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WORTMANN FX 73-170 (fx73170-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 73-170 (fx73170-il)
Reynolds number: 500,000
Max Cl/Cd: 110.3 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx73170-il-500000.txt
Download as CSV file: xf-fx73170-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 73-170                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.0759   0.10061   0.09691  -0.1318   0.7821   0.0233
 -12.250  -0.0834   0.09271   0.08902  -0.1367   0.7809   0.0238
 -12.000  -0.0787   0.08860   0.08492  -0.1394   0.7798   0.0238
 -11.750  -0.0733   0.08554   0.08188  -0.1409   0.7785   0.0240
 -11.500  -0.0644   0.08352   0.07987  -0.1419   0.7771   0.0244
 -11.250  -0.0623   0.07918   0.07555  -0.1448   0.7758   0.0246
 -11.000  -0.0580   0.07566   0.07205  -0.1472   0.7743   0.0251
 -10.750  -0.0076   0.05060   0.04714  -0.1509   0.7678   0.0283
 -10.500  -0.0316   0.04305   0.03953  -0.1556   0.7667   0.0280
 -10.250  -0.0590   0.03715   0.03353  -0.1588   0.7654   0.0279
 -10.000  -0.0815   0.03303   0.02933  -0.1599   0.7639   0.0278
  -9.750  -0.1055   0.02977   0.02597  -0.1596   0.7623   0.0280
  -9.500  -0.1348   0.02757   0.02361  -0.1577   0.7603   0.0285
  -9.250  -0.1639   0.02757   0.02342  -0.1526   0.7578   0.0290
  -9.000  -0.2359   0.03044   0.02524  -0.1544   0.7591   0.0180
  -8.750  -0.2326   0.02772   0.02224  -0.1521   0.7574   0.0174
  -8.500  -0.2236   0.02522   0.01942  -0.1501   0.7557   0.0170
  -8.250  -0.2078   0.02367   0.01762  -0.1488   0.7540   0.0174
  -8.000  -0.1891   0.02197   0.01568  -0.1479   0.7526   0.0172
  -7.750  -0.1681   0.02080   0.01432  -0.1472   0.7512   0.0177
  -7.500  -0.1457   0.01986   0.01322  -0.1466   0.7498   0.0180
  -7.250  -0.1239   0.01941   0.01262  -0.1458   0.7484   0.0187
  -7.000  -0.1036   0.01819   0.01136  -0.1449   0.7471   0.0195
  -6.750  -0.0834   0.01745   0.01063  -0.1440   0.7456   0.0201
  -6.500  -0.0626   0.01691   0.01008  -0.1431   0.7440   0.0207
  -6.250  -0.0415   0.01641   0.00956  -0.1422   0.7423   0.0215
  -6.000  -0.0199   0.01596   0.00907  -0.1415   0.7407   0.0227
  -5.750   0.0026   0.01555   0.00860  -0.1408   0.7391   0.0235
  -5.500   0.0217   0.01484   0.00789  -0.1398   0.7378   0.0253
  -5.250   0.0457   0.01453   0.00756  -0.1396   0.7365   0.0276
  -5.000   0.0690   0.01414   0.00711  -0.1392   0.7353   0.0303
  -4.750   0.0929   0.01385   0.00680  -0.1389   0.7340   0.0338
  -4.500   0.1157   0.01355   0.00649  -0.1383   0.7327   0.0387
  -4.250   0.1379   0.01321   0.00621  -0.1377   0.7312   0.0504
  -4.000   0.1580   0.01264   0.00590  -0.1368   0.7294   0.1060
  -3.750   0.1750   0.01174   0.00558  -0.1358   0.7276   0.2511
  -3.500   0.1881   0.01061   0.00519  -0.1341   0.7259   0.4588
  -3.250   0.2096   0.01051   0.00547  -0.1330   0.7245   0.5863
  -3.000   0.2372   0.01072   0.00564  -0.1329   0.7232   0.6103
  -2.750   0.2653   0.01095   0.00583  -0.1329   0.7220   0.6258
  -2.500   0.2938   0.01125   0.00609  -0.1329   0.7209   0.6393
  -2.250   0.3225   0.01149   0.00624  -0.1331   0.7197   0.6494
  -2.000   0.3519   0.01193   0.00670  -0.1331   0.7184   0.6601
  -1.750   0.3773   0.01224   0.00704  -0.1325   0.7170   0.6692
  -1.500   0.4028   0.01250   0.00734  -0.1320   0.7154   0.6758
  -1.250   0.4283   0.01266   0.00745  -0.1317   0.7137   0.6813
  -1.000   0.4541   0.01270   0.00751  -0.1314   0.7121   0.6840
  -0.750   0.4809   0.01276   0.00756  -0.1314   0.7105   0.6864
  -0.500   0.5082   0.01278   0.00757  -0.1315   0.7090   0.6888
  -0.250   0.5358   0.01279   0.00754  -0.1317   0.7076   0.6911
   0.000   0.5638   0.01281   0.00751  -0.1320   0.7064   0.6933
   0.250   0.5924   0.01281   0.00747  -0.1324   0.7053   0.6952
   0.500   0.6215   0.01286   0.00745  -0.1330   0.7042   0.6968
   0.750   0.6501   0.01290   0.00747  -0.1335   0.7029   0.6979
   1.000   0.6721   0.01293   0.00755  -0.1326   0.7010   0.6991
   1.250   0.6954   0.01301   0.00766  -0.1320   0.6991   0.7003
   1.500   0.7199   0.01307   0.00775  -0.1317   0.6972   0.7014
   1.750   0.7457   0.01310   0.00778  -0.1316   0.6954   0.7025
   2.000   0.7726   0.01310   0.00780  -0.1317   0.6938   0.7037
   2.250   0.8002   0.01311   0.00780  -0.1319   0.6924   0.7050
   2.500   0.8285   0.01311   0.00779  -0.1323   0.6911   0.7064
   2.750   0.8580   0.01310   0.00777  -0.1329   0.6898   0.7076
   3.000   0.8879   0.01315   0.00781  -0.1336   0.6886   0.7087
   3.250   0.9111   0.01328   0.00798  -0.1331   0.6867   0.7099
   3.500   0.9305   0.01340   0.00816  -0.1317   0.6840   0.7111
   3.750   0.9539   0.01346   0.00825  -0.1312   0.6815   0.7122
   4.000   0.9799   0.01343   0.00825  -0.1311   0.6794   0.7134
   4.250   1.0082   0.01332   0.00816  -0.1314   0.6774   0.7146
   4.500   1.0396   0.01316   0.00802  -0.1323   0.6755   0.7156
   4.750   1.0743   0.01303   0.00787  -0.1338   0.6735   0.7166
   5.000   1.0892   0.01310   0.00805  -0.1315   0.6696   0.7178
   5.250   1.1110   0.01302   0.00803  -0.1305   0.6658   0.7190
   5.500   1.1411   0.01271   0.00774  -0.1310   0.6621   0.7202
   5.750   1.1766   0.01245   0.00744  -0.1326   0.6589   0.7215
   6.000   1.1893   0.01247   0.00757  -0.1298   0.6539   0.7229
   6.250   1.2124   0.01221   0.00735  -0.1289   0.6481   0.7245
   6.500   1.2366   0.01194   0.00707  -0.1281   0.6416   0.7260
   6.750   1.2489   0.01180   0.00697  -0.1250   0.6333   0.7275
   7.000   1.2632   0.01168   0.00687  -0.1223   0.6249   0.7287
   7.250   1.2731   0.01162   0.00688  -0.1188   0.6177   0.7301
   7.500   1.2825   0.01165   0.00697  -0.1153   0.6096   0.7315
   7.750   1.2949   0.01174   0.00709  -0.1124   0.6012   0.7331
   8.000   1.3015   0.01197   0.00739  -0.1085   0.5907   0.7348
   8.250   1.3098   0.01224   0.00770  -0.1051   0.5791   0.7365
   8.500   1.3145   0.01267   0.00812  -0.1013   0.5630   0.7383
   8.750   1.3148   0.01336   0.00876  -0.0971   0.5415   0.7402
   9.000   1.3135   0.01437   0.00970  -0.0931   0.5157   0.7422
   9.250   1.3007   0.01614   0.01129  -0.0880   0.4782   0.7442
   9.500   1.2897   0.01830   0.01327  -0.0840   0.4390   0.7462
   9.750   1.2769   0.02077   0.01555  -0.0801   0.3997   0.7481
  10.000   1.2630   0.02344   0.01800  -0.0765   0.3582   0.7499
  10.250   1.2565   0.02577   0.02018  -0.0737   0.3226   0.7519
  10.500   1.2522   0.02809   0.02234  -0.0714   0.2876   0.7539
  10.750   1.2460   0.03061   0.02464  -0.0691   0.2494   0.7559
  11.000   1.2441   0.03288   0.02673  -0.0672   0.2135   0.7579
  11.250   1.2432   0.03515   0.02881  -0.0655   0.1792   0.7598
  11.500   1.2465   0.03734   0.03085  -0.0645   0.1485   0.7619
  11.750   1.2495   0.03953   0.03289  -0.0634   0.1192   0.7642
  12.000   1.2533   0.04166   0.03488  -0.0624   0.0946   0.7666
  12.250   1.2592   0.04363   0.03678  -0.0616   0.0767   0.7693
  12.500   1.2661   0.04553   0.03864  -0.0608   0.0640   0.7721
  12.750   1.2735   0.04743   0.04051  -0.0601   0.0557   0.7750
  13.000   1.2836   0.04935   0.04244  -0.0600   0.0491   0.7782
  13.250   1.2945   0.05116   0.04432  -0.0599   0.0448   0.7820
  13.500   1.3046   0.05307   0.04629  -0.0597   0.0416   0.7860
  13.750   1.3103   0.05531   0.04854  -0.0592   0.0377   0.7903
  14.000   1.3245   0.05711   0.05047  -0.0597   0.0355   0.7952
  14.250   1.3358   0.05912   0.05255  -0.0600   0.0332   0.8012
  14.500   1.3385   0.06191   0.05540  -0.0597   0.0308   0.8074
  14.750   1.3534   0.06383   0.05745  -0.0605   0.0290   0.8165
  15.000   1.3675   0.06599   0.05975  -0.0615   0.0273   0.8297
  15.250   1.3800   0.06903   0.06291  -0.0634   0.0253   0.8521
  15.500   1.4063   0.07290   0.06706  -0.0689   0.0234   0.9256
  15.750   1.4145   0.07523   0.06945  -0.0684   0.0221   1.0000
  16.000   1.4201   0.07754   0.07180  -0.0681   0.0210   1.0000
  16.250   1.4207   0.08043   0.07472  -0.0677   0.0198   1.0000
  16.500   1.4190   0.08360   0.07796  -0.0672   0.0189   1.0000
  16.750   1.4246   0.08599   0.08045  -0.0671   0.0182   1.0000
  17.000   1.4285   0.08861   0.08315  -0.0670   0.0174   1.0000
  17.250   1.4321   0.09129   0.08590  -0.0669   0.0165   1.0000
  17.500   1.4330   0.09428   0.08893  -0.0670   0.0158   1.0000
  17.750   1.4273   0.09805   0.09276  -0.0668   0.0153   1.0000
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