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S1012 (s1012-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: S1012 (s1012-il)
Reynolds number: 200,000
Max Cl/Cd: 39.99 at α=9.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1012-il-200000-n5.txt
Download as CSV file: xf-s1012-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1012                                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.9459   0.09927   0.09494  -0.0227   1.0000   0.0243
 -16.250  -0.9889   0.08587   0.08124  -0.0315   1.0000   0.0241
 -16.000  -1.0124   0.07735   0.07253  -0.0370   1.0000   0.0242
 -15.750  -1.0290   0.07069   0.06572  -0.0411   1.0000   0.0244
 -15.500  -1.0438   0.06484   0.05969  -0.0443   1.0000   0.0245
 -15.250  -1.0548   0.06007   0.05479  -0.0466   1.0000   0.0247
 -15.000  -1.0632   0.05604   0.05062  -0.0481   1.0000   0.0250
 -14.750  -1.0701   0.05248   0.04692  -0.0490   1.0000   0.0253
 -14.500  -1.0752   0.04936   0.04366  -0.0493   1.0000   0.0256
 -14.250  -1.0791   0.04652   0.04068  -0.0492   1.0000   0.0260
 -14.000  -1.0805   0.04411   0.03813  -0.0488   1.0000   0.0266
 -13.750  -1.0808   0.04185   0.03572  -0.0480   1.0000   0.0272
 -13.500  -1.0794   0.03979   0.03348  -0.0471   1.0000   0.0280
 -13.250  -1.0764   0.03789   0.03136  -0.0460   1.0000   0.0289
 -13.000  -1.0722   0.03612   0.02945  -0.0447   1.0000   0.0296
 -12.750  -1.0670   0.03460   0.02788  -0.0434   1.0000   0.0303
 -12.500  -1.0595   0.03328   0.02648  -0.0420   1.0000   0.0311
 -12.250  -1.0507   0.03206   0.02515  -0.0406   1.0000   0.0320
 -12.000  -1.0409   0.03085   0.02383  -0.0392   1.0000   0.0331
 -11.750  -1.0297   0.02971   0.02255  -0.0378   1.0000   0.0343
 -11.500  -1.0171   0.02865   0.02133  -0.0364   1.0000   0.0357
 -11.250  -1.0065   0.02761   0.02028  -0.0348   1.0000   0.0369
 -11.000  -0.9935   0.02681   0.01942  -0.0333   1.0000   0.0385
 -10.750  -0.9794   0.02602   0.01855  -0.0319   1.0000   0.0402
 -10.500  -0.9644   0.02523   0.01764  -0.0304   1.0000   0.0420
 -10.250  -0.9506   0.02441   0.01676  -0.0287   1.0000   0.0435
 -10.000  -0.9386   0.02376   0.01611  -0.0267   1.0000   0.0454
  -9.750  -0.9236   0.02323   0.01553  -0.0252   0.9967   0.0476
  -9.250  -0.8682   0.02172   0.01385  -0.0270   0.9732   0.0535
  -9.000  -0.8405   0.02111   0.01320  -0.0278   0.9654   0.0569
  -8.750  -0.8123   0.02054   0.01251  -0.0284   0.9587   0.0604
  -8.500  -0.7871   0.01988   0.01183  -0.0287   0.9523   0.0640
  -8.250  -0.7620   0.01939   0.01129  -0.0287   0.9464   0.0678
  -8.000  -0.7360   0.01893   0.01072  -0.0288   0.9417   0.0718
  -7.750  -0.7143   0.01839   0.01019  -0.0281   0.9362   0.0759
  -7.500  -0.6910   0.01798   0.00974  -0.0277   0.9314   0.0805
  -7.250  -0.6666   0.01760   0.00927  -0.0273   0.9277   0.0853
  -7.000  -0.6444   0.01715   0.00885  -0.0266   0.9237   0.0906
  -6.750  -0.6214   0.01683   0.00846  -0.0260   0.9193   0.0964
  -6.500  -0.5993   0.01644   0.00808  -0.0252   0.9154   0.1024
  -6.250  -0.5760   0.01613   0.00774  -0.0245   0.9123   0.1098
  -6.000  -0.5535   0.01578   0.00741  -0.0238   0.9095   0.1173
  -5.750  -0.5302   0.01551   0.00711  -0.0232   0.9063   0.1259
  -5.500  -0.5077   0.01518   0.00683  -0.0225   0.9032   0.1360
  -5.250  -0.4846   0.01489   0.00657  -0.0218   0.9005   0.1475
  -5.000  -0.4616   0.01460   0.00631  -0.0211   0.8979   0.1607
  -4.750  -0.4387   0.01431   0.00607  -0.0203   0.8955   0.1769
  -4.500  -0.4160   0.01402   0.00586  -0.0196   0.8927   0.1968
  -4.250  -0.3934   0.01373   0.00567  -0.0189   0.8900   0.2209
  -4.000  -0.3715   0.01340   0.00548  -0.0181   0.8875   0.2523
  -3.750  -0.3503   0.01303   0.00529  -0.0171   0.8849   0.2929
  -3.500  -0.3302   0.01260   0.00510  -0.0159   0.8823   0.3463
  -3.250  -0.3117   0.01210   0.00490  -0.0144   0.8801   0.4163
  -3.000  -0.2950   0.01156   0.00479  -0.0125   0.8775   0.5050
  -2.750  -0.2783   0.01114   0.00496  -0.0101   0.8743   0.6156
  -2.500  -0.2539   0.01129   0.00544  -0.0087   0.8719   0.6945
  -2.250  -0.2287   0.01145   0.00560  -0.0079   0.8696   0.7280
  -2.000  -0.2033   0.01156   0.00569  -0.0072   0.8673   0.7482
  -1.750  -0.1773   0.01169   0.00578  -0.0065   0.8654   0.7635
  -1.500  -0.1508   0.01182   0.00589  -0.0060   0.8635   0.7753
  -1.250  -0.1265   0.01196   0.00602  -0.0053   0.8600   0.7863
  -1.000  -0.1008   0.01211   0.00619  -0.0046   0.8568   0.7958
  -0.750  -0.0749   0.01224   0.00632  -0.0039   0.8538   0.8048
  -0.500  -0.0499   0.01236   0.00643  -0.0029   0.8508   0.8166
  -0.250  -0.0234   0.01260   0.00671  -0.0017   0.8476   0.8291
   0.000   0.0000   0.01277   0.00692   0.0000   0.8394   0.8394
   0.250   0.0234   0.01260   0.00670   0.0017   0.8290   0.8476
   0.500   0.0499   0.01237   0.00643   0.0029   0.8166   0.8508
   0.750   0.0749   0.01224   0.00632   0.0039   0.8048   0.8538
   1.000   0.1009   0.01212   0.00619   0.0046   0.7959   0.8568
   1.250   0.1265   0.01196   0.00602   0.0053   0.7864   0.8600
   1.500   0.1508   0.01182   0.00590   0.0060   0.7754   0.8635
   1.750   0.1773   0.01169   0.00578   0.0065   0.7637   0.8654
   2.000   0.2033   0.01156   0.00569   0.0072   0.7481   0.8674
   2.250   0.2287   0.01145   0.00560   0.0079   0.7280   0.8696
   2.500   0.2539   0.01130   0.00545   0.0087   0.6949   0.8719
   2.750   0.2783   0.01114   0.00496   0.0101   0.6153   0.8743
   3.000   0.2950   0.01155   0.00479   0.0125   0.5053   0.8774
   3.250   0.3116   0.01210   0.00490   0.0144   0.4163   0.8801
   3.500   0.3302   0.01260   0.00510   0.0159   0.3460   0.8823
   3.750   0.3504   0.01303   0.00529   0.0171   0.2934   0.8849
   4.000   0.3715   0.01340   0.00548   0.0181   0.2526   0.8874
   4.250   0.3935   0.01373   0.00566   0.0189   0.2211   0.8900
   4.500   0.4160   0.01402   0.00586   0.0196   0.1968   0.8927
   4.750   0.4387   0.01431   0.00607   0.0203   0.1771   0.8955
   5.000   0.4616   0.01460   0.00631   0.0211   0.1607   0.8979
   5.250   0.4846   0.01489   0.00657   0.0218   0.1474   0.9005
   5.500   0.5077   0.01518   0.00683   0.0225   0.1359   0.9033
   5.750   0.5301   0.01551   0.00711   0.0232   0.1259   0.9063
   6.000   0.5535   0.01578   0.00740   0.0238   0.1173   0.9095
   6.250   0.5761   0.01612   0.00774   0.0245   0.1096   0.9123
   6.500   0.5993   0.01644   0.00808   0.0252   0.1024   0.9154
   6.750   0.6214   0.01683   0.00846   0.0260   0.0965   0.9193
   7.000   0.6444   0.01715   0.00885   0.0266   0.0906   0.9237
   7.250   0.6666   0.01760   0.00927   0.0273   0.0852   0.9277
   7.500   0.6910   0.01799   0.00974   0.0277   0.0805   0.9315
   7.750   0.7143   0.01839   0.01019   0.0281   0.0759   0.9362
   8.000   0.7361   0.01892   0.01071   0.0288   0.0718   0.9418
   8.250   0.7621   0.01939   0.01128   0.0287   0.0679   0.9464
   8.500   0.7872   0.01988   0.01182   0.0286   0.0639   0.9524
   8.750   0.8124   0.02054   0.01250   0.0284   0.0604   0.9587
   9.000   0.8407   0.02110   0.01319   0.0277   0.0568   0.9654
   9.250   0.8685   0.02172   0.01385   0.0269   0.0535   0.9732
   9.750   0.9239   0.02322   0.01553   0.0251   0.0476   0.9968
  10.000   0.9387   0.02377   0.01612   0.0267   0.0454   1.0000
  10.250   0.9508   0.02442   0.01676   0.0287   0.0436   1.0000
  10.500   0.9647   0.02523   0.01764   0.0303   0.0420   1.0000
  10.750   0.9796   0.02602   0.01855   0.0318   0.0401   1.0000
  11.000   0.9938   0.02680   0.01942   0.0333   0.0384   1.0000
  11.250   1.0068   0.02763   0.02030   0.0348   0.0370   1.0000
  11.500   1.0173   0.02866   0.02134   0.0364   0.0356   1.0000
  11.750   1.0301   0.02971   0.02255   0.0377   0.0343   1.0000
  12.000   1.0413   0.03086   0.02383   0.0392   0.0331   1.0000
  12.250   1.0511   0.03205   0.02515   0.0406   0.0320   1.0000
  12.500   1.0599   0.03328   0.02647   0.0420   0.0310   1.0000
  12.750   1.0673   0.03459   0.02787   0.0433   0.0303   1.0000
  13.000   1.0728   0.03610   0.02943   0.0446   0.0296   1.0000
  13.250   1.0770   0.03788   0.03137   0.0459   0.0288   1.0000
  13.500   1.0798   0.03982   0.03351   0.0470   0.0280   1.0000
  13.750   1.0812   0.04187   0.03574   0.0480   0.0272   1.0000
  14.000   1.0809   0.04415   0.03818   0.0487   0.0266   1.0000
  14.250   1.0794   0.04659   0.04076   0.0491   0.0261   1.0000
  14.500   1.0764   0.04929   0.04359   0.0492   0.0256   1.0000
  14.750   1.0716   0.05238   0.04682   0.0489   0.0253   1.0000
  15.000   1.0650   0.05590   0.05046   0.0480   0.0249   1.0000
  15.250   1.0559   0.06002   0.05473   0.0465   0.0247   1.0000
  15.500   1.0449   0.06480   0.05966   0.0442   0.0245   1.0000
  15.750   1.0312   0.07045   0.06546   0.0411   0.0243   1.0000
  16.000   1.0138   0.07726   0.07243   0.0369   0.0242   1.0000
  16.250   0.9914   0.08556   0.08092   0.0315   0.0241   1.0000
  16.500   0.9484   0.09894   0.09460   0.0227   0.0243   1.0000
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