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Cambered plate C=14% T=5% R=0.96 (cp-140-050-gn) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Cambered plate C=14% T=5% R=0.96 (cp-140-050-gn)
Reynolds number: 1,000,000
Max Cl/Cd: 45 at α=2°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-cp-140-050-gn-1000000-n5.txt
Download as CSV file: xf-cp-140-050-gn-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Cambered plate C=14% T=5% R=0.96                
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000   0.3152   0.10283   0.10013  -0.2222   0.9024   0.0133
 -11.750   0.3235   0.10077   0.09806  -0.2229   0.8990   0.0136
 -11.500   0.3309   0.09767   0.09494  -0.2243   0.8956   0.0142
 -11.250   0.3444   0.09589   0.09313  -0.2261   0.8927   0.0144
 -11.000   0.3582   0.09380   0.09101  -0.2281   0.8897   0.0145
 -10.750   0.3703   0.09230   0.08950  -0.2292   0.8867   0.0148
 -10.500   0.3800   0.09070   0.08790  -0.2297   0.8832   0.0151
 -10.250   0.3903   0.08880   0.08599  -0.2307   0.8798   0.0152
 -10.000   0.4019   0.08687   0.08403  -0.2319   0.8764   0.0157
  -9.500   0.4217   0.08299   0.08012  -0.2337   0.8696   0.0162
  -9.250   0.4265   0.08033   0.07745  -0.2341   0.8656   0.0168
  -9.000   0.4386   0.07905   0.07615  -0.2347   0.8620   0.0169
  -8.750   0.4506   0.07751   0.07457  -0.2356   0.8586   0.0171
  -8.500   0.4629   0.07652   0.07359  -0.2360   0.8554   0.0177
  -8.250   0.4703   0.07486   0.07193  -0.2359   0.8515   0.0177
  -8.000   0.4789   0.07331   0.07037  -0.2360   0.8477   0.0179
  -7.750   0.4879   0.07171   0.06874  -0.2362   0.8438   0.0178
  -7.500   0.4967   0.07020   0.06722  -0.2362   0.8403   0.0186
  -7.250   0.5025   0.06874   0.06576  -0.2355   0.8364   0.0187
  -7.000   0.5020   0.06644   0.06346  -0.2345   0.8316   0.0194
  -6.750   0.5103   0.06545   0.06244  -0.2338   0.8277   0.0195
  -6.500   0.5164   0.06442   0.06142  -0.2326   0.8240   0.0196
  -6.250   0.5208   0.06368   0.06070  -0.2308   0.8201   0.0199
  -6.000   0.5216   0.06286   0.05989  -0.2282   0.8156   0.0201
  -5.750   0.5225   0.06178   0.05879  -0.2261   0.8114   0.0202
  -5.500   0.5255   0.06080   0.05782  -0.2242   0.8075   0.0205
  -5.250   0.5262   0.05977   0.05680  -0.2218   0.8032   0.0207
  -5.000   0.5293   0.05865   0.05568  -0.2200   0.7989   0.0210
  -4.750   0.5347   0.05736   0.05438  -0.2189   0.7948   0.0211
  -4.500   0.5405   0.05603   0.05305  -0.2179   0.7912   0.0213
  -4.250   0.5435   0.05373   0.05075  -0.2176   0.7867   0.0221
  -4.000   0.5504   0.05267   0.04970  -0.2163   0.7826   0.0223
  -3.750   0.5604   0.05194   0.04895  -0.2152   0.7789   0.0225
  -3.500   0.5715   0.05077   0.04778  -0.2148   0.7754   0.0227
  -3.250   0.5829   0.04947   0.04649  -0.2146   0.7717   0.0229
  -3.000   0.5944   0.04821   0.04523  -0.2144   0.7677   0.0232
  -2.750   0.6088   0.04684   0.04383  -0.2147   0.7639   0.0235
  -2.500   0.6266   0.04526   0.04222  -0.2160   0.7604   0.0237
  -2.250   0.6460   0.04361   0.04058  -0.2176   0.7573   0.0241
  -2.000   0.6740   0.04081   0.03774  -0.2222   0.7537   0.0252
  -1.750   0.6921   0.03985   0.03677  -0.2225   0.7501   0.0254
  -1.500   0.7131   0.03881   0.03571  -0.2235   0.7466   0.0257
  -1.250   0.7389   0.03737   0.03424  -0.2259   0.7434   0.0260
  -1.000   0.7660   0.03594   0.03281  -0.2284   0.7404   0.0264
  -0.750   0.7939   0.03443   0.03127  -0.2310   0.7357   0.0267
  -0.500   0.8172   0.03308   0.02984  -0.2325   0.7274   0.0270
  -0.250   0.8615   0.03050   0.02720  -0.2394   0.7220   0.0283
   0.500   0.9380   0.02785   0.02444  -0.2432   0.7028   0.0292
   0.750   0.9653   0.02686   0.02338  -0.2448   0.6950   0.0296
   1.000   0.9899   0.02596   0.02241  -0.2458   0.6816   0.0299
   1.250   1.0168   0.02501   0.02135  -0.2472   0.6664   0.0308
   1.500   1.0534   0.02363   0.01981  -0.2507   0.6515   0.0316
   1.750   1.0601   0.02390   0.01996  -0.2474   0.6275   0.0318
   2.000   1.0742   0.02387   0.01978  -0.2457   0.6011   0.0320
   2.250   1.0727   0.02459   0.02026  -0.2408   0.5589   0.0322
   2.500   1.0693   0.02547   0.02081  -0.2358   0.5005   0.0323
   2.750   1.0365   0.02805   0.02280  -0.2254   0.3868   0.0323
   3.000   1.0079   0.03074   0.02488  -0.2163   0.2515   0.0323
   3.250   0.9881   0.03321   0.02676  -0.2093   0.0793   0.0324
   3.500   1.0087   0.03328   0.02665  -0.2092   0.0280   0.0326
   3.750   1.0364   0.03295   0.02623  -0.2102   0.0235   0.0333
   4.000   1.0698   0.03223   0.02541  -0.2122   0.0223   0.0340
   4.250   1.1102   0.03099   0.02398  -0.2153   0.0214   0.0350
   4.500   1.1314   0.03107   0.02403  -0.2148   0.0206   0.0351
   4.750   1.1527   0.03116   0.02407  -0.2143   0.0200   0.0354
   5.000   1.1740   0.03129   0.02415  -0.2137   0.0194   0.0358
   5.250   1.1968   0.03130   0.02408  -0.2134   0.0190   0.0364
   5.500   1.2284   0.03044   0.02300  -0.2143   0.0185   0.0374
   5.750   1.2614   0.02895   0.02096  -0.2152   0.0183   0.0388
   6.000   1.2780   0.02953   0.02151  -0.2136   0.0181   0.0391
   6.250   1.2942   0.03011   0.02204  -0.2119   0.0179   0.0394
   6.500   1.3105   0.03070   0.02258  -0.2103   0.0178   0.0397
   6.750   1.3266   0.03134   0.02319  -0.2086   0.0176   0.0401
   7.000   1.3419   0.03205   0.02387  -0.2069   0.0175   0.0405
   7.250   1.3562   0.03286   0.02465  -0.2050   0.0172   0.0406
   7.500   1.3706   0.03371   0.02549  -0.2032   0.0172   0.0410
   7.750   1.3858   0.03449   0.02627  -0.2015   0.0169   0.0412
   8.000   1.3997   0.03541   0.02718  -0.1997   0.0166   0.0414
   8.250   1.4127   0.03642   0.02820  -0.1978   0.0166   0.0416
   8.500   1.4256   0.03747   0.02928  -0.1959   0.0165   0.0419
   8.750   1.4388   0.03851   0.03033  -0.1940   0.0163   0.0421
   9.000   1.4502   0.03972   0.03158  -0.1920   0.0162   0.0422
   9.250   1.4620   0.04089   0.03278  -0.1901   0.0162   0.0426
   9.500   1.4742   0.04207   0.03399  -0.1883   0.0161   0.0427
   9.750   1.4851   0.04339   0.03535  -0.1863   0.0159   0.0432
  10.000   1.4957   0.04476   0.03677  -0.1844   0.0159   0.0436
  10.250   1.5063   0.04618   0.03823  -0.1825   0.0158   0.0442
  10.500   1.5163   0.04766   0.03976  -0.1806   0.0157   0.0448
  10.750   1.5259   0.04921   0.04134  -0.1788   0.0156   0.0451
  11.000   1.5365   0.05068   0.04284  -0.1770   0.0154   0.0457
  11.250   1.5446   0.05244   0.04466  -0.1751   0.0154   0.0464
  11.500   1.5537   0.05412   0.04638  -0.1733   0.0153   0.0466
  11.750   1.5619   0.05592   0.04822  -0.1715   0.0151   0.0476
  12.000   1.5691   0.05786   0.05022  -0.1697   0.0151   0.0494
  12.250   1.5765   0.05979   0.05220  -0.1679   0.0150   0.0512
  12.500   1.5820   0.06197   0.05444  -0.1660   0.0148   0.0545
  12.750   1.5854   0.06443   0.05697  -0.1640   0.0146   0.0598
  13.000   1.5964   0.06600   0.05866  -0.1627   0.0146   0.1357
  13.250   1.6077   0.06754   0.06036  -0.1615   0.0145   0.2498
  14.000   1.6456   0.07267   0.06636  -0.1594   0.0142   1.0000
  14.250   1.6551   0.07437   0.06810  -0.1580   0.0142   1.0000
  14.500   1.6642   0.07615   0.06992  -0.1567   0.0141   1.0000
  14.750   1.6734   0.07792   0.07174  -0.1553   0.0140   1.0000
  15.000   1.6830   0.07962   0.07349  -0.1540   0.0139   1.0000
  15.250   1.6930   0.08128   0.07519  -0.1528   0.0137   1.0000
  15.500   1.7031   0.08292   0.07688  -0.1516   0.0136   1.0000
  15.750   1.7129   0.08461   0.07861  -0.1504   0.0135   1.0000
  16.000   1.7228   0.08628   0.08033  -0.1492   0.0134   1.0000
  16.250   1.7329   0.08792   0.08203  -0.1481   0.0133   1.0000
  16.500   1.7434   0.08949   0.08366  -0.1470   0.0132   1.0000
  16.750   1.7536   0.09111   0.08532  -0.1460   0.0131   1.0000
  17.000   1.7637   0.09273   0.08700  -0.1450   0.0130   1.0000
  17.250   1.7734   0.09440   0.08875  -0.1440   0.0129   1.0000
  17.500   1.7824   0.09618   0.09059  -0.1430   0.0128   1.0000
  17.750   1.7911   0.09798   0.09246  -0.1421   0.0127   1.0000
  18.000   1.7998   0.09975   0.09430  -0.1413   0.0126   1.0000
  18.250   1.8078   0.10162   0.09624  -0.1405   0.0125   1.0000
  18.500   1.8146   0.10367   0.09836  -0.1397   0.0124   1.0000
  18.750   1.8203   0.10586   0.10062  -0.1391   0.0123   1.0000
  19.000   1.8263   0.10799   0.10282  -0.1384   0.0122   1.0000
  19.250   1.8314   0.11025   0.10514  -0.1379   0.0121   1.0000
  19.500   1.8360   0.11258   0.10755  -0.1374   0.0121   1.0000
  19.750   1.8408   0.11486   0.10990  -0.1369   0.0120   1.0000
  20.000   1.8450   0.11720   0.11232  -0.1365   0.0119   1.0000
  20.250   1.8485   0.11964   0.11484  -0.1362   0.0119   1.0000
  20.500   1.8521   0.12204   0.11731  -0.1359   0.0118   1.0000
  20.750   1.8546   0.12461   0.11996  -0.1358   0.0118   1.0000
  21.000   1.8565   0.12723   0.12267  -0.1357   0.0117   1.0000
  21.250   1.8581   0.12988   0.12541  -0.1356   0.0116   1.0000
  21.500   1.8573   0.13287   0.12852  -0.1358   0.0115   1.0000
  21.750   1.8527   0.13637   0.13218  -0.1361   0.0114   1.0000
  22.000   1.8507   0.13965   0.13559  -0.1365   0.0114   1.0000
  22.250   1.8481   0.14302   0.13910  -0.1371   0.0113   1.0000
  22.500   1.8438   0.14672   0.14294  -0.1379   0.0113   1.0000
  22.750   1.8389   0.15051   0.14688  -0.1389   0.0113   1.0000
  23.000   1.8315   0.15476   0.15130  -0.1403   0.0112   1.0000
  23.250   1.8217   0.15949   0.15621  -0.1420   0.0111   1.0000
  23.500   1.8079   0.16500   0.16194  -0.1444   0.0110   1.0000
  23.750   1.7842   0.17249   0.16971  -0.1482   0.0109   1.0000
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