Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

TsAGI R-3a (12%) (tsagi-r-3a-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: TsAGI R-3a (12%) (tsagi-r-3a-il)
Reynolds number: 100,000
Max Cl/Cd: 32.99 at α=8°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-tsagi-r-3a-il-100000.txt
Download as CSV file: xf-tsagi-r-3a-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: TsAGI R-3a (12%)                                
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.500  -0.4152   0.10167   0.09721   0.0054   1.0045   0.1049
  -8.250  -0.4302   0.09837   0.09401  -0.0023   1.0045   0.1091
  -8.000  -0.4492   0.09321   0.08893  -0.0129   1.0045   0.1104
  -7.750  -0.4148   0.09011   0.08587  -0.0033   1.0045   0.1128
  -7.500  -0.4035   0.08704   0.08285  -0.0031   1.0045   0.1161
  -7.250  -0.4037   0.08341   0.07930  -0.0068   1.0045   0.1204
  -7.000  -0.4180   0.07710   0.07292  -0.0199   1.0045   0.1256
  -6.750  -0.3982   0.07433   0.07029  -0.0156   1.0045   0.1281
  -6.500  -0.3856   0.07146   0.06747  -0.0157   1.0045   0.1335
  -6.250  -0.3865   0.06621   0.06210  -0.0232   1.0045   0.1421
  -6.000  -0.3690   0.06378   0.05983  -0.0205   1.0045   0.1465
  -5.750  -0.3642   0.05979   0.05566  -0.0252   1.0045   0.1586
  -5.500  -0.3483   0.05710   0.05318  -0.0231   1.0045   0.1627
  -5.250  -0.3438   0.05426   0.05025  -0.0250   1.0045   0.1759
  -5.000  -0.2939   0.04969   0.04560  -0.0328   0.9581   0.1937
  -4.750  -0.2520   0.04589   0.04161  -0.0370   0.8757   0.2121
  -4.500  -0.2079   0.02927   0.02205  -0.0412   0.8491   0.0736
  -4.250  -0.1848   0.02737   0.01957  -0.0393   0.7917   0.0732
  -4.000  -0.1606   0.02593   0.01746  -0.0376   0.7523   0.0748
  -3.750  -0.1364   0.02461   0.01599  -0.0366   0.7218   0.0778
  -3.500  -0.1103   0.02343   0.01447  -0.0355   0.6970   0.0804
  -3.250  -0.0831   0.02232   0.01294  -0.0345   0.6766   0.0839
  -3.000  -0.0567   0.02128   0.01182  -0.0337   0.6584   0.0903
  -2.750  -0.0300   0.02045   0.01092  -0.0329   0.6422   0.1018
  -2.500  -0.0033   0.01968   0.01012  -0.0322   0.6289   0.1186
  -2.250   0.0225   0.01911   0.00956  -0.0316   0.6176   0.1454
  -2.000   0.0481   0.01826   0.00892  -0.0308   0.6058   0.1831
  -1.750   0.0705   0.01680   0.00821  -0.0298   0.5961   0.3114
  -1.500   0.0882   0.01493   0.00843  -0.0250   0.5864   0.8565
  -1.250   0.1802   0.01519   0.00826  -0.0353   0.5697   0.9955
  -1.000   0.2042   0.01536   0.00814  -0.0347   0.5601   0.9955
  -0.750   0.2284   0.01551   0.00806  -0.0341   0.5495   0.9955
  -0.500   0.2529   0.01572   0.00806  -0.0335   0.5390   0.9955
  -0.250   0.2771   0.01595   0.00802  -0.0328   0.5290   0.9955
   0.000   0.3019   0.01618   0.00812  -0.0322   0.5174   0.9955
   0.250   0.3265   0.01647   0.00817  -0.0315   0.5077   0.9955
   0.500   0.3513   0.01673   0.00832  -0.0309   0.4961   0.9955
   0.750   0.3762   0.01707   0.00851  -0.0302   0.4850   0.9955
   1.000   0.4011   0.01739   0.00860  -0.0295   0.4749   0.9955
   1.250   0.4262   0.01774   0.00889  -0.0290   0.4626   0.9955
   1.500   0.4514   0.01813   0.00912  -0.0284   0.4524   0.9955
   1.750   0.4768   0.01849   0.00934  -0.0278   0.4422   0.9955
   2.000   0.5022   0.01899   0.00978  -0.0273   0.4325   0.9955
   2.250   0.5280   0.01942   0.01008  -0.0269   0.4243   0.9955
   2.500   0.5535   0.02000   0.01063  -0.0265   0.4163   0.9955
   2.750   0.5792   0.02048   0.01105  -0.0261   0.4085   0.9955
   3.000   0.6050   0.02102   0.01146  -0.0257   0.4024   0.9955
   3.250   0.6301   0.02161   0.01213  -0.0254   0.3944   0.9955
   3.500   0.6562   0.02208   0.01250  -0.0250   0.3890   0.9955
   3.750   0.6814   0.02279   0.01324  -0.0247   0.3835   0.9955
   4.000   0.7063   0.02344   0.01396  -0.0244   0.3769   0.9955
   4.250   0.7325   0.02385   0.01428  -0.0240   0.3719   0.9955
   4.500   0.7571   0.02454   0.01502  -0.0236   0.3663   0.9955
   4.750   0.7816   0.02514   0.01570  -0.0233   0.3597   0.9955
   5.000   0.8080   0.02543   0.01588  -0.0229   0.3549   0.9955
   5.250   0.8318   0.02620   0.01675  -0.0225   0.3495   0.9955
   5.500   0.8555   0.02691   0.01756  -0.0221   0.3436   0.9955
   5.750   0.8818   0.02720   0.01777  -0.0217   0.3391   0.9955
   6.000   0.9056   0.02794   0.01857  -0.0213   0.3342   0.9955
   6.250   0.9276   0.02885   0.01965  -0.0209   0.3281   0.9955
   6.500   0.9539   0.02907   0.01981  -0.0204   0.3236   0.9955
   6.750   0.9776   0.02977   0.02053  -0.0200   0.3189   0.9955
   7.000   0.9976   0.03089   0.02188  -0.0195   0.3126   0.9955
   7.250   1.0239   0.03109   0.02202  -0.0190   0.3082   0.9955
   7.500   1.0467   0.03188   0.02285  -0.0185   0.3034   0.9955
   7.750   1.0649   0.03309   0.02428  -0.0179   0.2969   0.9955
   8.000   1.0925   0.03312   0.02422  -0.0175   0.2924   0.9955
   8.250   1.1108   0.03447   0.02573  -0.0168   0.2872   0.9955
   8.500   1.1269   0.03597   0.02744  -0.0160   0.2813   0.9955
   8.750   1.1546   0.03608   0.02747  -0.0157   0.2771   0.9955
   9.000   1.1690   0.03786   0.02943  -0.0148   0.2719   0.9955
   9.250   1.1788   0.03993   0.03175  -0.0138   0.2658   0.9955
   9.500   1.2070   0.04003   0.03177  -0.0135   0.2617   0.9955
   9.750   1.2242   0.04163   0.03345  -0.0128   0.2577   0.9955
  10.000   1.1962   0.04751   0.03993  -0.0109   0.2519   0.9955
  10.250   1.2052   0.04954   0.04206  -0.0101   0.2480   0.9955
  10.500   1.2489   0.04827   0.04064  -0.0099   0.2449   0.9955
  10.750   0.7779   0.13115   0.12420  -0.0494   0.2907   0.9955
  11.000   0.7348   0.13513   0.12816  -0.0531   0.2825   0.9955
<< Back to TsAGI R-3a (12%) (tsagi-r-3a-il)

Polar data table (+)

Polar graphs


<< Back to TsAGI R-3a (12%) (tsagi-r-3a-il)