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FX 38-153 AIRFOIL (fx38153-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: FX 38-153 AIRFOIL (fx38153-il)
Reynolds number: 100,000
Max Cl/Cd: 36.07 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx38153-il-100000-n5.txt
Download as CSV file: xf-fx38153-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 38-153 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
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.5461   0.09770   0.09291  -0.0503   0.9995   0.0214
 -10.500  -0.5601   0.09067   0.08582  -0.0548   0.9976   0.0211
 -10.250  -0.5785   0.08439   0.07945  -0.0583   0.9953   0.0207
 -10.000  -0.5986   0.07895   0.07387  -0.0603   0.9926   0.0204
  -9.750  -0.6197   0.07453   0.06930  -0.0602   0.9890   0.0202
  -9.500  -0.6405   0.07088   0.06548  -0.0589   0.9855   0.0200
  -9.250  -0.6591   0.06769   0.06209  -0.0570   0.9817   0.0199
  -9.000  -0.6750   0.06456   0.05875  -0.0540   0.9772   0.0198
  -8.750  -0.6824   0.06105   0.05496  -0.0520   0.9733   0.0198
  -8.500  -0.6817   0.05724   0.05078  -0.0509   0.9699   0.0198
  -8.250  -0.6830   0.05388   0.04706  -0.0484   0.9664   0.0196
  -8.000  -0.6811   0.05067   0.04347  -0.0458   0.9628   0.0193
  -7.750  -0.6711   0.04744   0.03979  -0.0442   0.9596   0.0191
  -7.500  -0.6549   0.04448   0.03636  -0.0434   0.9572   0.0190
  -7.250  -0.6344   0.04194   0.03338  -0.0430   0.9555   0.0190
  -7.000  -0.6139   0.03986   0.03095  -0.0422   0.9535   0.0191
  -6.750  -0.5972   0.03814   0.02897  -0.0406   0.9502   0.0192
  -6.500  -0.5752   0.03657   0.02716  -0.0397   0.9475   0.0194
  -6.250  -0.5506   0.03516   0.02556  -0.0393   0.9452   0.0198
  -6.000  -0.5244   0.03392   0.02415  -0.0392   0.9433   0.0202
  -5.750  -0.4975   0.03281   0.02292  -0.0392   0.9415   0.0208
  -5.500  -0.4697   0.03182   0.02181  -0.0395   0.9399   0.0215
  -5.250  -0.4545   0.03096   0.02088  -0.0375   0.9359   0.0222
  -5.000  -0.4358   0.03015   0.02005  -0.0366   0.9325   0.0232
  -4.750  -0.4118   0.02945   0.01929  -0.0365   0.9295   0.0247
  -4.500  -0.3842   0.02883   0.01860  -0.0371   0.9270   0.0276
  -4.250  -0.3537   0.02829   0.01802  -0.0382   0.9250   0.0343
  -4.000  -0.3357   0.02765   0.01736  -0.0369   0.9201   0.0446
  -3.750  -0.3122   0.02689   0.01679  -0.0367   0.9161   0.0751
  -3.500  -0.2878   0.02531   0.01629  -0.0377   0.9135   0.2651
  -3.250  -0.2827   0.02481   0.01788  -0.0312   0.9106   0.6230
  -3.000  -0.2699   0.02605   0.01918  -0.0265   0.9050   0.7209
  -2.750  -0.2494   0.02702   0.02002  -0.0242   0.9002   0.7560
  -2.500  -0.2263   0.02803   0.02089  -0.0216   0.8966   0.7751
  -2.250  -0.2061   0.02895   0.02171  -0.0184   0.8924   0.7941
  -2.000  -0.1927   0.02954   0.02221  -0.0143   0.8856   0.8094
  -1.750  -0.1661   0.02992   0.02246  -0.0131   0.8819   0.8217
  -1.500  -0.1334   0.02996   0.02234  -0.0142   0.8794   0.8290
  -1.250  -0.1217   0.02984   0.02214  -0.0117   0.8714   0.8345
  -1.000  -0.0915   0.02973   0.02190  -0.0123   0.8675   0.8377
  -0.750  -0.0557   0.02956   0.02160  -0.0142   0.8647   0.8412
  -0.500  -0.0404   0.02936   0.02133  -0.0128   0.8554   0.8473
  -0.250  -0.0089   0.02920   0.02107  -0.0135   0.8518   0.8499
   0.000   0.0104   0.02910   0.02093  -0.0121   0.8447   0.8536
   0.250   0.0391   0.02888   0.02064  -0.0127   0.8390   0.8568
   0.500   0.0762   0.02857   0.02025  -0.0149   0.8357   0.8594
   0.750   0.0936   0.02844   0.02008  -0.0137   0.8257   0.8631
   1.000   0.1261   0.02816   0.01976  -0.0146   0.8219   0.8651
   1.250   0.1441   0.02808   0.01967  -0.0132   0.8130   0.8681
   1.500   0.1764   0.02776   0.01933  -0.0142   0.8079   0.8708
   1.750   0.1995   0.02759   0.01916  -0.0138   0.7988   0.8741
   2.000   0.2331   0.02725   0.01880  -0.0153   0.7932   0.8766
   2.250   0.2562   0.02708   0.01865  -0.0147   0.7846   0.8788
   2.500   0.2861   0.02672   0.01831  -0.0152   0.7785   0.8805
   2.750   0.3106   0.02648   0.01810  -0.0148   0.7692   0.8824
   3.000   0.3423   0.02600   0.01764  -0.0155   0.7625   0.8844
   3.250   0.3660   0.02577   0.01746  -0.0150   0.7516   0.8868
   3.500   0.4010   0.02518   0.01691  -0.0162   0.7458   0.8884
   3.750   0.4257   0.02503   0.01680  -0.0161   0.7336   0.8903
   4.000   0.4548   0.02471   0.01653  -0.0166   0.7216   0.8922
   4.250   0.4824   0.02420   0.01607  -0.0162   0.7090   0.8939
   4.500   0.5110   0.02373   0.01565  -0.0162   0.6942   0.8955
   4.750   0.5424   0.02324   0.01520  -0.0166   0.6787   0.8968
   5.000   0.5752   0.02276   0.01474  -0.0173   0.6625   0.8984
   5.250   0.6078   0.02235   0.01437  -0.0180   0.6431   0.9001
   5.500   0.6443   0.02189   0.01389  -0.0193   0.6213   0.9015
   5.750   0.6774   0.02165   0.01362  -0.0202   0.5949   0.9029
   6.000   0.7088   0.02155   0.01347  -0.0210   0.5654   0.9041
   6.250   0.7391   0.02158   0.01343  -0.0216   0.5359   0.9054
   6.500   0.7645   0.02178   0.01356  -0.0216   0.5045   0.9070
   6.750   0.7845   0.02201   0.01369  -0.0204   0.4739   0.9088
   7.000   0.8030   0.02236   0.01396  -0.0191   0.4439   0.9107
   7.250   0.8216   0.02278   0.01432  -0.0181   0.4151   0.9123
   7.500   0.8392   0.02328   0.01476  -0.0169   0.3853   0.9140
   7.750   0.8552   0.02389   0.01526  -0.0157   0.3535   0.9157
   8.000   0.8706   0.02457   0.01585  -0.0145   0.3212   0.9174
   8.250   0.8850   0.02536   0.01650  -0.0132   0.2895   0.9193
   8.500   0.9009   0.02615   0.01721  -0.0123   0.2600   0.9212
   8.750   0.9136   0.02686   0.01786  -0.0106   0.2366   0.9232
   9.000   0.9282   0.02758   0.01857  -0.0093   0.2180   0.9250
   9.250   0.9443   0.02831   0.01933  -0.0084   0.2010   0.9267
   9.500   0.9598   0.02911   0.02015  -0.0075   0.1864   0.9283
   9.750   0.9752   0.02996   0.02103  -0.0066   0.1727   0.9300
  10.000   0.9909   0.03084   0.02198  -0.0058   0.1580   0.9317
  10.250   1.0061   0.03179   0.02296  -0.0051   0.1438   0.9335
  10.500   1.0205   0.03278   0.02401  -0.0043   0.1329   0.9354
  10.750   1.0306   0.03381   0.02506  -0.0028   0.1232   0.9375
  11.000   1.0444   0.03471   0.02612  -0.0018   0.1116   0.9397
  11.250   1.0563   0.03581   0.02731  -0.0007   0.1008   0.9418
  11.500   1.0669   0.03709   0.02864   0.0003   0.0906   0.9437
  11.750   1.0756   0.03856   0.03014   0.0013   0.0817   0.9455
  12.000   1.0870   0.03992   0.03166   0.0020   0.0714   0.9474
  12.250   1.0947   0.04151   0.03334   0.0031   0.0642   0.9493
  12.500   1.0978   0.04333   0.03519   0.0045   0.0591   0.9517
  12.750   1.1026   0.04513   0.03716   0.0057   0.0544   0.9543
  13.000   1.1043   0.04729   0.03942   0.0068   0.0508   0.9570
  13.250   1.1056   0.04964   0.04188   0.0077   0.0479   0.9596
  13.500   1.1090   0.05187   0.04433   0.0084   0.0450   0.9621
  13.750   1.1101   0.05427   0.04690   0.0091   0.0427   0.9646
  14.000   1.1099   0.05695   0.04972   0.0095   0.0411   0.9674
  14.250   1.1086   0.05987   0.05275   0.0097   0.0399   0.9703
  14.750   1.1092   0.06569   0.05897   0.0096   0.0379   0.9769
  15.000   1.1084   0.06879   0.06225   0.0093   0.0370   0.9816
  15.250   1.1063   0.07195   0.06558   0.0088   0.0363   0.9902
  15.500   1.1050   0.07534   0.06914   0.0079   0.0356   0.9999
  15.750   1.1049   0.07902   0.07299   0.0067   0.0350   0.9999
  16.000   1.1044   0.08283   0.07695   0.0053   0.0345   0.9999
  16.250   1.1037   0.08673   0.08100   0.0038   0.0340   0.9999
  16.500   1.1027   0.09071   0.08512   0.0022   0.0336   0.9999
  16.750   1.1018   0.09470   0.08924   0.0006   0.0331   0.9999
  17.000   1.0997   0.09897   0.09364  -0.0013   0.0326   0.9999
  17.250   1.0912   0.10461   0.09955  -0.0043   0.0323   0.9999
  17.500   1.0806   0.11083   0.10602  -0.0079   0.0320   0.9999
  17.750   1.0671   0.11785   0.11330  -0.0122   0.0318   0.9999
  18.000   1.0514   0.12561   0.12129  -0.0172   0.0316   0.9999
  18.250   1.0323   0.13451   0.13040  -0.0232   0.0317   0.9999
  18.500   1.0074   0.14533   0.14143  -0.0305   0.0319   0.9999
  18.750   0.9705   0.16016   0.15643  -0.0404   0.0323   0.9999
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