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MARSKE XM-1D AIRFOIL (F14-3.0) (marske1-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MARSKE XM-1D AIRFOIL (F14-3.0) (marske1-il)
Reynolds number: 1,000,000
Max Cl/Cd: 104.68 at α=8.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-marske1-il-1000000-n5.txt
Download as CSV file: xf-marske1-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MARSKE XM-1D AIRFOIL (F14-3.0)                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -1.0997   0.03413   0.02936  -0.0170   0.5865   0.0209
 -12.500  -1.1026   0.03264   0.02773  -0.0131   0.5843   0.0210
 -12.250  -1.0956   0.03134   0.02629  -0.0105   0.5819   0.0210
 -12.000  -1.0836   0.03037   0.02522  -0.0084   0.5798   0.0211
 -11.750  -1.0694   0.02951   0.02428  -0.0065   0.5777   0.0212
 -11.500  -1.0540   0.02866   0.02335  -0.0047   0.5751   0.0212
 -11.250  -1.0374   0.02785   0.02245  -0.0031   0.5722   0.0213
 -11.000  -1.0189   0.02725   0.02177  -0.0016   0.5694   0.0214
 -10.750  -1.0006   0.02647   0.02090  -0.0002   0.5664   0.0214
 -10.500  -0.9813   0.02579   0.02013   0.0012   0.5633   0.0215
 -10.250  -0.9608   0.02519   0.01947   0.0024   0.5610   0.0216
 -10.000  -0.9402   0.02452   0.01872   0.0037   0.5581   0.0217
  -9.750  -0.9195   0.02375   0.01786   0.0048   0.5547   0.0218
  -9.500  -0.8985   0.02291   0.01692   0.0060   0.5511   0.0220
  -9.250  -0.8766   0.02217   0.01608   0.0071   0.5478   0.0221
  -9.000  -0.8550   0.02121   0.01500   0.0082   0.5448   0.0224
  -8.750  -0.8326   0.02027   0.01397   0.0092   0.5412   0.0226
  -8.500  -0.8099   0.01933   0.01290   0.0101   0.5365   0.0229
  -8.250  -0.7865   0.01849   0.01196   0.0110   0.5319   0.0233
  -8.000  -0.7628   0.01772   0.01107   0.0119   0.5278   0.0235
  -7.750  -0.7385   0.01704   0.01032   0.0127   0.5236   0.0237
  -7.500  -0.7140   0.01644   0.00965   0.0135   0.5179   0.0238
  -7.250  -0.6891   0.01595   0.00907   0.0142   0.5114   0.0240
  -7.000  -0.6646   0.01535   0.00843   0.0150   0.5045   0.0242
  -6.750  -0.6394   0.01496   0.00799   0.0157   0.4954   0.0243
  -6.500  -0.6136   0.01464   0.00763   0.0164   0.4872   0.0245
  -6.250  -0.5878   0.01435   0.00730   0.0170   0.4777   0.0246
  -6.000  -0.5617   0.01410   0.00701   0.0176   0.4694   0.0248
  -5.750  -0.5356   0.01383   0.00669   0.0182   0.4600   0.0250
  -5.500  -0.5094   0.01358   0.00639   0.0188   0.4516   0.0252
  -5.250  -0.4832   0.01333   0.00609   0.0193   0.4423   0.0254
  -5.000  -0.4571   0.01307   0.00579   0.0199   0.4340   0.0257
  -4.750  -0.4310   0.01279   0.00547   0.0205   0.4263   0.0260
  -4.250  -0.3786   0.01226   0.00486   0.0217   0.4140   0.0266
  -4.000  -0.3523   0.01202   0.00458   0.0223   0.4084   0.0269
  -3.750  -0.3258   0.01183   0.00434   0.0228   0.4022   0.0272
  -3.500  -0.2994   0.01160   0.00409   0.0233   0.3968   0.0275
  -3.250  -0.2726   0.01141   0.00390   0.0238   0.3916   0.0278
  -3.000  -0.2456   0.01127   0.00374   0.0243   0.3864   0.0281
  -2.750  -0.2186   0.01114   0.00359   0.0247   0.3813   0.0284
  -2.500  -0.1914   0.01100   0.00344   0.0251   0.3773   0.0287
  -2.250  -0.1643   0.01085   0.00329   0.0255   0.3728   0.0291
  -2.000  -0.1372   0.01072   0.00314   0.0260   0.3678   0.0296
  -1.750  -0.1101   0.01061   0.00300   0.0264   0.3631   0.0301
  -1.500  -0.0828   0.01049   0.00286   0.0268   0.3596   0.0305
  -1.250  -0.0555   0.01036   0.00273   0.0271   0.3558   0.0309
  -1.000  -0.0282   0.01025   0.00262   0.0275   0.3514   0.0314
  -0.750  -0.0007   0.01019   0.00255   0.0278   0.3473   0.0319
  -0.500   0.0270   0.01014   0.00250   0.0281   0.3432   0.0326
  -0.250   0.0547   0.01007   0.00243   0.0284   0.3404   0.0334
   0.000   0.0823   0.00999   0.00235   0.0287   0.3370   0.0341
   0.250   0.1099   0.00993   0.00228   0.0290   0.3332   0.0347
   0.500   0.1375   0.00988   0.00223   0.0293   0.3296   0.0354
   0.750   0.1651   0.00985   0.00220   0.0296   0.3260   0.0362
   1.000   0.1930   0.00981   0.00217   0.0298   0.3235   0.0371
   1.250   0.2209   0.00978   0.00215   0.0300   0.3211   0.0382
   1.500   0.2487   0.00973   0.00212   0.0303   0.3180   0.0393
   1.750   0.2765   0.00972   0.00211   0.0305   0.3144   0.0405
   2.000   0.3042   0.00972   0.00211   0.0307   0.3108   0.0417
   2.250   0.3319   0.00973   0.00212   0.0309   0.3073   0.0429
   2.500   0.3599   0.00971   0.00212   0.0311   0.3054   0.0444
   2.750   0.3879   0.00971   0.00213   0.0313   0.3031   0.0463
   3.000   0.4158   0.00970   0.00214   0.0314   0.3004   0.0483
   3.250   0.4436   0.00972   0.00217   0.0316   0.2975   0.0506
   3.500   0.4713   0.00974   0.00220   0.0318   0.2944   0.0544
   3.750   0.4984   0.00973   0.00226   0.0321   0.2906   0.1004
   4.000   0.5259   0.00971   0.00230   0.0322   0.2882   0.1220
   4.250   0.5481   0.00917   0.00237   0.0332   0.2854   0.3600
   4.500   0.5589   0.00801   0.00234   0.0364   0.2823   0.7399
   4.750   0.5808   0.00785   0.00244   0.0378   0.2781   0.8189
   5.000   0.6052   0.00783   0.00257   0.0387   0.2740   0.8687
   5.250   0.6319   0.00784   0.00270   0.0392   0.2715   0.9031
   5.500   0.6609   0.00791   0.00283   0.0392   0.2683   0.9271
   5.750   0.6931   0.00803   0.00298   0.0384   0.2637   0.9451
   6.000   0.7237   0.00820   0.00313   0.0379   0.2587   0.9542
   6.250   0.7594   0.00835   0.00330   0.0363   0.2543   0.9619
   6.500   0.7890   0.00849   0.00343   0.0360   0.2497   0.9682
   6.750   0.8214   0.00867   0.00359   0.0350   0.2450   0.9707
   7.000   0.8541   0.00885   0.00376   0.0339   0.2409   0.9724
   7.250   0.8871   0.00900   0.00391   0.0328   0.2371   0.9744
   7.500   0.9192   0.00918   0.00409   0.0318   0.2321   0.9773
   7.750   0.9470   0.00940   0.00430   0.0317   0.2273   0.9816
   8.000   0.9806   0.00958   0.00448   0.0304   0.2231   0.9826
   8.250   1.0127   0.00978   0.00468   0.0293   0.2175   0.9837
   8.500   1.0439   0.01006   0.00493   0.0283   0.2105   0.9851
   8.750   1.0751   0.01027   0.00514   0.0274   0.2039   0.9866
   9.000   1.1047   0.01061   0.00544   0.0267   0.1943   0.9884
   9.250   1.1332   0.01102   0.00578   0.0261   0.1812   0.9904
   9.500   1.1603   0.01148   0.00617   0.0257   0.1673   0.9925
   9.750   1.1890   0.01203   0.00665   0.0248   0.1507   0.9940
  10.000   1.2178   0.01261   0.00715   0.0238   0.1370   0.9956
  10.250   1.2463   0.01318   0.00768   0.0229   0.1266   0.9973
  10.500   1.2753   0.01367   0.00815   0.0219   0.1196   0.9987
  10.750   1.3038   0.01420   0.00867   0.0210   0.1136   0.9998
  11.000   1.3243   0.01465   0.00912   0.0218   0.1092   1.0000
  11.250   1.3402   0.01519   0.00966   0.0233   0.1045   1.0000
  11.500   1.3573   0.01565   0.01013   0.0247   0.1015   1.0000
  11.750   1.3740   0.01611   0.01063   0.0260   0.0985   1.0000
  12.000   1.3889   0.01670   0.01122   0.0275   0.0950   1.0000
  12.250   1.4023   0.01736   0.01189   0.0291   0.0916   1.0000
  12.500   1.4168   0.01794   0.01251   0.0305   0.0890   1.0000
  12.750   1.4277   0.01871   0.01331   0.0322   0.0856   1.0000
  13.000   1.4316   0.01981   0.01442   0.0343   0.0821   1.0000
  13.250   1.4272   0.02159   0.01629   0.0359   0.0802   1.0000
  13.500   1.4280   0.02438   0.01916   0.0344   0.0776   1.0000
  13.750   1.4252   0.02717   0.02199   0.0338   0.0748   1.0000
  14.000   1.4197   0.03009   0.02495   0.0334   0.0723   1.0000
  14.250   1.4166   0.03276   0.02768   0.0332   0.0703   1.0000
  14.500   1.4107   0.03574   0.03071   0.0328   0.0680   1.0000
  14.750   1.3995   0.03930   0.03432   0.0322   0.0653   1.0000
  15.000   1.3913   0.04268   0.03775   0.0316   0.0634   1.0000
  15.250   1.3829   0.04615   0.04129   0.0308   0.0613   1.0000
  15.500   1.3735   0.04986   0.04506   0.0299   0.0593   1.0000
  15.750   1.3626   0.05393   0.04917   0.0288   0.0573   1.0000
  16.000   1.3553   0.05765   0.05296   0.0277   0.0556   1.0000
  16.250   1.3476   0.06150   0.05687   0.0265   0.0541   1.0000
  16.500   1.3382   0.06560   0.06103   0.0252   0.0524   1.0000
  16.750   1.3295   0.06963   0.06511   0.0239   0.0509   1.0000
  17.000   1.3208   0.07377   0.06930   0.0225   0.0493   1.0000
  17.250   1.3149   0.07759   0.07317   0.0212   0.0482   1.0000
  17.500   1.3086   0.08146   0.07710   0.0199   0.0465   1.0000
  17.750   1.3010   0.08562   0.08131   0.0184   0.0456   1.0000
  18.000   1.2938   0.08970   0.08543   0.0169   0.0442   1.0000
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