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WORTMANN FX 60-126/1 AIRFOIL (fx601261-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 60-126/1 AIRFOIL (fx601261-il)
Reynolds number: 1,000,000
Max Cl/Cd: 88.21 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx601261-il-1000000-n5.txt
Download as CSV file: xf-fx601261-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 60-126/1 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.3535   0.11180   0.11008  -0.0348   1.0000   0.0047
 -11.000  -0.3528   0.10756   0.10586  -0.0360   1.0000   0.0047
 -10.750  -0.3525   0.10335   0.10166  -0.0372   1.0000   0.0047
 -10.500  -0.2439   0.07644   0.07481  -0.0578   0.9543   0.0047
 -10.250  -0.2308   0.07104   0.06940  -0.0642   0.9443   0.0045
 -10.000  -0.2536   0.05634   0.05465  -0.0723   0.9392   0.0042
  -9.750  -0.3530   0.07761   0.07596  -0.0532   0.9825   0.0046
  -9.500  -0.3670   0.06482   0.06313  -0.0640   0.9566   0.0042
  -9.250  -0.3610   0.04479   0.04269  -0.0960   0.9316   0.0041
  -9.000  -0.3419   0.03283   0.03005  -0.1232   0.8831   0.0039
  -8.750  -0.3389   0.02964   0.02653  -0.1259   0.8607   0.0038
  -8.500  -0.3325   0.02653   0.02305  -0.1269   0.8454   0.0038
  -8.250  -0.3190   0.02407   0.02027  -0.1274   0.8336   0.0037
  -8.000  -0.3013   0.02197   0.01789  -0.1276   0.8238   0.0037
  -7.750  -0.2805   0.02022   0.01588  -0.1278   0.8166   0.0038
  -7.500  -0.2579   0.01872   0.01416  -0.1279   0.8093   0.0039
  -7.250  -0.2338   0.01748   0.01271  -0.1279   0.8032   0.0040
  -7.000  -0.2086   0.01643   0.01149  -0.1280   0.7967   0.0042
  -6.500  -0.1561   0.01500   0.00976  -0.1279   0.7829   0.0045
  -6.250  -0.1282   0.01502   0.00958  -0.1280   0.7751   0.0048
  -6.000  -0.1032   0.01353   0.00802  -0.1279   0.7684   0.0049
  -5.750  -0.0768   0.01277   0.00720  -0.1279   0.7612   0.0050
  -5.500  -0.0498   0.01211   0.00649  -0.1280   0.7544   0.0051
  -5.250  -0.0225   0.01156   0.00589  -0.1281   0.7465   0.0052
  -5.000   0.0051   0.01109   0.00536  -0.1281   0.7380   0.0053
  -4.750   0.0327   0.01068   0.00490  -0.1283   0.7289   0.0056
  -4.500   0.0609   0.01030   0.00447  -0.1284   0.7206   0.0058
  -4.250   0.0891   0.00996   0.00407  -0.1285   0.7123   0.0060
  -4.000   0.1177   0.00962   0.00366  -0.1287   0.7025   0.0059
  -3.750   0.1460   0.00933   0.00330  -0.1288   0.6920   0.0058
  -3.500   0.1745   0.00909   0.00297  -0.1289   0.6814   0.0058
  -3.250   0.2032   0.00887   0.00270  -0.1290   0.6723   0.0057
  -3.000   0.2317   0.00869   0.00245  -0.1291   0.6626   0.0056
  -2.750   0.2602   0.00855   0.00224  -0.1291   0.6513   0.0056
  -2.500   0.2883   0.00845   0.00206  -0.1291   0.6352   0.0056
  -2.250   0.3161   0.00841   0.00191  -0.1289   0.6163   0.0056
  -2.000   0.3437   0.00839   0.00179  -0.1288   0.5955   0.0056
  -1.750   0.3710   0.00842   0.00169  -0.1286   0.5712   0.0057
  -1.500   0.3989   0.00843   0.00161  -0.1285   0.5536   0.0057
  -1.250   0.4267   0.00845   0.00155  -0.1284   0.5375   0.0059
  -1.000   0.4547   0.00848   0.00151  -0.1283   0.5226   0.0062
  -0.750   0.4825   0.00853   0.00148  -0.1282   0.5060   0.0066
  -0.500   0.5107   0.00851   0.00145  -0.1282   0.4919   0.0392
  -0.250   0.5398   0.00817   0.00137  -0.1287   0.4781   0.1624
   0.000   0.5689   0.00776   0.00135  -0.1294   0.4617   0.3198
   0.250   0.5960   0.00784   0.00143  -0.1293   0.4329   0.3632
   0.500   0.6222   0.00803   0.00155  -0.1291   0.3983   0.3980
   0.750   0.6485   0.00826   0.00166  -0.1288   0.3656   0.4117
   1.000   0.6754   0.00844   0.00177  -0.1286   0.3448   0.4255
   1.250   0.7022   0.00862   0.00188  -0.1284   0.3241   0.4378
   1.500   0.7286   0.00885   0.00202  -0.1281   0.2974   0.4481
   1.750   0.7554   0.00904   0.00214  -0.1278   0.2810   0.4585
   2.000   0.7819   0.00925   0.00228  -0.1276   0.2599   0.4655
   2.250   0.8073   0.00959   0.00247  -0.1271   0.2289   0.4731
   2.500   0.8331   0.00987   0.00266  -0.1268   0.2038   0.4816
   2.750   0.8582   0.01022   0.00288  -0.1263   0.1767   0.4906
   3.000   0.8846   0.01044   0.00306  -0.1260   0.1612   0.4987
   3.250   0.9100   0.01075   0.00328  -0.1256   0.1396   0.5063
   3.500   0.9362   0.01098   0.00347  -0.1253   0.1282   0.5145
   3.750   0.9622   0.01122   0.00367  -0.1250   0.1174   0.5223
   4.000   0.9881   0.01146   0.00389  -0.1246   0.1032   0.5300
   4.250   1.0139   0.01172   0.00410  -0.1242   0.0951   0.5379
   4.500   1.0401   0.01192   0.00431  -0.1240   0.0897   0.5464
   4.750   1.0662   0.01213   0.00452  -0.1236   0.0847   0.5554
   5.000   1.0915   0.01241   0.00478  -0.1232   0.0745   0.5646
   5.250   1.1151   0.01284   0.00512  -0.1225   0.0574   0.5741
   5.750   1.1661   0.01330   0.00563  -0.1218   0.0515   0.5988
   6.000   1.1910   0.01357   0.00592  -0.1213   0.0475   0.6118
   6.250   1.2164   0.01379   0.00618  -0.1209   0.0438   0.6251
   6.500   1.2387   0.01428   0.00662  -0.1201   0.0310   0.6391
   6.750   1.2627   0.01460   0.00696  -0.1195   0.0290   0.6549
   7.000   1.2866   0.01491   0.00732  -0.1189   0.0265   0.6746
   7.250   1.3108   0.01518   0.00766  -0.1183   0.0251   0.6998
   7.500   1.3351   0.01541   0.00800  -0.1178   0.0245   0.7358
   7.750   1.3587   0.01564   0.00837  -0.1172   0.0228   0.7884
   8.000   1.3717   0.01578   0.00881  -0.1143   0.0154   1.0000
   8.250   1.3871   0.01673   0.00969  -0.1124   0.0025   1.0000
   8.500   1.4082   0.01716   0.01015  -0.1114   0.0022   1.0000
   8.750   1.4287   0.01762   0.01063  -0.1102   0.0021   1.0000
   9.000   1.4484   0.01810   0.01115  -0.1090   0.0020   1.0000
   9.250   1.4664   0.01861   0.01170  -0.1075   0.0019   1.0000
   9.500   1.4822   0.01913   0.01227  -0.1055   0.0018   1.0000
   9.750   1.4968   0.01970   0.01289  -0.1035   0.0017   1.0000
  10.000   1.5107   0.02030   0.01354  -0.1013   0.0017   1.0000
  10.250   1.5242   0.02094   0.01422  -0.0992   0.0016   1.0000
  10.500   1.5370   0.02163   0.01498  -0.0971   0.0016   1.0000
  10.750   1.5491   0.02239   0.01579  -0.0951   0.0016   1.0000
  11.000   1.5603   0.02323   0.01670  -0.0930   0.0015   1.0000
  11.250   1.5708   0.02415   0.01767  -0.0910   0.0014   1.0000
  11.500   1.5802   0.02519   0.01878  -0.0890   0.0014   1.0000
  11.750   1.5891   0.02632   0.01998  -0.0871   0.0014   1.0000
  12.000   1.5971   0.02758   0.02132  -0.0852   0.0013   1.0000
  12.250   1.6046   0.02893   0.02275  -0.0835   0.0013   1.0000
  12.500   1.6111   0.03044   0.02434  -0.0819   0.0013   1.0000
  12.750   1.6168   0.03209   0.02607  -0.0803   0.0012   1.0000
  13.000   1.6216   0.03388   0.02794  -0.0789   0.0012   1.0000
  13.250   1.6254   0.03585   0.03000  -0.0776   0.0012   1.0000
  13.500   1.6278   0.03803   0.03227  -0.0764   0.0012   1.0000
  13.750   1.6295   0.04037   0.03471  -0.0754   0.0011   1.0000
  14.000   1.6296   0.04301   0.03744  -0.0746   0.0011   1.0000
  14.250   1.6280   0.04593   0.04048  -0.0740   0.0011   1.0000
  14.500   1.6248   0.04917   0.04384  -0.0736   0.0011   1.0000
  14.750   1.6190   0.05292   0.04771  -0.0735   0.0010   1.0000
  15.000   1.6099   0.05729   0.05222  -0.0738   0.0010   1.0000
  15.250   1.5998   0.06206   0.05713  -0.0745   0.0010   1.0000
  15.500   1.5971   0.06596   0.06113  -0.0752   0.0010   1.0000
  15.750   1.5954   0.06984   0.06512  -0.0761   0.0010   1.0000
  16.000   1.5901   0.07440   0.06979  -0.0774   0.0009   1.0000
  16.250   1.5848   0.07913   0.07463  -0.0789   0.0009   1.0000
  16.500   1.5777   0.08432   0.07994  -0.0807   0.0009   1.0000
  16.750   1.5697   0.08977   0.08551  -0.0827   0.0009   1.0000
  17.000   1.5597   0.09575   0.09161  -0.0852   0.0009   1.0000
  17.250   1.5484   0.10213   0.09812  -0.0879   0.0009   1.0000
  17.500   1.5364   0.10880   0.10492  -0.0910   0.0009   1.0000
  17.750   1.5254   0.11537   0.11162  -0.0942   0.0008   1.0000
  18.000   1.5119   0.12259   0.11898  -0.0978   0.0008   1.0000
  18.250   1.4978   0.13009   0.12661  -0.1018   0.0008   1.0000
  18.500   1.4827   0.13788   0.13453  -0.1061   0.0008   1.0000
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