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LOCKHEED L-188 TIP AIRFOIL (l188tip-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: LOCKHEED L-188 TIP AIRFOIL (l188tip-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.56 at α=2.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-l188tip-il-1000000-n5.txt
Download as CSV file: xf-l188tip-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: LOCKHEED L-188 TIP AIRFOIL                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -1.0811   0.04804   0.04508  -0.0815   1.0000   0.0089
 -15.750  -1.1017   0.04117   0.03801  -0.0871   1.0000   0.0089
 -15.500  -1.1104   0.03691   0.03360  -0.0899   1.0000   0.0090
 -15.250  -1.1143   0.03377   0.03033  -0.0914   1.0000   0.0090
 -15.000  -1.1152   0.03141   0.02784  -0.0917   1.0000   0.0091
 -14.750  -1.1070   0.02946   0.02577  -0.0926   0.9905   0.0092
 -14.500  -1.0949   0.02788   0.02407  -0.0929   0.9810   0.0093
 -14.250  -1.0838   0.02664   0.02271  -0.0922   0.9719   0.0094
 -14.000  -1.0710   0.02552   0.02148  -0.0912   0.9648   0.0096
 -13.750  -1.0568   0.02450   0.02035  -0.0903   0.9587   0.0097
 -13.500  -1.0411   0.02355   0.01928  -0.0894   0.9535   0.0098
 -13.250  -1.0241   0.02266   0.01828  -0.0885   0.9483   0.0100
 -13.000  -1.0062   0.02183   0.01734  -0.0877   0.9439   0.0102
 -12.750  -0.9869   0.02106   0.01646  -0.0871   0.9402   0.0103
 -12.500  -0.9663   0.02035   0.01565  -0.0865   0.9363   0.0105
 -12.250  -0.9449   0.01971   0.01491  -0.0860   0.9326   0.0106
 -12.000  -0.9246   0.01894   0.01404  -0.0854   0.9291   0.0108
 -11.750  -0.9034   0.01821   0.01323  -0.0848   0.9259   0.0111
 -11.500  -0.8804   0.01761   0.01257  -0.0845   0.9229   0.0114
 -11.250  -0.8570   0.01706   0.01196  -0.0842   0.9199   0.0117
 -11.000  -0.8332   0.01655   0.01138  -0.0839   0.9168   0.0119
 -10.750  -0.8092   0.01606   0.01082  -0.0836   0.9139   0.0122
 -10.500  -0.7850   0.01559   0.01028  -0.0833   0.9111   0.0125
 -10.250  -0.7602   0.01513   0.00975  -0.0831   0.9086   0.0127
 -10.000  -0.7350   0.01469   0.00925  -0.0829   0.9060   0.0130
  -9.750  -0.7096   0.01429   0.00878  -0.0827   0.9032   0.0132
  -9.500  -0.6845   0.01383   0.00827  -0.0825   0.9004   0.0135
  -9.250  -0.6593   0.01339   0.00777  -0.0823   0.8977   0.0140
  -9.000  -0.6336   0.01303   0.00737  -0.0821   0.8951   0.0145
  -8.750  -0.6072   0.01270   0.00701  -0.0820   0.8927   0.0150
  -8.500  -0.5806   0.01239   0.00667  -0.0820   0.8900   0.0155
  -8.250  -0.5541   0.01208   0.00632  -0.0819   0.8873   0.0160
  -8.000  -0.5274   0.01179   0.00597  -0.0819   0.8844   0.0163
  -7.750  -0.5011   0.01144   0.00558  -0.0817   0.8816   0.0170
  -7.500  -0.4745   0.01115   0.00526  -0.0816   0.8789   0.0176
  -7.250  -0.4474   0.01088   0.00498  -0.0816   0.8763   0.0184
  -7.000  -0.4201   0.01064   0.00471  -0.0816   0.8735   0.0191
  -6.750  -0.3927   0.01042   0.00446  -0.0817   0.8703   0.0199
  -6.500  -0.3657   0.01014   0.00417  -0.0816   0.8673   0.0210
  -6.250  -0.3384   0.00992   0.00393  -0.0816   0.8643   0.0221
  -6.000  -0.3109   0.00972   0.00371  -0.0816   0.8614   0.0232
  -5.500  -0.2556   0.00930   0.00328  -0.0817   0.8546   0.0260
  -5.250  -0.2278   0.00913   0.00309  -0.0817   0.8510   0.0278
  -5.000  -0.2002   0.00895   0.00290  -0.0817   0.8476   0.0297
  -4.750  -0.1723   0.00878   0.00273  -0.0818   0.8441   0.0321
  -4.500  -0.1442   0.00863   0.00257  -0.0819   0.8400   0.0343
  -4.250  -0.1164   0.00846   0.00241  -0.0820   0.8356   0.0375
  -4.000  -0.0884   0.00833   0.00227  -0.0820   0.8315   0.0410
  -3.750  -0.0603   0.00817   0.00214  -0.0821   0.8272   0.0457
  -3.500  -0.0323   0.00803   0.00201  -0.0822   0.8220   0.0509
  -3.250  -0.0043   0.00791   0.00189  -0.0822   0.8169   0.0569
  -3.000   0.0238   0.00777   0.00178  -0.0823   0.8117   0.0649
  -2.750   0.0519   0.00763   0.00168  -0.0824   0.8056   0.0750
  -2.500   0.0798   0.00752   0.00158  -0.0825   0.7998   0.0867
  -2.250   0.1079   0.00739   0.00150  -0.0826   0.7932   0.1021
  -2.000   0.1357   0.00726   0.00141  -0.0826   0.7865   0.1218
  -1.750   0.1635   0.00712   0.00135  -0.0827   0.7800   0.1489
  -1.500   0.1911   0.00697   0.00128  -0.0827   0.7727   0.1826
  -1.250   0.2186   0.00677   0.00122  -0.0827   0.7661   0.2310
  -0.750   0.2720   0.00619   0.00110  -0.0827   0.7520   0.3957
  -0.500   0.2985   0.00588   0.00108  -0.0826   0.7448   0.4976
  -0.250   0.3256   0.00574   0.00109  -0.0825   0.7381   0.5557
   0.000   0.3535   0.00566   0.00111  -0.0825   0.7310   0.5953
   0.250   0.3811   0.00563   0.00113  -0.0825   0.7238   0.6252
   0.500   0.4085   0.00561   0.00116  -0.0823   0.7125   0.6547
   0.750   0.4342   0.00566   0.00121  -0.0819   0.6896   0.6875
   1.250   0.4851   0.00582   0.00134  -0.0808   0.6391   0.7477
   1.500   0.5119   0.00593   0.00140  -0.0806   0.6199   0.7570
   1.750   0.5384   0.00605   0.00146  -0.0803   0.5995   0.7650
   2.000   0.5646   0.00620   0.00153  -0.0800   0.5770   0.7737
   2.250   0.5904   0.00636   0.00163  -0.0796   0.5513   0.7819
   2.500   0.6156   0.00658   0.00173  -0.0791   0.5199   0.7913
   2.750   0.6394   0.00687   0.00188  -0.0784   0.4772   0.8005
   3.000   0.6609   0.00733   0.00209  -0.0773   0.4135   0.8110
   3.250   0.6817   0.00784   0.00235  -0.0761   0.3491   0.8239
   3.500   0.7032   0.00825   0.00260  -0.0751   0.2979   0.8408
   3.750   0.7245   0.00857   0.00283  -0.0739   0.2550   0.8705
   4.000   0.7462   0.00882   0.00309  -0.0726   0.2198   0.9382
   4.250   0.7817   0.00922   0.00335  -0.0746   0.1858   0.9855
   4.500   0.8108   0.00958   0.00357  -0.0752   0.1600   1.0000
   4.750   0.8337   0.00988   0.00378  -0.0744   0.1418   1.0000
   5.000   0.8569   0.01017   0.00399  -0.0736   0.1262   1.0000
   5.250   0.8801   0.01046   0.00420  -0.0729   0.1122   1.0000
   5.500   0.9032   0.01076   0.00443  -0.0721   0.1002   1.0000
   5.750   0.9266   0.01104   0.00466  -0.0714   0.0902   1.0000
   6.000   0.9501   0.01130   0.00489  -0.0707   0.0827   1.0000
   6.250   0.9730   0.01160   0.00514  -0.0699   0.0747   1.0000
   6.500   0.9961   0.01189   0.00540  -0.0691   0.0682   1.0000
   6.750   1.0189   0.01218   0.00566  -0.0684   0.0628   1.0000
   7.000   1.0414   0.01249   0.00594  -0.0675   0.0573   1.0000
   7.250   1.0639   0.01279   0.00623  -0.0667   0.0532   1.0000
   7.500   1.0859   0.01311   0.00652  -0.0658   0.0493   1.0000
   7.750   1.1072   0.01344   0.00684  -0.0647   0.0457   1.0000
   8.000   1.1278   0.01375   0.00715  -0.0635   0.0428   1.0000
   8.250   1.1474   0.01411   0.00749  -0.0622   0.0398   1.0000
   8.500   1.1676   0.01445   0.00784  -0.0610   0.0379   1.0000
   8.750   1.1875   0.01481   0.00821  -0.0598   0.0358   1.0000
   9.000   1.2065   0.01523   0.00862  -0.0584   0.0333   1.0000
   9.250   1.2263   0.01561   0.00902  -0.0572   0.0318   1.0000
   9.500   1.2457   0.01603   0.00945  -0.0560   0.0302   1.0000
   9.750   1.2644   0.01649   0.00991  -0.0547   0.0286   1.0000
  10.000   1.2828   0.01696   0.01040  -0.0534   0.0272   1.0000
  10.250   1.3016   0.01742   0.01088  -0.0522   0.0261   1.0000
  10.500   1.3198   0.01792   0.01140  -0.0510   0.0248   1.0000
  10.750   1.3370   0.01847   0.01197  -0.0496   0.0236   1.0000
  11.000   1.3542   0.01905   0.01257  -0.0482   0.0227   1.0000
  11.250   1.3717   0.01959   0.01316  -0.0470   0.0220   1.0000
  11.500   1.3885   0.02018   0.01378  -0.0457   0.0212   1.0000
  11.750   1.4047   0.02082   0.01444  -0.0443   0.0203   1.0000
  12.000   1.4200   0.02153   0.01517  -0.0429   0.0194   1.0000
  12.250   1.4352   0.02225   0.01593  -0.0415   0.0187   1.0000
  12.500   1.4506   0.02296   0.01669  -0.0401   0.0182   1.0000
  12.750   1.4656   0.02370   0.01748  -0.0388   0.0177   1.0000
  13.000   1.4797   0.02451   0.01834  -0.0374   0.0172   1.0000
  13.250   1.4932   0.02537   0.01924  -0.0360   0.0166   1.0000
  13.500   1.5057   0.02631   0.02022  -0.0345   0.0161   1.0000
  13.750   1.5171   0.02736   0.02131  -0.0330   0.0156   1.0000
  14.000   1.5293   0.02835   0.02236  -0.0316   0.0152   1.0000
  14.250   1.5413   0.02935   0.02343  -0.0303   0.0149   1.0000
  14.500   1.5524   0.03045   0.02459  -0.0290   0.0145   1.0000
  14.750   1.5627   0.03163   0.02583  -0.0276   0.0141   1.0000
  15.000   1.5723   0.03289   0.02715  -0.0263   0.0138   1.0000
  15.250   1.5809   0.03424   0.02856  -0.0250   0.0134   1.0000
  15.500   1.5884   0.03571   0.03010  -0.0237   0.0131   1.0000
  15.750   1.5946   0.03734   0.03179  -0.0225   0.0128   1.0000
  16.000   1.5994   0.03916   0.03368  -0.0212   0.0125   1.0000
  16.250   1.6060   0.04085   0.03546  -0.0202   0.0123   1.0000
  16.500   1.6117   0.04267   0.03737  -0.0193   0.0122   1.0000
  16.750   1.6165   0.04463   0.03942  -0.0185   0.0120   1.0000
  17.000   1.6207   0.04673   0.04160  -0.0178   0.0117   1.0000
  17.250   1.6239   0.04897   0.04393  -0.0171   0.0115   1.0000
  17.500   1.6260   0.05138   0.04643  -0.0166   0.0113   1.0000
  17.750   1.6272   0.05398   0.04911  -0.0163   0.0111   1.0000
  18.000   1.6272   0.05679   0.05201  -0.0161   0.0109   1.0000
  18.250   1.6257   0.05986   0.05517  -0.0160   0.0107   1.0000
  18.500   1.6227   0.06320   0.05861  -0.0162   0.0105   1.0000
  18.750   1.6174   0.06691   0.06242  -0.0165   0.0104   1.0000
  19.000   1.6098   0.07107   0.06669  -0.0172   0.0102   1.0000
  19.250   1.6003   0.07565   0.07138  -0.0181   0.0101   1.0000
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