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FX 75-VG-166/22 (fx75vg166-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: FX 75-VG-166/22 (fx75vg166-il)
Reynolds number: 100,000
Max Cl/Cd: 25.73 at α=10.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx75vg166-il-100000-n5.txt
Download as CSV file: xf-fx75vg166-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 75-VG-166/22                                 
  
 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  -0.3172   0.10052   0.09444  -0.0952   0.8151   0.0294
 -12.750  -0.3225   0.09410   0.08804  -0.0987   0.8143   0.0292
 -12.500  -0.3319   0.08686   0.08082  -0.1031   0.8135   0.0288
 -12.250  -0.3538   0.07857   0.07248  -0.1086   0.8128   0.0285
 -12.000  -0.3740   0.07253   0.06635  -0.1121   0.8120   0.0281
 -11.750  -0.4023   0.06676   0.06043  -0.1142   0.8111   0.0279
 -11.500  -0.4226   0.06272   0.05623  -0.1144   0.8100   0.0277
 -11.250  -0.4421   0.05917   0.05249  -0.1134   0.8087   0.0276
 -10.750  -0.4787   0.05284   0.04571  -0.1089   0.8062   0.0277
 -10.500  -0.4888   0.05040   0.04307  -0.1062   0.8050   0.0276
 -10.250  -0.5006   0.04793   0.04035  -0.1028   0.8036   0.0278
 -10.000  -0.5093   0.04593   0.03807  -0.0990   0.8021   0.0281
  -9.750  -0.5118   0.04396   0.03580  -0.0958   0.8004   0.0282
  -9.500  -0.5105   0.04175   0.03321  -0.0928   0.7987   0.0287
  -9.250  -0.5050   0.03985   0.03086  -0.0901   0.7972   0.0294
  -9.000  -0.4904   0.03848   0.02941  -0.0891   0.7960   0.0305
  -8.750  -0.4753   0.03749   0.02833  -0.0879   0.7949   0.0318
  -8.500  -0.4578   0.03620   0.02682  -0.0868   0.7938   0.0332
  -8.250  -0.4359   0.03471   0.02503  -0.0861   0.7928   0.0346
  -8.000  -0.4104   0.03328   0.02329  -0.0859   0.7917   0.0359
  -7.750  -0.3861   0.03211   0.02218  -0.0860   0.7906   0.0377
  -7.500  -0.3643   0.03133   0.02136  -0.0855   0.7892   0.0404
  -7.250  -0.3391   0.03047   0.02036  -0.0853   0.7876   0.0430
  -7.000  -0.3134   0.02949   0.01937  -0.0852   0.7860   0.0450
  -6.750  -0.2949   0.02893   0.01883  -0.0842   0.7843   0.0484
  -6.500  -0.2759   0.02844   0.01826  -0.0830   0.7828   0.0522
  -6.250  -0.2604   0.02789   0.01772  -0.0813   0.7815   0.0558
  -6.000  -0.2449   0.02750   0.01728  -0.0796   0.7802   0.0605
  -5.750  -0.2297   0.02710   0.01687  -0.0778   0.7791   0.0675
  -5.500  -0.2172   0.02685   0.01662  -0.0757   0.7771   0.0763
  -5.250  -0.2051   0.02653   0.01640  -0.0736   0.7748   0.0896
  -5.000  -0.1923   0.02613   0.01621  -0.0715   0.7725   0.1182
  -4.750  -0.1802   0.02560   0.01608  -0.0693   0.7705   0.1888
  -4.500  -0.1776   0.02484   0.01607  -0.0656   0.7686   0.3249
  -4.250  -0.1043   0.02653   0.01933  -0.0678   0.7687   0.6459
  -4.000  -0.0943   0.02731   0.02002  -0.0640   0.7669   0.6857
  -3.750  -0.1090   0.02782   0.02052  -0.0571   0.7630   0.7126
  -3.500  -0.0951   0.02907   0.02170  -0.0538   0.7601   0.7392
  -3.250  -0.0884   0.03008   0.02261  -0.0495   0.7572   0.7628
  -3.000  -0.0558   0.03126   0.02365  -0.0488   0.7557   0.7819
  -2.750  -0.0279   0.03184   0.02409  -0.0482   0.7544   0.7944
  -2.500  -0.0141   0.03219   0.02432  -0.0457   0.7528   0.8060
  -2.250   0.0039   0.03270   0.02479  -0.0444   0.7490   0.8121
  -2.000   0.0056   0.03300   0.02504  -0.0402   0.7450   0.8221
  -1.750   0.0328   0.03315   0.02509  -0.0403   0.7430   0.8273
  -1.500   0.0404   0.03325   0.02510  -0.0370   0.7408   0.8356
  -1.250   0.0733   0.03331   0.02506  -0.0381   0.7396   0.8388
  -1.000   0.0465   0.03383   0.02562  -0.0295   0.7326   0.8499
  -0.750   0.0708   0.03393   0.02564  -0.0293   0.7296   0.8530
  -0.500   0.0941   0.03395   0.02558  -0.0288   0.7273   0.8566
  -0.250   0.1126   0.03389   0.02544  -0.0274   0.7254   0.8613
   0.000   0.0915   0.03433   0.02591  -0.0199   0.7174   0.8688
   0.250   0.1101   0.03439   0.02592  -0.0187   0.7143   0.8728
   0.500   0.1258   0.03436   0.02582  -0.0170   0.7122   0.8765
   1.000   0.1133   0.03462   0.02606  -0.0068   0.7005   0.8855
   1.250   0.1372   0.03460   0.02599  -0.0065   0.6985   0.8878
   1.500   0.1641   0.03454   0.02588  -0.0065   0.6970   0.8906
   1.750   0.1324   0.03484   0.02620   0.0022   0.6865   0.8968
   2.000   0.1617   0.03477   0.02608   0.0017   0.6845   0.8982
   2.500   0.1757   0.03510   0.02640   0.0068   0.6726   0.9030
   2.750   0.2026   0.03504   0.02632   0.0067   0.6704   0.9041
   3.000   0.2324   0.03495   0.02621   0.0061   0.6688   0.9050
   3.250   0.2191   0.03552   0.02678   0.0111   0.6584   0.9089
   3.500   0.2472   0.03546   0.02674   0.0107   0.6560   0.9098
   3.750   0.2786   0.03535   0.02663   0.0100   0.6542   0.9104
   4.000   0.2768   0.03590   0.02721   0.0131   0.6439   0.9125
   4.250   0.3071   0.03571   0.02704   0.0126   0.6411   0.9136
   4.500   0.3398   0.03550   0.02686   0.0118   0.6392   0.9145
   4.750   0.3404   0.03616   0.02755   0.0144   0.6285   0.9167
   5.000   0.3712   0.03599   0.02742   0.0137   0.6260   0.9177
   5.500   0.4052   0.03650   0.02803   0.0154   0.6128   0.9201
   5.750   0.4370   0.03624   0.02783   0.0147   0.6104   0.9205
   6.000   0.4430   0.03696   0.02860   0.0164   0.5996   0.9218
   6.250   0.4730   0.03673   0.02844   0.0160   0.5961   0.9223
   6.500   0.5071   0.03628   0.02808   0.0152   0.5938   0.9227
   7.000   0.5488   0.03626   0.02823   0.0162   0.5783   0.9247
   7.250   0.5604   0.03670   0.02876   0.0174   0.5661   0.9260
   7.500   0.5970   0.03573   0.02790   0.0168   0.5625   0.9265
   7.750   0.6109   0.03607   0.02833   0.0178   0.5500   0.9274
   8.000   0.6314   0.03597   0.02833   0.0184   0.5389   0.9281
   8.250   0.6642   0.03506   0.02754   0.0182   0.5320   0.9286
   8.500   0.6813   0.03534   0.02793   0.0188   0.5185   0.9294
   8.750   0.7031   0.03536   0.02806   0.0192   0.5062   0.9302
   9.000   0.7316   0.03488   0.02771   0.0191   0.4949   0.9308
   9.250   0.7617   0.03424   0.02716   0.0191   0.4807   0.9314
   9.500   0.7855   0.03407   0.02706   0.0194   0.4605   0.9321
   9.750   0.8127   0.03365   0.02667   0.0196   0.4358   0.9328
  10.000   0.8405   0.03314   0.02606   0.0200   0.4018   0.9334
  10.250   0.8592   0.03339   0.02614   0.0208   0.3620   0.9341
  10.500   0.8698   0.03424   0.02670   0.0220   0.3160   0.9350
  10.750   0.8756   0.03560   0.02783   0.0233   0.2731   0.9361
  11.250   0.8837   0.03898   0.03076   0.0253   0.2009   0.9383
  11.500   0.8927   0.04052   0.03223   0.0257   0.1756   0.9393
  11.750   0.8997   0.04225   0.03385   0.0261   0.1530   0.9402
  12.000   0.9087   0.04389   0.03547   0.0264   0.1320   0.9410
  12.250   0.9167   0.04566   0.03720   0.0267   0.1133   0.9418
  12.500   0.9235   0.04759   0.03907   0.0269   0.0960   0.9427
  12.750   0.9309   0.04952   0.04097   0.0270   0.0813   0.9438
  13.000   0.9376   0.05157   0.04302   0.0272   0.0711   0.9452
  13.250   0.9448   0.05362   0.04510   0.0272   0.0622   0.9464
  13.500   0.9505   0.05587   0.04736   0.0272   0.0560   0.9477
  13.750   0.9571   0.05810   0.04967   0.0271   0.0508   0.9491
  14.000   0.9634   0.06039   0.05203   0.0269   0.0477   0.9506
  14.250   0.9715   0.06257   0.05433   0.0266   0.0445   0.9520
  14.500   0.9772   0.06504   0.05685   0.0262   0.0418   0.9535
  14.750   0.9840   0.06743   0.05932   0.0258   0.0395   0.9550
  15.000   0.9932   0.06958   0.06163   0.0255   0.0377   0.9564
  15.250   1.0005   0.07200   0.06418   0.0249   0.0357   0.9580
  15.500   1.0068   0.07448   0.06673   0.0243   0.0343   0.9599
  15.750   1.0133   0.07693   0.06923   0.0238   0.0330   0.9621
  16.250   1.0266   0.08190   0.07460   0.0228   0.0307   0.9717
  16.500   1.0307   0.08461   0.07748   0.0220   0.0296   0.9873
  16.750   1.0387   0.08774   0.08078   0.0204   0.0288   0.9951
  17.000   1.0353   0.09022   0.08334   0.0217   0.0284   1.0000
  17.250   1.0396   0.09317   0.08635   0.0209   0.0277   1.0000
  17.500   1.0441   0.09613   0.08941   0.0201   0.0273   1.0000
  17.750   1.0403   0.10050   0.09402   0.0186   0.0269   1.0000
  18.000   1.0318   0.10571   0.09952   0.0164   0.0265   1.0000
  18.250   1.0221   0.11125   0.10532   0.0138   0.0263   1.0000
  18.500   1.0092   0.11758   0.11190   0.0105   0.0260   1.0000
  18.750   0.9954   0.12432   0.11889   0.0068   0.0260   1.0000
  19.000   0.9755   0.13262   0.12743   0.0019   0.0258   1.0000
  19.250   0.9517   0.14228   0.13734  -0.0041   0.0260   1.0000
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