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FX 60-177 AIRFOIL (fx60177-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: FX 60-177 AIRFOIL (fx60177-il)
Reynolds number: 100,000
Max Cl/Cd: 40.42 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx60177-il-100000.txt
Download as CSV file: xf-fx60177-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 60-177 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.4648   0.10214   0.09781  -0.0525   1.0001   0.0527
 -11.750  -0.6049   0.08129   0.07643  -0.0629   1.0001   0.0454
 -11.500  -0.6186   0.07717   0.07224  -0.0619   1.0001   0.0447
 -11.250  -0.7210   0.07789   0.07246  -0.0621   1.0001   0.0444
 -11.000  -0.7414   0.07481   0.06932  -0.0595   1.0001   0.0440
 -10.750  -0.7650   0.07215   0.06658  -0.0562   1.0001   0.0436
 -10.500  -0.7904   0.06991   0.06425  -0.0522   1.0001   0.0433
 -10.250  -0.8170   0.06796   0.06222  -0.0475   1.0001   0.0430
 -10.000  -0.8373   0.06532   0.05943  -0.0440   1.0001   0.0425
  -9.750  -0.8532   0.06235   0.05626  -0.0407   1.0001   0.0420
  -9.500  -0.8652   0.05917   0.05281  -0.0376   1.0001   0.0413
  -9.250  -0.8731   0.05584   0.04916  -0.0347   1.0001   0.0407
  -9.000  -0.8756   0.05253   0.04546  -0.0322   1.0001   0.0402
  -8.750  -0.8723   0.04946   0.04202  -0.0301   1.0001   0.0400
  -8.500  -0.8640   0.04683   0.03906  -0.0283   1.0001   0.0403
  -8.250  -0.8526   0.04464   0.03658  -0.0267   1.0001   0.0414
  -8.000  -0.8392   0.04267   0.03427  -0.0252   1.0001   0.0432
  -7.750  -0.8241   0.04114   0.03227  -0.0238   1.0001   0.0451
  -7.500  -0.8073   0.03872   0.02996  -0.0225   1.0001   0.0480
  -7.250  -0.7898   0.03734   0.02847  -0.0211   1.0001   0.0519
  -7.000  -0.7716   0.03567   0.02664  -0.0194   1.0001   0.0566
  -6.750  -0.7549   0.03472   0.02574  -0.0185   1.0001   0.0645
  -6.500  -0.7380   0.03356   0.02468  -0.0176   1.0001   0.0735
  -6.250  -0.7199   0.03251   0.02358  -0.0162   1.0001   0.0817
  -6.000  -0.7017   0.03159   0.02274  -0.0151   1.0001   0.0909
  -5.750  -0.6836   0.03044   0.02174  -0.0140   1.0001   0.1016
  -5.500  -0.6632   0.02936   0.02077  -0.0138   1.0001   0.1220
  -5.250  -0.6361   0.02708   0.01932  -0.0163   1.0001   0.1980
  -5.000  -0.6100   0.02538   0.02009  -0.0174   1.0001   0.5421
  -4.750  -0.5974   0.02657   0.02136  -0.0134   1.0001   0.6015
  -4.500  -0.5843   0.02792   0.02262  -0.0096   1.0001   0.6338
  -4.250  -0.5749   0.02939   0.02402  -0.0047   1.0001   0.6527
  -4.000  -0.5638   0.03069   0.02522  -0.0005   1.0001   0.6676
  -3.750  -0.5521   0.03189   0.02633   0.0034   1.0001   0.6815
  -3.500  -0.4986   0.03617   0.03040   0.0033   0.9779   0.7013
  -3.250  -0.4707   0.03839   0.03250   0.0062   0.9663   0.7174
  -3.000  -0.4378   0.04001   0.03398   0.0072   0.9571   0.7313
  -2.750  -0.4150   0.04077   0.03462   0.0091   0.9478   0.7448
  -2.500  -0.3891   0.04152   0.03525   0.0103   0.9387   0.7589
  -2.250  -0.3580   0.04211   0.03570   0.0099   0.9315   0.7730
  -2.000  -0.3367   0.04240   0.03590   0.0119   0.9224   0.7814
  -1.750  -0.2970   0.04267   0.03603   0.0095   0.9154   0.7919
  -1.500  -0.2765   0.04240   0.03566   0.0097   0.9044   0.8019
  -1.250  -0.2480   0.04237   0.03553   0.0098   0.8951   0.8093
  -1.000  -0.2134   0.04230   0.03534   0.0076   0.8870   0.8200
  -0.750  -0.1934   0.04215   0.03514   0.0092   0.8772   0.8269
  -0.500  -0.1544   0.04205   0.03492   0.0060   0.8711   0.8356
  -0.250  -0.1383   0.04179   0.03463   0.0079   0.8604   0.8418
   0.000  -0.1041   0.04161   0.03435   0.0056   0.8524   0.8502
   0.250  -0.0750   0.04125   0.03394   0.0056   0.8427   0.8563
   0.500  -0.0529   0.04102   0.03366   0.0055   0.8318   0.8649
   0.750  -0.0106   0.04059   0.03317   0.0034   0.8258   0.8702
   1.000   0.0056   0.04036   0.03291   0.0044   0.8144   0.8762
   1.250   0.0495   0.03992   0.03242   0.0012   0.8095   0.8813
   1.500   0.0663   0.03960   0.03209   0.0026   0.7972   0.8865
   1.750   0.0921   0.03925   0.03172   0.0023   0.7869   0.8923
   2.000   0.1322   0.03858   0.03102   0.0003   0.7800   0.8972
   2.250   0.1536   0.03824   0.03068   0.0010   0.7684   0.9025
   2.500   0.1986   0.03747   0.02989  -0.0019   0.7635   0.9070
   2.750   0.2179   0.03710   0.02953  -0.0010   0.7509   0.9110
   3.000   0.2715   0.03586   0.02829  -0.0046   0.7471   0.9141
   3.250   0.2910   0.03543   0.02788  -0.0035   0.7339   0.9185
   3.500   0.3428   0.03409   0.02655  -0.0068   0.7310   0.9218
   3.750   0.3603   0.03377   0.02627  -0.0056   0.7178   0.9254
   4.000   0.4145   0.03216   0.02469  -0.0089   0.7153   0.9286
   4.250   0.4354   0.03159   0.02415  -0.0078   0.7023   0.9327
   4.500   0.4934   0.02964   0.02224  -0.0114   0.6998   0.9357
   4.750   0.5186   0.02890   0.02155  -0.0109   0.6867   0.9391
   5.000   0.5553   0.02788   0.02057  -0.0119   0.6755   0.9421
   5.250   0.6244   0.02599   0.01873  -0.0176   0.6692   0.9444
   5.500   0.6599   0.02514   0.01791  -0.0186   0.6545   0.9477
   5.750   0.7020   0.02424   0.01702  -0.0207   0.6384   0.9503
   6.000   0.7534   0.02339   0.01613  -0.0245   0.6187   0.9523
   6.250   0.7791   0.02308   0.01580  -0.0242   0.5957   0.9552
   6.500   0.8212   0.02271   0.01532  -0.0267   0.5721   0.9579
   6.750   0.8335   0.02271   0.01528  -0.0242   0.5498   0.9621
   7.000   0.8684   0.02272   0.01516  -0.0257   0.5253   0.9648
   7.250   0.8896   0.02292   0.01531  -0.0251   0.5025   0.9680
   7.500   0.9091   0.02315   0.01547  -0.0242   0.4806   0.9715
   7.750   0.9354   0.02344   0.01560  -0.0244   0.4586   0.9748
   8.000   0.9513   0.02382   0.01600  -0.0232   0.4372   0.9790
   8.250   0.9708   0.02423   0.01636  -0.0225   0.4175   0.9830
   8.500   0.9968   0.02476   0.01681  -0.0231   0.3980   0.9863
   8.750   1.0247   0.02536   0.01734  -0.0241   0.3794   0.9900
   9.000   1.0496   0.02597   0.01790  -0.0246   0.3621   0.9941
   9.250   1.0741   0.02663   0.01855  -0.0252   0.3452   0.9980
   9.500   1.0808   0.02707   0.01902  -0.0225   0.3325   0.9999
   9.750   1.0884   0.02766   0.01967  -0.0200   0.3201   0.9999
  10.000   1.1026   0.02836   0.02040  -0.0188   0.3072   0.9999
  10.250   1.1216   0.02913   0.02116  -0.0185   0.2945   0.9999
  10.500   1.1472   0.02998   0.02192  -0.0192   0.2820   0.9999
  10.750   1.1604   0.03091   0.02300  -0.0182   0.2705   0.9999
  11.000   1.1765   0.03193   0.02413  -0.0177   0.2589   0.9999
  11.250   1.1959   0.03291   0.02510  -0.0178   0.2476   0.9999
  11.500   1.2189   0.03386   0.02599  -0.0183   0.2362   0.9999
  11.750   1.2264   0.03514   0.02750  -0.0169   0.2262   0.9999
  12.000   1.2435   0.03634   0.02873  -0.0168   0.2159   0.9999
  12.250   1.2615   0.03744   0.02982  -0.0168   0.2057   0.9999
  12.500   1.2681   0.03899   0.03163  -0.0156   0.1969   0.9999
  12.750   1.2884   0.04024   0.03282  -0.0160   0.1877   0.9999
  13.000   1.2946   0.04186   0.03464  -0.0149   0.1794   0.9999
  13.250   1.3092   0.04347   0.03630  -0.0148   0.1710   0.9999
  13.500   1.3162   0.04516   0.03812  -0.0140   0.1632   0.9999
  13.750   1.3267   0.04701   0.04007  -0.0137   0.1559   0.9999
  14.000   1.3303   0.04894   0.04218  -0.0128   0.1492   0.9999
  14.250   1.3427   0.05071   0.04396  -0.0128   0.1426   0.9999
  14.500   1.3387   0.05322   0.04675  -0.0117   0.1373   0.9999
  14.750   1.3613   0.05442   0.04774  -0.0125   0.1302   0.9999
  15.000   1.3477   0.05770   0.05144  -0.0112   0.1266   0.9999
  15.250   1.3438   0.06045   0.05439  -0.0107   0.1220   0.9999
  15.500   1.3646   0.06170   0.05545  -0.0115   0.1159   0.9999
  15.750   1.3476   0.06568   0.05984  -0.0109   0.1133   0.9999
  16.000   1.3357   0.06962   0.06407  -0.0109   0.1103   0.9999
  16.250   1.3371   0.07237   0.06691  -0.0115   0.1066   0.9999
  16.500   1.3523   0.07406   0.06853  -0.0121   0.1022   0.9999
  16.750   1.3310   0.07938   0.07423  -0.0130   0.1005   0.9999
  17.000   1.3098   0.08514   0.08031  -0.0146   0.0987   0.9999
  17.250   1.2895   0.09116   0.08661  -0.0168   0.0969   0.9999
  17.500   1.2717   0.09721   0.09288  -0.0194   0.0951   0.9999
  17.750   1.3079   0.09548   0.09086  -0.0193   0.0892   0.9999
  18.000   1.2776   0.10354   0.09927  -0.0230   0.0886   0.9999
  18.250   1.2406   0.11335   0.10939  -0.0281   0.0886   0.9999
  18.500   1.1929   0.12597   0.12230  -0.0353   0.0895   0.9999
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