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FX S 03-182 AIRFOIL (fxs03182-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: FX S 03-182 AIRFOIL (fxs03182-il)
Reynolds number: 100,000
Max Cl/Cd: 28.08 at α=9.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxs03182-il-100000-n5.txt
Download as CSV file: xf-fxs03182-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX S 03-182 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
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.4049   0.09688   0.09224  -0.0775   0.9933   0.0143
 -12.750  -0.4258   0.08543   0.08068  -0.0863   0.9835   0.0138
 -12.500  -0.4474   0.07608   0.07114  -0.0940   0.9722   0.0136
 -12.250  -0.4690   0.06794   0.06271  -0.1006   0.9612   0.0137
 -12.000  -0.4765   0.06216   0.05668  -0.1057   0.9521   0.0131
 -11.750  -0.4845   0.05658   0.05076  -0.1100   0.9418   0.0132
 -11.500  -0.4875   0.05183   0.04563  -0.1132   0.9308   0.0132
 -11.250  -0.4858   0.04768   0.04102  -0.1157   0.9203   0.0140
 -11.000  -0.4749   0.04432   0.03727  -0.1177   0.9112   0.0140
 -10.750  -0.4636   0.04138   0.03391  -0.1184   0.9006   0.0145
 -10.500  -0.4462   0.03896   0.03109  -0.1187   0.8915   0.0150
 -10.250  -0.4281   0.03699   0.02896  -0.1192   0.8832   0.0155
 -10.000  -0.4131   0.03551   0.02731  -0.1189   0.8736   0.0162
  -9.750  -0.3937   0.03412   0.02575  -0.1188   0.8663   0.0171
  -9.500  -0.3766   0.03289   0.02436  -0.1181   0.8581   0.0182
  -9.250  -0.3581   0.03162   0.02288  -0.1173   0.8515   0.0201
  -9.000  -0.3438   0.03055   0.02167  -0.1163   0.8437   0.0215
  -8.750  -0.3297   0.02948   0.02056  -0.1155   0.8373   0.0243
  -8.500  -0.3159   0.02869   0.01965  -0.1143   0.8299   0.0279
  -8.250  -0.2987   0.02790   0.01878  -0.1137   0.8246   0.0342
  -8.000  -0.2867   0.02725   0.01807  -0.1122   0.8177   0.0410
  -7.750  -0.2718   0.02658   0.01732  -0.1111   0.8125   0.0472
  -7.500  -0.2597   0.02593   0.01660  -0.1095   0.8072   0.0521
  -7.250  -0.2487   0.02542   0.01602  -0.1076   0.8016   0.0569
  -7.000  -0.2357   0.02490   0.01541  -0.1060   0.7972   0.0637
  -6.750  -0.2271   0.02444   0.01496  -0.1038   0.7920   0.0761
  -6.500  -0.2188   0.02384   0.01448  -0.1017   0.7868   0.0950
  -6.250  -0.2094   0.02307   0.01387  -0.0999   0.7828   0.1266
  -6.000  -0.2074   0.02219   0.01328  -0.0971   0.7780   0.1832
  -5.750  -0.2098   0.02100   0.01259  -0.0940   0.7731   0.2751
  -5.500  -0.2046   0.02011   0.01252  -0.0912   0.7695   0.4206
  -5.250  -0.1754   0.02126   0.01399  -0.0892   0.7674   0.5175
  -5.000  -0.1589   0.02134   0.01391  -0.0881   0.7633   0.5558
  -4.750  -0.1380   0.02179   0.01421  -0.0870   0.7595   0.5839
  -4.500  -0.1135   0.02273   0.01500  -0.0855   0.7564   0.6105
  -4.250  -0.0840   0.02434   0.01656  -0.0831   0.7542   0.6304
  -4.000  -0.0553   0.02536   0.01745  -0.0815   0.7522   0.6444
  -3.750  -0.0409   0.02557   0.01759  -0.0796   0.7480   0.6545
  -3.500  -0.0185   0.02583   0.01774  -0.0784   0.7450   0.6582
  -3.250   0.0040   0.02573   0.01749  -0.0781   0.7425   0.6638
  -3.000   0.0281   0.02543   0.01704  -0.0784   0.7403   0.6689
  -2.750   0.0555   0.02543   0.01691  -0.0784   0.7386   0.6715
  -2.500   0.0724   0.02557   0.01699  -0.0770   0.7350   0.6754
  -2.250   0.0900   0.02537   0.01668  -0.0767   0.7312   0.6823
  -2.000   0.1126   0.02547   0.01672  -0.0760   0.7287   0.6844
  -1.750   0.1375   0.02548   0.01665  -0.0758   0.7267   0.6868
  -1.500   0.1642   0.02541   0.01648  -0.0761   0.7251   0.6897
  -1.250   0.1930   0.02525   0.01621  -0.0771   0.7237   0.6932
  -1.000   0.2022   0.02552   0.01647  -0.0754   0.7189   0.6974
  -0.750   0.2208   0.02573   0.01666  -0.0742   0.7156   0.6995
  -0.500   0.2445   0.02582   0.01670  -0.0739   0.7134   0.7018
  -0.250   0.2710   0.02584   0.01668  -0.0743   0.7116   0.7043
   0.000   0.2998   0.02580   0.01658  -0.0752   0.7102   0.7071
   0.250   0.3179   0.02607   0.01681  -0.0749   0.7069   0.7106
   0.500   0.3273   0.02661   0.01738  -0.0728   0.7021   0.7127
   0.750   0.3482   0.02687   0.01765  -0.0722   0.6996   0.7144
   1.000   0.3739   0.02700   0.01777  -0.0724   0.6977   0.7165
   1.250   0.4034   0.02702   0.01778  -0.0732   0.6962   0.7187
   1.500   0.4355   0.02699   0.01772  -0.0746   0.6949   0.7209
   1.750   0.4203   0.02854   0.01936  -0.0695   0.6866   0.7240
   2.000   0.4478   0.02871   0.01952  -0.0704   0.6843   0.7264
   2.250   0.4753   0.02882   0.01965  -0.0707   0.6826   0.7282
   2.500   0.5050   0.02888   0.01975  -0.0714   0.6813   0.7301
   3.000   0.5091   0.03090   0.02189  -0.0656   0.6692   0.7351
   3.250   0.5430   0.03084   0.02185  -0.0671   0.6677   0.7373
   3.500   0.5794   0.03075   0.02179  -0.0690   0.6665   0.7397
   4.000   0.5845   0.03317   0.02437  -0.0637   0.6536   0.7446
   4.250   0.6167   0.03307   0.02434  -0.0645   0.6523   0.7470
   4.750   0.6355   0.03535   0.02677  -0.0619   0.6391   0.7527
   5.000   0.6613   0.03563   0.02711  -0.0623   0.6355   0.7555
   5.500   0.6930   0.03700   0.02869  -0.0604   0.6246   0.7602
   5.750   0.7230   0.03686   0.02867  -0.0608   0.6219   0.7631
   6.250   0.7621   0.03781   0.02983  -0.0600   0.6096   0.7702
   6.750   0.7936   0.03891   0.03120  -0.0579   0.5958   0.7759
   7.000   0.8312   0.03795   0.03038  -0.0587   0.5933   0.7793
   7.500   0.8859   0.03677   0.02946  -0.0580   0.5795   0.7865
   8.000   0.8973   0.03849   0.03145  -0.0540   0.5531   0.7950
   9.000   0.9400   0.04030   0.03371  -0.0477   0.4774   0.8148
   9.250   0.9651   0.03932   0.03277  -0.0465   0.4440   0.8201
   9.500   1.0140   0.03622   0.02934  -0.0461   0.3903   0.8264
   9.750   1.0273   0.03658   0.02945  -0.0443   0.3439   0.8321
  10.000   1.0287   0.03815   0.03077  -0.0422   0.2997   0.8388
  10.250   1.0271   0.04011   0.03252  -0.0401   0.2604   0.8459
  10.500   1.0242   0.04226   0.03445  -0.0382   0.2227   0.8540
  10.750   1.0246   0.04418   0.03626  -0.0365   0.1905   0.8629
  11.000   1.0257   0.04611   0.03805  -0.0350   0.1618   0.8735
  11.500   1.0303   0.04955   0.04137  -0.0319   0.1126   0.9053
  11.750   1.0310   0.05104   0.04282  -0.0300   0.0956   0.9486
  12.000   1.0387   0.05286   0.04458  -0.0300   0.0816   1.0000
  12.250   1.0505   0.05470   0.04643  -0.0303   0.0679   1.0000
  12.500   1.0601   0.05674   0.04844  -0.0304   0.0601   1.0000
  12.750   1.0708   0.05869   0.05045  -0.0306   0.0538   1.0000
  13.000   1.0802   0.06077   0.05258  -0.0308   0.0482   1.0000
  13.250   1.0899   0.06284   0.05474  -0.0310   0.0431   1.0000
  13.500   1.0991   0.06496   0.05700  -0.0311   0.0391   1.0000
  13.750   1.1065   0.06730   0.05938  -0.0313   0.0351   1.0000
  14.000   1.1139   0.06970   0.06185  -0.0316   0.0321   1.0000
  14.250   1.1195   0.07231   0.06451  -0.0319   0.0293   1.0000
  14.500   1.1236   0.07515   0.06739  -0.0322   0.0265   1.0000
  14.750   1.1312   0.07760   0.07004  -0.0326   0.0242   1.0000
  15.000   1.1369   0.08032   0.07295  -0.0330   0.0220   1.0000
  15.250   1.1412   0.08326   0.07605  -0.0335   0.0203   1.0000
  15.500   1.1448   0.08635   0.07926  -0.0342   0.0185   1.0000
  15.750   1.1477   0.08958   0.08263  -0.0350   0.0171   1.0000
  16.000   1.1492   0.09304   0.08622  -0.0359   0.0158   1.0000
  16.250   1.1489   0.09685   0.09016  -0.0370   0.0150   1.0000
  16.500   1.1465   0.10105   0.09451  -0.0384   0.0143   1.0000
  16.750   1.1433   0.10545   0.09905  -0.0399   0.0135   1.0000
  17.000   1.1412   0.10978   0.10357  -0.0415   0.0127   1.0000
  17.250   1.1374   0.11448   0.10846  -0.0434   0.0118   1.0000
  17.500   1.1328   0.11939   0.11354  -0.0456   0.0114   1.0000
  17.750   1.1272   0.12460   0.11893  -0.0481   0.0110   1.0000
  18.000   1.1208   0.13008   0.12458  -0.0509   0.0106   1.0000
  18.250   1.1139   0.13580   0.13045  -0.0540   0.0103   1.0000
  18.500   1.1066   0.14173   0.13654  -0.0574   0.0101   1.0000
  18.750   1.0983   0.14799   0.14295  -0.0611   0.0099   1.0000
  19.000   1.0906   0.15426   0.14936  -0.0650   0.0097   1.0000
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