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S8052 (11.88%) (s8052-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: S8052 (11.88%) (s8052-il)
Reynolds number: 200,000
Max Cl/Cd: 58.56 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8052-il-200000-n5.txt
Download as CSV file: xf-s8052-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8052 (11.88%)                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.6429   0.06586   0.06191  -0.0435   1.0000   0.0134
 -11.000  -0.6638   0.05915   0.05505  -0.0487   1.0000   0.0133
 -10.750  -0.6859   0.05370   0.04942  -0.0518   1.0000   0.0133
 -10.500  -0.7008   0.04995   0.04552  -0.0527   1.0000   0.0133
 -10.250  -0.7184   0.04656   0.04192  -0.0518   1.0000   0.0133
 -10.000  -0.7303   0.04387   0.03904  -0.0495   1.0000   0.0132
  -9.750  -0.7376   0.04078   0.03564  -0.0475   1.0000   0.0133
  -9.500  -0.7389   0.03791   0.03246  -0.0455   1.0000   0.0133
  -9.250  -0.7355   0.03533   0.02955  -0.0436   1.0000   0.0133
  -9.000  -0.7289   0.03308   0.02698  -0.0416   1.0000   0.0134
  -8.750  -0.7182   0.03091   0.02458  -0.0402   0.9969   0.0135
  -8.500  -0.6920   0.02857   0.02198  -0.0416   0.9796   0.0137
  -8.250  -0.6636   0.02671   0.01992  -0.0429   0.9662   0.0140
  -8.000  -0.6344   0.02512   0.01812  -0.0442   0.9542   0.0144
  -7.750  -0.6059   0.02373   0.01655  -0.0450   0.9425   0.0148
  -7.500  -0.5791   0.02251   0.01515  -0.0454   0.9310   0.0151
  -7.250  -0.5533   0.02154   0.01403  -0.0454   0.9198   0.0160
  -7.000  -0.5278   0.02067   0.01300  -0.0451   0.9096   0.0169
  -6.750  -0.5040   0.01978   0.01197  -0.0446   0.8994   0.0175
  -6.500  -0.4821   0.01878   0.01091  -0.0438   0.8900   0.0181
  -6.250  -0.4595   0.01804   0.01010  -0.0430   0.8818   0.0187
  -6.000  -0.4370   0.01737   0.00936  -0.0422   0.8730   0.0195
  -5.750  -0.4140   0.01677   0.00865  -0.0413   0.8660   0.0204
  -5.500  -0.3906   0.01621   0.00798  -0.0406   0.8581   0.0217
  -5.250  -0.3673   0.01563   0.00731  -0.0398   0.8517   0.0235
  -5.000  -0.3430   0.01515   0.00677  -0.0392   0.8448   0.0265
  -4.750  -0.3190   0.01464   0.00624  -0.0385   0.8387   0.0340
  -4.500  -0.2952   0.01408   0.00576  -0.0379   0.8330   0.0537
  -4.250  -0.2712   0.01356   0.00536  -0.0374   0.8268   0.0852
  -4.000  -0.2473   0.01305   0.00502  -0.0368   0.8218   0.1305
  -3.750  -0.2252   0.01232   0.00473  -0.0363   0.8159   0.2196
  -3.500  -0.2029   0.01167   0.00447  -0.0356   0.8103   0.3126
  -3.250  -0.1798   0.01118   0.00423  -0.0348   0.8057   0.3932
  -3.000  -0.1570   0.01071   0.00410  -0.0340   0.7997   0.4786
  -2.750  -0.1336   0.01041   0.00408  -0.0329   0.7943   0.5597
  -2.500  -0.1084   0.01030   0.00406  -0.0321   0.7896   0.6133
  -2.250  -0.0823   0.01025   0.00405  -0.0315   0.7835   0.6495
  -2.000  -0.0560   0.01023   0.00402  -0.0309   0.7782   0.6764
  -1.750  -0.0293   0.01023   0.00398  -0.0304   0.7733   0.6981
  -1.500  -0.0026   0.01022   0.00397  -0.0299   0.7673   0.7160
  -1.250   0.0242   0.01022   0.00394  -0.0294   0.7620   0.7324
  -1.000   0.0510   0.01022   0.00392  -0.0290   0.7561   0.7472
  -0.750   0.0778   0.01022   0.00389  -0.0285   0.7496   0.7608
  -0.500   0.1048   0.01022   0.00384  -0.0281   0.7442   0.7736
  -0.250   0.1314   0.01022   0.00386  -0.0276   0.7368   0.7847
   0.000   0.1583   0.01020   0.00381  -0.0271   0.7304   0.7957
   0.250   0.1849   0.01020   0.00381  -0.0267   0.7222   0.8069
   0.500   0.2116   0.01018   0.00376  -0.0262   0.7147   0.8180
   0.750   0.2379   0.01016   0.00377  -0.0256   0.7050   0.8284
   1.000   0.2644   0.01014   0.00373  -0.0251   0.6959   0.8389
   1.250   0.2908   0.01013   0.00371  -0.0246   0.6857   0.8498
   1.500   0.3173   0.01010   0.00371  -0.0240   0.6745   0.8590
   1.750   0.3440   0.01009   0.00369  -0.0236   0.6630   0.8685
   2.000   0.3709   0.01008   0.00368  -0.0232   0.6507   0.8782
   2.250   0.3981   0.01007   0.00367  -0.0229   0.6361   0.8877
   2.500   0.4255   0.01007   0.00367  -0.0226   0.6188   0.8980
   2.750   0.4538   0.01009   0.00368  -0.0225   0.5995   0.9089
   3.000   0.4834   0.01014   0.00367  -0.0227   0.5783   0.9196
   3.250   0.5139   0.01023   0.00370  -0.0232   0.5538   0.9308
   3.500   0.5452   0.01038   0.00377  -0.0239   0.5257   0.9426
   3.750   0.5777   0.01059   0.00386  -0.0249   0.4949   0.9545
   4.000   0.6106   0.01087   0.00399  -0.0262   0.4605   0.9665
   4.250   0.6433   0.01119   0.00417  -0.0275   0.4242   0.9798
   4.500   0.6763   0.01158   0.00441  -0.0290   0.3878   0.9933
   4.750   0.7021   0.01199   0.00466  -0.0291   0.3539   1.0000
   5.000   0.7207   0.01240   0.00492  -0.0277   0.3240   1.0000
   5.250   0.7401   0.01283   0.00522  -0.0264   0.2963   1.0000
   5.500   0.7606   0.01326   0.00553  -0.0254   0.2712   1.0000
   5.750   0.7814   0.01370   0.00587  -0.0244   0.2507   1.0000
   6.000   0.8029   0.01411   0.00622  -0.0235   0.2326   1.0000
   6.250   0.8244   0.01453   0.00660  -0.0226   0.2158   1.0000
   6.500   0.8459   0.01497   0.00699  -0.0218   0.2006   1.0000
   6.750   0.8674   0.01541   0.00739  -0.0209   0.1872   1.0000
   7.000   0.8887   0.01588   0.00783  -0.0201   0.1744   1.0000
   7.250   0.9097   0.01636   0.00827  -0.0192   0.1622   1.0000
   7.500   0.9308   0.01683   0.00873  -0.0183   0.1509   1.0000
   7.750   0.9518   0.01729   0.00920  -0.0175   0.1404   1.0000
   8.000   0.9722   0.01780   0.00972  -0.0165   0.1309   1.0000
   8.250   0.9915   0.01837   0.01026  -0.0155   0.1214   1.0000
   8.500   1.0119   0.01886   0.01079  -0.0146   0.1126   1.0000
   8.750   1.0308   0.01943   0.01138  -0.0135   0.1044   1.0000
   9.000   1.0488   0.02004   0.01199  -0.0123   0.0962   1.0000
   9.250   1.0669   0.02063   0.01264  -0.0111   0.0890   1.0000
   9.500   1.0823   0.02135   0.01334  -0.0097   0.0827   1.0000
   9.750   1.0979   0.02198   0.01405  -0.0081   0.0775   1.0000
  10.000   1.1106   0.02274   0.01482  -0.0063   0.0726   1.0000
  10.250   1.1227   0.02356   0.01568  -0.0044   0.0687   1.0000
  10.500   1.1359   0.02436   0.01658  -0.0029   0.0645   1.0000
  10.750   1.1468   0.02531   0.01756  -0.0012   0.0610   1.0000
  11.000   1.1562   0.02641   0.01870   0.0005   0.0582   1.0000
  11.250   1.1681   0.02740   0.01981   0.0018   0.0559   1.0000
  11.500   1.1788   0.02850   0.02101   0.0032   0.0535   1.0000
  11.750   1.1880   0.02973   0.02231   0.0045   0.0514   1.0000
  12.000   1.1946   0.03119   0.02381   0.0058   0.0495   1.0000
  12.250   1.2018   0.03268   0.02538   0.0070   0.0479   1.0000
  12.500   1.2113   0.03404   0.02689   0.0079   0.0463   1.0000
  12.750   1.2193   0.03555   0.02853   0.0088   0.0447   1.0000
  13.000   1.2262   0.03718   0.03028   0.0096   0.0434   1.0000
  13.250   1.2320   0.03896   0.03215   0.0104   0.0422   1.0000
  13.500   1.2358   0.04092   0.03417   0.0109   0.0407   1.0000
  13.750   1.2376   0.04319   0.03652   0.0115   0.0398   1.0000
  14.000   1.2414   0.04533   0.03880   0.0118   0.0384   1.0000
  14.250   1.2454   0.04751   0.04114   0.0119   0.0371   1.0000
  14.500   1.2482   0.04985   0.04364   0.0118   0.0356   1.0000
  14.750   1.2493   0.05247   0.04639   0.0115   0.0344   1.0000
  15.000   1.2486   0.05538   0.04941   0.0109   0.0332   1.0000
  15.250   1.2451   0.05874   0.05286   0.0100   0.0321   1.0000
  15.500   1.2399   0.06249   0.05668   0.0090   0.0312   1.0000
  15.750   1.2382   0.06609   0.06049   0.0077   0.0301   1.0000
  16.000   1.2340   0.07014   0.06472   0.0061   0.0294   1.0000
  16.250   1.2287   0.07453   0.06928   0.0041   0.0284   1.0000
  16.500   1.2214   0.07942   0.07433   0.0018   0.0275   1.0000
  16.750   1.2130   0.08466   0.07972  -0.0008   0.0269   1.0000
  17.000   1.2029   0.09038   0.08557  -0.0038   0.0264   1.0000
  17.250   1.1911   0.09657   0.09189  -0.0073   0.0258   1.0000
  17.500   1.1781   0.10314   0.09858  -0.0109   0.0253   1.0000
  17.750   1.1652   0.10981   0.10537  -0.0146   0.0250   1.0000
  18.000   1.1517   0.11671   0.11235  -0.0185   0.0245   1.0000
  18.250   1.1360   0.12438   0.12020  -0.0230   0.0243   1.0000
  18.500   1.1180   0.13278   0.12878  -0.0280   0.0240   1.0000
  18.750   1.0983   0.14179   0.13795  -0.0334   0.0237   1.0000
  19.000   1.0742   0.15217   0.14850  -0.0397   0.0236   1.0000
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