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FX 83-W-227 (fx83w227-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX 83-W-227 (fx83w227-il)
Reynolds number: 200,000
Max Cl/Cd: 49.98 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx83w227-il-200000-n5.txt
Download as CSV file: xf-fx83w227-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 83-W-227                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -0.6859   0.11101   0.10618  -0.0836   1.0000   0.0549
 -19.000  -0.7364   0.09975   0.09467  -0.0892   1.0000   0.0556
 -18.750  -0.7664   0.09240   0.08714  -0.0925   1.0000   0.0563
 -18.500  -0.7913   0.08616   0.08073  -0.0950   1.0000   0.0571
 -18.250  -0.8116   0.08089   0.07529  -0.0968   1.0000   0.0578
 -18.000  -0.8301   0.07614   0.07036  -0.0982   1.0000   0.0585
 -17.750  -0.8415   0.07261   0.06674  -0.0987   1.0000   0.0591
 -17.500  -0.8463   0.07016   0.06428  -0.0985   1.0000   0.0598
 -17.250  -0.8527   0.06764   0.06173  -0.0983   1.0000   0.0604
 -17.000  -0.8563   0.06497   0.05901  -0.0987   0.9996   0.0611
 -16.750  -0.8469   0.06168   0.05562  -0.1020   0.9972   0.0622
 -16.500  -0.8379   0.05852   0.05233  -0.1052   0.9943   0.0634
 -16.250  -0.8292   0.05550   0.04915  -0.1080   0.9913   0.0645
 -16.000  -0.8208   0.05261   0.04607  -0.1105   0.9876   0.0657
 -15.750  -0.8051   0.05058   0.04405  -0.1127   0.9845   0.0667
 -15.500  -0.7889   0.04851   0.04193  -0.1152   0.9819   0.0678
 -15.250  -0.7772   0.04651   0.03986  -0.1166   0.9766   0.0690
 -15.000  -0.7621   0.04457   0.03783  -0.1185   0.9724   0.0703
 -14.750  -0.7443   0.04269   0.03583  -0.1208   0.9695   0.0718
 -14.500  -0.7329   0.04103   0.03403  -0.1213   0.9624   0.0730
 -14.250  -0.7145   0.03943   0.03244  -0.1230   0.9582   0.0743
 -14.000  -0.6981   0.03794   0.03092  -0.1241   0.9528   0.0756
 -13.750  -0.6828   0.03653   0.02945  -0.1249   0.9462   0.0771
 -13.500  -0.6610   0.03512   0.02796  -0.1267   0.9422   0.0790
 -13.250  -0.6455   0.03393   0.02665  -0.1270   0.9340   0.0807
 -13.000  -0.6235   0.03264   0.02532  -0.1286   0.9288   0.0824
 -12.750  -0.5993   0.03139   0.02405  -0.1306   0.9239   0.0841
 -12.500  -0.5789   0.03030   0.02290  -0.1316   0.9159   0.0861
 -12.250  -0.5502   0.02919   0.02170  -0.1339   0.9108   0.0886
 -12.000  -0.5274   0.02823   0.02065  -0.1350   0.9029   0.0910
 -11.750  -0.5028   0.02715   0.01956  -0.1367   0.8957   0.0933
 -11.500  -0.4774   0.02623   0.01858  -0.1382   0.8880   0.0959
 -11.250  -0.4525   0.02542   0.01766  -0.1394   0.8792   0.0989
 -11.000  -0.4279   0.02458   0.01676  -0.1405   0.8711   0.1019
 -10.750  -0.4091   0.02383   0.01597  -0.1405   0.8616   0.1047
 -10.500  -0.3868   0.02316   0.01522  -0.1409   0.8533   0.1082
 -10.250  -0.3685   0.02264   0.01458  -0.1403   0.8438   0.1113
 -10.000  -0.3512   0.02196   0.01388  -0.1398   0.8355   0.1146
  -9.750  -0.3381   0.02146   0.01334  -0.1383   0.8263   0.1183
  -9.500  -0.3184   0.02101   0.01277  -0.1377   0.8191   0.1225
  -9.250  -0.3079   0.02053   0.01228  -0.1356   0.8103   0.1259
  -9.000  -0.2937   0.02008   0.01178  -0.1340   0.8027   0.1301
  -8.750  -0.2783   0.01972   0.01135  -0.1325   0.7957   0.1351
  -8.500  -0.2674   0.01932   0.01094  -0.1301   0.7880   0.1395
  -8.250  -0.2526   0.01894   0.01050  -0.1284   0.7815   0.1446
  -8.000  -0.2393   0.01866   0.01017  -0.1263   0.7747   0.1502
  -7.750  -0.2293   0.01829   0.00981  -0.1236   0.7675   0.1556
  -7.500  -0.2139   0.01797   0.00943  -0.1218   0.7618   0.1625
  -7.250  -0.2039   0.01769   0.00915  -0.1189   0.7551   0.1687
  -7.000  -0.1933   0.01741   0.00887  -0.1161   0.7485   0.1763
  -6.750  -0.1792   0.01714   0.00855  -0.1138   0.7429   0.1848
  -6.500  -0.1707   0.01693   0.00836  -0.1104   0.7367   0.1935
  -6.250  -0.1618   0.01675   0.00818  -0.1071   0.7303   0.2026
  -6.000  -0.1491   0.01655   0.00796  -0.1044   0.7249   0.2146
  -5.750  -0.1379   0.01633   0.00777  -0.1015   0.7194   0.2270
  -5.500  -0.1274   0.01613   0.00762  -0.0984   0.7132   0.2405
  -5.250  -0.1136   0.01590   0.00741  -0.0959   0.7078   0.2572
  -5.000  -0.0971   0.01566   0.00718  -0.0940   0.7033   0.2764
  -4.750  -0.0871   0.01548   0.00709  -0.0907   0.6973   0.2957
  -4.500  -0.0741   0.01527   0.00694  -0.0880   0.6916   0.3173
  -4.250  -0.0577   0.01504   0.00676  -0.0859   0.6869   0.3421
  -4.000  -0.0428   0.01485   0.00663  -0.0836   0.6819   0.3670
  -3.750  -0.0308   0.01467   0.00656  -0.0806   0.6763   0.3917
  -3.500  -0.0152   0.01450   0.00645  -0.0783   0.6711   0.4181
  -3.250   0.0040   0.01433   0.00633  -0.0767   0.6667   0.4458
  -3.000   0.0186   0.01422   0.00631  -0.0741   0.6615   0.4707
  -2.750   0.0341   0.01413   0.00630  -0.0717   0.6562   0.4953
  -2.500   0.0535   0.01406   0.00626  -0.0701   0.6512   0.5190
  -2.250   0.0769   0.01401   0.00619  -0.0692   0.6471   0.5412
  -2.000   0.0922   0.01400   0.00624  -0.0667   0.6416   0.5592
  -1.750   0.1102   0.01399   0.00626  -0.0647   0.6364   0.5762
  -1.500   0.1321   0.01398   0.00624  -0.0635   0.6317   0.5921
  -1.250   0.1561   0.01399   0.00622  -0.0627   0.6275   0.6073
  -1.000   0.1710   0.01402   0.00627  -0.0602   0.6219   0.6213
  -0.750   0.1900   0.01405   0.00633  -0.0584   0.6168   0.6350
  -0.500   0.2126   0.01407   0.00633  -0.0573   0.6123   0.6487
  -0.250   0.2341   0.01412   0.00633  -0.0561   0.6078   0.6620
   0.000   0.2492   0.01416   0.00643  -0.0535   0.6022   0.6724
   0.250   0.2670   0.01418   0.00643  -0.0515   0.5971   0.6834
   0.500   0.2907   0.01422   0.00645  -0.0507   0.5928   0.6932
   0.750   0.3086   0.01426   0.00646  -0.0488   0.5881   0.7031
   1.000   0.3235   0.01431   0.00656  -0.0463   0.5825   0.7113
   1.250   0.3422   0.01436   0.00657  -0.0445   0.5776   0.7206
   1.500   0.3671   0.01440   0.00658  -0.0440   0.5733   0.7282
   1.750   0.3830   0.01450   0.00670  -0.0417   0.5683   0.7370
   2.000   0.3981   0.01460   0.00681  -0.0394   0.5628   0.7454
   2.250   0.4192   0.01467   0.00689  -0.0381   0.5579   0.7532
   2.500   0.4426   0.01474   0.00688  -0.0374   0.5536   0.7625
   2.750   0.4564   0.01488   0.00711  -0.0348   0.5482   0.7707
   3.000   0.4731   0.01500   0.00725  -0.0328   0.5429   0.7799
   3.250   0.4944   0.01509   0.00731  -0.0317   0.5382   0.7883
   3.500   0.5148   0.01520   0.00742  -0.0304   0.5335   0.7972
   3.750   0.5286   0.01536   0.00763  -0.0280   0.5280   0.8069
   4.000   0.5484   0.01549   0.00779  -0.0267   0.5230   0.8161
   4.250   0.5705   0.01559   0.00785  -0.0258   0.5186   0.8261
   4.500   0.5898   0.01576   0.00809  -0.0245   0.5134   0.8363
   4.750   0.6076   0.01596   0.00834  -0.0230   0.5079   0.8480
   5.000   0.6336   0.01613   0.00853  -0.0230   0.5031   0.8595
   5.250   0.6654   0.01630   0.00868  -0.0242   0.4990   0.8712
   5.500   0.6912   0.01663   0.00912  -0.0245   0.4933   0.8857
   5.750   0.7257   0.01695   0.00948  -0.0265   0.4875   0.8983
   6.000   0.7650   0.01724   0.00974  -0.0294   0.4826   0.9104
   6.250   0.8016   0.01761   0.01015  -0.0319   0.4779   0.9236
   6.500   0.8357   0.01802   0.01062  -0.0341   0.4721   0.9371
   6.750   0.8719   0.01838   0.01097  -0.0365   0.4670   0.9483
   7.000   0.9079   0.01871   0.01125  -0.0388   0.4623   0.9591
   7.250   0.9366   0.01920   0.01182  -0.0401   0.4570   0.9719
   7.500   0.9665   0.01964   0.01227  -0.0415   0.4518   0.9837
   7.750   0.9995   0.02004   0.01263  -0.0434   0.4469   0.9937
   8.000   1.0265   0.02054   0.01314  -0.0444   0.4423   1.0000
   8.250   1.0295   0.02094   0.01356  -0.0407   0.4376   1.0000
   8.500   1.0375   0.02132   0.01393  -0.0379   0.4332   1.0000
   8.750   1.0500   0.02165   0.01421  -0.0358   0.4291   1.0000
   9.000   1.0598   0.02210   0.01467  -0.0334   0.4248   1.0000
   9.250   1.0660   0.02269   0.01531  -0.0306   0.4199   1.0000
   9.500   1.0764   0.02320   0.01582  -0.0284   0.4154   1.0000
   9.750   1.0908   0.02361   0.01621  -0.0268   0.4114   1.0000
  10.000   1.1017   0.02418   0.01679  -0.0249   0.4071   1.0000
  10.250   1.1082   0.02494   0.01762  -0.0225   0.4022   1.0000
  10.500   1.1191   0.02557   0.01826  -0.0207   0.3978   1.0000
  10.750   1.1338   0.02607   0.01873  -0.0193   0.3937   1.0000
  11.000   1.1444   0.02677   0.01947  -0.0176   0.3894   1.0000
  11.250   1.1500   0.02773   0.02050  -0.0154   0.3845   1.0000
  11.500   1.1601   0.02851   0.02130  -0.0137   0.3798   1.0000
  11.750   1.1752   0.02905   0.02181  -0.0126   0.3756   1.0000
  12.000   1.1809   0.03011   0.02295  -0.0107   0.3706   1.0000
  12.250   1.1859   0.03126   0.02417  -0.0088   0.3653   1.0000
  12.500   1.1966   0.03211   0.02501  -0.0075   0.3604   1.0000
  12.750   1.2099   0.03282   0.02572  -0.0064   0.3561   1.0000
  13.000   1.2107   0.03437   0.02739  -0.0044   0.3506   1.0000
  13.250   1.2174   0.03556   0.02862  -0.0030   0.3453   1.0000
  13.500   1.2305   0.03632   0.02934  -0.0021   0.3405   1.0000
  13.750   1.2297   0.03815   0.03128  -0.0003   0.3344   1.0000
  14.000   1.2326   0.03970   0.03286   0.0011   0.3275   1.0000
  14.250   1.2388   0.04104   0.03419   0.0023   0.3211   1.0000
  14.500   1.2362   0.04318   0.03643   0.0038   0.3136   1.0000
  14.750   1.2425   0.04458   0.03779   0.0048   0.3070   1.0000
  15.000   1.2403   0.04686   0.04017   0.0060   0.2999   1.0000
  15.250   1.2426   0.04873   0.04206   0.0070   0.2929   1.0000
  15.500   1.2451   0.05065   0.04402   0.0079   0.2868   1.0000
  15.750   1.2439   0.05300   0.04645   0.0087   0.2799   1.0000
  16.000   1.2488   0.05472   0.04814   0.0094   0.2736   1.0000
  16.250   1.2456   0.05739   0.05093   0.0101   0.2668   1.0000
  16.500   1.2454   0.05972   0.05327   0.0108   0.2595   1.0000
  16.750   1.2450   0.06216   0.05577   0.0113   0.2532   1.0000
  17.000   1.2422   0.06490   0.05856   0.0118   0.2455   1.0000
  17.250   1.2404   0.06753   0.06121   0.0122   0.2382   1.0000
  17.500   1.2357   0.07057   0.06431   0.0125   0.2302   1.0000
  17.750   1.2328   0.07341   0.06716   0.0127   0.2224   1.0000
  18.000   1.2276   0.07658   0.07037   0.0129   0.2142   1.0000
  18.250   1.2221   0.07982   0.07364   0.0129   0.2058   1.0000
  18.500   1.2170   0.08305   0.07687   0.0129   0.1976   1.0000
  18.750   1.2106   0.08650   0.08036   0.0128   0.1889   1.0000
  19.000   1.2038   0.08999   0.08382   0.0126   0.1806   1.0000
  19.250   1.1972   0.09355   0.08743   0.0123   0.1718   1.0000
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