0.9605   0.01352   0.00684  -0.0266   0.0757   1.0000
   7.750   0.9836   0.01388   0.00723  -0.0259   0.0691   1.0000
   8.000   1.0049   0.01439   0.00773  -0.0249   0.0618   1.0000
   8.250   1.0270   0.01483   0.00817  -0.0240   0.0553   1.0000
   8.500   1.0482   0.01534   0.00872  -0.0230   0.0499   1.0000
   8.750   1.0696   0.01582   0.00920  -0.0221   0.0450   1.0000
   9.000   1.0894   0.01644   0.00985  -0.0209   0.0406   1.0000
   9.250   1.1110   0.01688   0.01031  -0.0200   0.0368   1.0000
   9.500   1.1278   0.01771   0.01117  -0.0184   0.0330   1.0000
   9.750   1.1490   0.01815   0.01168  -0.0175   0.0303   1.0000
  10.000   1.1666   0.01885   0.01238  -0.0161   0.0273   1.0000
  10.250   1.1829   0.01962   0.01323  -0.0144   0.0245   1.0000
  10.500   1.2010   0.02022   0.01387  -0.0131   0.0221   1.0000
  10.750   1.2088   0.02146   0.01514  -0.0104   0.0200   1.0000
  11.000   1.2239   0.02206   0.01587  -0.0085   0.0187   1.0000
  11.250   1.2355   0.02286   0.01673  -0.0062   0.0174   1.0000
  11.500   1.2444   0.02381   0.01774  -0.0038   0.0164   1.0000
  11.750   1.2415   0.02558   0.01959  -0.0001   0.0154   1.0000
  12.000   1.2502   0.02664   0.02076   0.0021   0.0150   1.0000
  12.250   1.2583   0.02776   0.02201   0.0041   0.0143   1.0000
  12.500   1.2645   0.02905   0.02340   0.0060   0.0137   1.0000
  12.750   1.2706   0.03037   0.02481   0.0077   0.0131   1.0000
  13.000   1.2751   0.03189   0.02643   0.0092   0.0127   1.0000
  13.250   1.2754   0.03386   0.02850   0.0107   0.0124   1.0000
  13.500   1.2694   0.03656   0.03129   0.0120   0.0119   1.0000
  13.750   1.2603   0.03986   0.03475   0.0130   0.0116   1.0000
  14.000   1.2625   0.04214   0.03717   0.0132   0.0114   1.0000
  14.250   1.2598   0.04512   0.04031   0.0132   0.0111   1.0000
  14.500   1.2553   0.04848   0.04381   0.0128   0.0111   1.0000
  14.750   1.2507   0.05206   0.04754   0.0119   0.0109   1.0000
  15.000   1.2439   0.05614   0.05178   0.0106   0.0106   1.0000
  15.250   1.2357   0.06062   0.05640   0.0089   0.0105   1.0000
  15.500   1.2255   0.06561   0.06155   0.0067   0.0105   1.0000
  15.750   1.2160   0.07079   0.06687   0.0041   0.0103   1.0000
  16.000   1.2013   0.07701   0.07326   0.0010   0.0103   1.0000
  16.250   1.1882   0.08331   0.07971  -0.0024   0.0102   1.0000
  16.500   1.1735   0.09015   0.08670  -0.0063   0.0101   1.0000
  16.750   1.1589   0.09727   0.09396  -0.0104   0.0101   1.0000
  17.000   1.1388   0.10571   0.10257  -0.0152   0.0102   1.0000
  17.250   1.1208   0.11412   0.11113  -0.0202   0.0102   1.0000
  17.500   1.0990   0.12367   0.12083  -0.0259   0.0102   1.0000
  17.750   1.0738   0.13447   0.13180  -0.0324   0.0104   1.0000
  18.000   1.0410   0.14783   0.14534  -0.0404   0.0106   1.0000
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