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GOE 703 AIRFOIL (goe703-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 703 AIRFOIL (goe703-il)
Reynolds number: 200,000
Max Cl/Cd: 49.14 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe703-il-200000-n5.txt
Download as CSV file: xf-goe703-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 703 AIRFOIL                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.7644   0.10082   0.09523  -0.0696   1.0000   0.0381
 -17.750  -0.8266   0.08382   0.07775  -0.0795   1.0000   0.0382
 -17.500  -0.8376   0.07911   0.07293  -0.0817   1.0000   0.0383
 -17.250  -0.8483   0.07458   0.06828  -0.0837   1.0000   0.0384
 -17.000  -0.8565   0.07060   0.06420  -0.0852   1.0000   0.0386
 -16.750  -0.8632   0.06698   0.06049  -0.0863   1.0000   0.0388
 -16.500  -0.8686   0.06368   0.05710  -0.0871   1.0000   0.0389
 -16.250  -0.8735   0.06060   0.05392  -0.0876   1.0000   0.0392
 -16.000  -0.8783   0.05766   0.05088  -0.0878   1.0000   0.0394
 -15.750  -0.8820   0.05502   0.04815  -0.0877   1.0000   0.0396
 -15.500  -0.8849   0.05256   0.04558  -0.0872   1.0000   0.0398
 -15.250  -0.8871   0.05030   0.04322  -0.0865   1.0000   0.0401
 -15.000  -0.8885   0.04823   0.04106  -0.0855   1.0000   0.0404
 -14.750  -0.8890   0.04632   0.03905  -0.0843   1.0000   0.0406
 -14.500  -0.8889   0.04454   0.03717  -0.0828   1.0000   0.0410
 -14.250  -0.8871   0.04294   0.03548  -0.0812   1.0000   0.0412
 -14.000  -0.8854   0.04144   0.03389  -0.0794   1.0000   0.0415
 -13.750  -0.8830   0.04003   0.03239  -0.0774   1.0000   0.0418
 -13.500  -0.8801   0.03874   0.03100  -0.0753   1.0000   0.0421
 -13.250  -0.8767   0.03757   0.02975  -0.0730   1.0000   0.0424
 -13.000  -0.8731   0.03649   0.02859  -0.0706   1.0000   0.0427
 -12.750  -0.8698   0.03546   0.02755  -0.0680   1.0000   0.0431
 -12.500  -0.8673   0.03455   0.02665  -0.0651   1.0000   0.0433
 -12.250  -0.8529   0.03346   0.02555  -0.0645   0.9982   0.0438
 -12.000  -0.8271   0.03218   0.02425  -0.0659   0.9919   0.0444
 -11.750  -0.8040   0.03102   0.02305  -0.0667   0.9852   0.0450
 -11.500  -0.7811   0.02995   0.02192  -0.0673   0.9777   0.0458
 -11.250  -0.7590   0.02896   0.02087  -0.0676   0.9683   0.0468
 -11.000  -0.7373   0.02804   0.01985  -0.0677   0.9577   0.0476
 -10.750  -0.7138   0.02700   0.01881  -0.0683   0.9491   0.0485
 -10.500  -0.6890   0.02607   0.01786  -0.0689   0.9396   0.0494
 -10.250  -0.6609   0.02516   0.01692  -0.0702   0.9312   0.0507
 -10.000  -0.6296   0.02427   0.01596  -0.0719   0.9227   0.0520
  -9.750  -0.5937   0.02339   0.01500  -0.0746   0.9150   0.0536
  -9.500  -0.5593   0.02248   0.01408  -0.0771   0.9049   0.0553
  -9.250  -0.5220   0.02168   0.01321  -0.0799   0.8954   0.0578
  -9.000  -0.4874   0.02093   0.01241  -0.0822   0.8838   0.0604
  -8.750  -0.4542   0.02025   0.01168  -0.0841   0.8718   0.0644
  -8.500  -0.4218   0.01962   0.01101  -0.0857   0.8592   0.0685
  -8.250  -0.3973   0.01913   0.01048  -0.0856   0.8456   0.0737
  -8.000  -0.3724   0.01864   0.00996  -0.0856   0.8338   0.0812
  -7.750  -0.3520   0.01821   0.00955  -0.0846   0.8210   0.0907
  -7.500  -0.3321   0.01782   0.00918  -0.0834   0.8088   0.1034
  -7.250  -0.3118   0.01749   0.00884  -0.0823   0.7965   0.1181
  -7.000  -0.2938   0.01721   0.00857  -0.0806   0.7843   0.1314
  -6.750  -0.2739   0.01695   0.00829  -0.0792   0.7730   0.1443
  -6.500  -0.2567   0.01670   0.00805  -0.0773   0.7610   0.1557
  -6.250  -0.2380   0.01647   0.00780  -0.0757   0.7497   0.1667
  -6.000  -0.2196   0.01626   0.00757  -0.0739   0.7378   0.1779
  -5.750  -0.2012   0.01607   0.00735  -0.0722   0.7266   0.1895
  -5.500  -0.1833   0.01586   0.00714  -0.0703   0.7159   0.2012
  -5.250  -0.1654   0.01566   0.00694  -0.0685   0.7060   0.2138
  -4.750  -0.1295   0.01529   0.00657  -0.0647   0.6872   0.2429
  -4.500  -0.1128   0.01508   0.00639  -0.0626   0.6784   0.2611
  -4.250  -0.0959   0.01487   0.00621  -0.0605   0.6709   0.2794
  -4.000  -0.0797   0.01466   0.00604  -0.0583   0.6632   0.2974
  -3.750  -0.0629   0.01447   0.00585  -0.0562   0.6562   0.3148
  -3.500  -0.0476   0.01425   0.00569  -0.0537   0.6495   0.3353
  -3.250  -0.0344   0.01400   0.00554  -0.0509   0.6428   0.3613
  -3.000  -0.0241   0.01371   0.00537  -0.0474   0.6368   0.3975
  -2.750  -0.0177   0.01337   0.00523  -0.0432   0.6315   0.4503
  -2.500  -0.0145   0.01301   0.00516  -0.0381   0.6255   0.5147
  -2.250  -0.0056   0.01269   0.00515  -0.0341   0.6198   0.5872
  -2.000   0.0365   0.01260   0.00538  -0.0367   0.6144   0.6740
  -1.750   0.1028   0.01306   0.00601  -0.0439   0.6079   0.7300
  -1.500   0.1445   0.01345   0.00640  -0.0461   0.6016   0.7562
  -1.250   0.1742   0.01371   0.00660  -0.0461   0.5959   0.7741
  -1.000   0.2027   0.01397   0.00681  -0.0459   0.5908   0.7877
  -0.750   0.2322   0.01424   0.00707  -0.0458   0.5848   0.7981
  -0.500   0.2486   0.01433   0.00712  -0.0433   0.5794   0.8115
  -0.250   0.2820   0.01472   0.00744  -0.0440   0.5743   0.8196
   0.000   0.3012   0.01494   0.00762  -0.0419   0.5694   0.8315
   0.250   0.3337   0.01535   0.00803  -0.0424   0.5636   0.8382
   0.500   0.3502   0.01550   0.00815  -0.0398   0.5584   0.8487
   0.750   0.3892   0.01593   0.00849  -0.0417   0.5535   0.8524
   1.000   0.4171   0.01619   0.00874  -0.0414   0.5484   0.8589
   1.250   0.4364   0.01634   0.00890  -0.0396   0.5430   0.8671
   1.500   0.4759   0.01670   0.00921  -0.0416   0.5373   0.8705
   1.750   0.5073   0.01697   0.00940  -0.0421   0.5325   0.8761
   2.000   0.5203   0.01704   0.00951  -0.0391   0.5273   0.8843
   2.250   0.5537   0.01720   0.00967  -0.0402   0.5214   0.8864
   2.500   0.5838   0.01733   0.00974  -0.0407   0.5159   0.8889
   2.750   0.6100   0.01744   0.00984  -0.0404   0.5106   0.8925
   3.000   0.6136   0.01745   0.00987  -0.0356   0.5055   0.9010
   3.250   0.6458   0.01757   0.00998  -0.0366   0.4998   0.9026
   3.500   0.6761   0.01769   0.01004  -0.0372   0.4942   0.9045
   3.750   0.7027   0.01780   0.01019  -0.0370   0.4866   0.9072
   4.000   0.7251   0.01789   0.01026  -0.0360   0.4794   0.9109
   4.250   0.7280   0.01795   0.01029  -0.0311   0.4740   0.9183
   4.500   0.7571   0.01806   0.01043  -0.0316   0.4655   0.9200
   4.750   0.7835   0.01817   0.01049  -0.0315   0.4577   0.9220
   5.000   0.8081   0.01829   0.01064  -0.0310   0.4496   0.9246
   5.250   0.8278   0.01842   0.01075  -0.0296   0.4415   0.9283
   5.750   0.8548   0.01866   0.01099  -0.0243   0.4259   0.9368
   6.000   0.8796   0.01882   0.01113  -0.0240   0.4170   0.9390
   6.250   0.9000   0.01898   0.01129  -0.0228   0.4074   0.9418
   6.500   0.9151   0.01915   0.01145  -0.0206   0.4004   0.9456
   6.750   0.9180   0.01931   0.01164  -0.0159   0.3938   0.9516
   7.000   0.9403   0.01948   0.01180  -0.0152   0.3863   0.9536
   7.250   0.9603   0.01965   0.01200  -0.0141   0.3790   0.9560
   7.500   0.9759   0.01987   0.01222  -0.0122   0.3715   0.9593
   7.750   0.9837   0.02014   0.01248  -0.0087   0.3653   0.9644
   8.000   0.9986   0.02038   0.01276  -0.0068   0.3575   0.9673
   8.250   1.0164   0.02069   0.01304  -0.0057   0.3491   0.9696
   8.500   1.0329   0.02102   0.01340  -0.0043   0.3389   0.9725
   8.750   1.0445   0.02147   0.01383  -0.0021   0.3300   0.9764
   9.000   1.0536   0.02194   0.01432   0.0005   0.3207   0.9802
   9.250   1.0705   0.02243   0.01481   0.0013   0.3111   0.9822
   9.500   1.0855   0.02299   0.01537   0.0024   0.3006   0.9847
   9.750   1.1004   0.02362   0.01602   0.0034   0.2910   0.9877
  10.000   1.1104   0.02445   0.01684   0.0049   0.2805   0.9910
  10.250   1.1228   0.02525   0.01765   0.0060   0.2687   0.9933
  10.500   1.1355   0.02614   0.01855   0.0068   0.2580   0.9957
  10.750   1.1464   0.02724   0.01963   0.0075   0.2472   0.9982
  11.000   1.1576   0.02836   0.02076   0.0082   0.2354   1.0000
  11.250   1.1522   0.02953   0.02193   0.0119   0.2269   1.0000
  11.500   1.1474   0.03076   0.02316   0.0154   0.2185   1.0000
  11.750   1.1422   0.03209   0.02449   0.0187   0.2105   1.0000
  12.000   1.1356   0.03361   0.02599   0.0219   0.2022   1.0000
  12.250   1.1314   0.03507   0.02745   0.0247   0.1955   1.0000
  12.500   1.1259   0.03670   0.02909   0.0275   0.1885   1.0000
  12.750   1.1213   0.03837   0.03076   0.0300   0.1825   1.0000
  13.000   1.1183   0.04002   0.03243   0.0322   0.1768   1.0000
  13.250   1.1137   0.04188   0.03428   0.0344   0.1722   1.0000
  13.500   1.1133   0.04348   0.03592   0.0362   0.1683   1.0000
  13.750   1.1127   0.04516   0.03763   0.0379   0.1642   1.0000
  14.000   1.1096   0.04713   0.03960   0.0396   0.1600   1.0000
  14.250   1.1082   0.04901   0.04150   0.0410   0.1563   1.0000
  14.500   1.1094   0.05074   0.04328   0.0423   0.1526   1.0000
  14.750   1.1088   0.05268   0.04524   0.0436   0.1489   1.0000
  15.000   1.1067   0.05479   0.04735   0.0447   0.1455   1.0000
  15.250   1.1085   0.05661   0.04921   0.0457   0.1429   1.0000
  15.500   1.1107   0.05845   0.05113   0.0466   0.1396   1.0000
  15.750   1.1112   0.06050   0.05322   0.0474   0.1365   1.0000
  16.000   1.1105   0.06270   0.05543   0.0481   0.1334   1.0000
  16.250   1.1112   0.06483   0.05759   0.0487   0.1307   1.0000
  16.500   1.1134   0.06687   0.05972   0.0492   0.1275   1.0000
  16.750   1.1139   0.06913   0.06202   0.0496   0.1244   1.0000
  17.000   1.1122   0.07166   0.06457   0.0499   0.1212   1.0000
  17.250   1.1122   0.07405   0.06703   0.0502   0.1180   1.0000
  17.500   1.1127   0.07648   0.06954   0.0503   0.1145   1.0000
  17.750   1.1106   0.07923   0.07233   0.0503   0.1111   1.0000
  18.000   1.1084   0.08203   0.07515   0.0503   0.1079   1.0000
  18.250   1.1080   0.08470   0.07794   0.0501   0.1040   1.0000
  18.500   1.1039   0.08786   0.08114   0.0498   0.1000   1.0000
  18.750   1.1010   0.09094   0.08430   0.0494   0.0959   1.0000
  19.000   1.0975   0.09414   0.08755   0.0489   0.0913   1.0000
  19.250   1.0930   0.09751   0.09098   0.0483   0.0870   1.0000
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