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Rhode St. Genese 30 (rhodesg30-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 30 (rhodesg30-il)
Reynolds number: 50,000
Max Cl/Cd: 36.27 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg30-il-50000-n5.txt
Download as CSV file: xf-rhodesg30-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Rhode St. Genese 30                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.4033   0.09576   0.08880  -0.0346   1.0000   0.0405
 -10.500  -0.4043   0.09215   0.08527  -0.0357   1.0000   0.0408
 -10.250  -0.4073   0.08843   0.08165  -0.0369   1.0000   0.0412
 -10.000  -0.4129   0.08466   0.07799  -0.0381   1.0000   0.0414
  -9.750  -0.4218   0.08097   0.07443  -0.0391   1.0000   0.0416
  -9.500  -0.4316   0.07704   0.07063  -0.0404   1.0000   0.0419
  -9.250  -0.4401   0.07274   0.06641  -0.0421   1.0000   0.0421
  -9.000  -0.4485   0.06824   0.06197  -0.0434   1.0000   0.0424
  -8.750  -0.4565   0.06362   0.05734  -0.0443   1.0000   0.0431
  -8.500  -0.4647   0.05849   0.05212  -0.0449   1.0000   0.0441
  -8.250  -0.4743   0.05204   0.04538  -0.0456   1.0000   0.0457
  -8.000  -0.4737   0.04788   0.04093  -0.0451   1.0000   0.0487
  -7.750  -0.4670   0.04505   0.03778  -0.0441   1.0000   0.0538
  -7.500  -0.4595   0.04133   0.03349  -0.0434   1.0000   0.0591
  -7.250  -0.4457   0.04112   0.03327  -0.0419   1.0000   0.0660
  -7.000  -0.4323   0.03836   0.02989  -0.0409   1.0000   0.0696
  -6.750  -0.4162   0.03629   0.02722  -0.0399   1.0000   0.0712
  -6.500  -0.3999   0.03525   0.02609  -0.0387   1.0000   0.0733
  -6.250  -0.3837   0.03523   0.02611  -0.0374   1.0000   0.0792
  -6.000  -0.3657   0.03423   0.02467  -0.0364   1.0000   0.0833
  -5.750  -0.3469   0.03321   0.02322  -0.0355   1.0000   0.0848
  -5.500  -0.3269   0.03248   0.02242  -0.0349   0.9992   0.0866
  -5.250  -0.2936   0.03242   0.02233  -0.0369   0.9924   0.0933
  -5.000  -0.2588   0.03183   0.02134  -0.0391   0.9858   0.0996
  -4.750  -0.2267   0.03144   0.02095  -0.0408   0.9785   0.1043
  -4.500  -0.1927   0.03061   0.01983  -0.0424   0.9719   0.1047
  -4.250  -0.1570   0.02978   0.01872  -0.0442   0.9648   0.1045
  -4.000  -0.1220   0.02902   0.01771  -0.0458   0.9560   0.1047
  -3.750  -0.0816   0.02829   0.01677  -0.0483   0.9463   0.1054
  -3.500  -0.0365   0.02750   0.01577  -0.0514   0.9349   0.1063
  -3.250   0.0081   0.02670   0.01480  -0.0541   0.9209   0.1071
  -3.000   0.0532   0.02594   0.01389  -0.0567   0.9067   0.1079
  -2.750   0.0947   0.02528   0.01308  -0.0587   0.8936   0.1091
  -2.500   0.1322   0.02476   0.01244  -0.0601   0.8822   0.1108
  -2.250   0.1694   0.02425   0.01186  -0.0615   0.8721   0.1132
  -2.000   0.2029   0.02381   0.01142  -0.0622   0.8606   0.1168
  -1.750   0.2335   0.02344   0.01104  -0.0624   0.8474   0.1219
  -1.500   0.2638   0.02306   0.01069  -0.0625   0.8338   0.1314
  -1.250   0.2937   0.02262   0.01036  -0.0625   0.8198   0.1540
  -1.000   0.3536   0.01957   0.01009  -0.0679   0.8085   1.0000
  -0.750   0.3813   0.01955   0.00980  -0.0673   0.7919   1.0000
  -0.500   0.4090   0.01950   0.00956  -0.0666   0.7744   1.0000
  -0.250   0.4370   0.01945   0.00934  -0.0659   0.7564   1.0000
   0.000   0.4637   0.01942   0.00915  -0.0651   0.7366   1.0000
   0.250   0.4893   0.01943   0.00903  -0.0641   0.7147   1.0000
   0.750   0.5427   0.01950   0.00882  -0.0624   0.6687   1.0000
   1.000   0.5695   0.01959   0.00876  -0.0617   0.6457   1.0000
   1.250   0.5948   0.01979   0.00884  -0.0608   0.6215   1.0000
   1.500   0.6204   0.02002   0.00892  -0.0600   0.5993   1.0000
   1.750   0.6450   0.02034   0.00915  -0.0592   0.5779   1.0000
   2.000   0.6700   0.02069   0.00938  -0.0586   0.5595   1.0000
   2.250   0.6951   0.02108   0.00969  -0.0580   0.5436   1.0000
   2.500   0.7202   0.02151   0.01009  -0.0575   0.5299   1.0000
   2.750   0.7455   0.02197   0.01053  -0.0571   0.5179   1.0000
   3.000   0.7713   0.02242   0.01096  -0.0567   0.5075   1.0000
   3.250   0.7968   0.02292   0.01150  -0.0564   0.4976   1.0000
   3.500   0.8219   0.02346   0.01211  -0.0560   0.4886   1.0000
   3.750   0.8484   0.02399   0.01268  -0.0558   0.4815   1.0000
   4.000   0.8731   0.02463   0.01347  -0.0556   0.4742   1.0000
   4.250   0.8990   0.02522   0.01416  -0.0553   0.4673   1.0000
   4.500   0.9229   0.02588   0.01497  -0.0549   0.4595   1.0000
   4.750   0.9482   0.02645   0.01564  -0.0544   0.4510   1.0000
   5.000   0.9697   0.02709   0.01644  -0.0535   0.4397   1.0000
   5.250   0.9904   0.02754   0.01694  -0.0523   0.4241   1.0000
   5.500   1.0103   0.02786   0.01724  -0.0507   0.4051   1.0000
   5.750   1.0269   0.02831   0.01779  -0.0489   0.3858   1.0000
   6.000   1.0446   0.02883   0.01843  -0.0473   0.3696   1.0000
   6.250   1.0629   0.02937   0.01913  -0.0459   0.3553   1.0000
   6.500   1.0764   0.02990   0.01983  -0.0438   0.3363   1.0000
   6.750   1.0883   0.03041   0.02051  -0.0415   0.3161   1.0000
   7.000   1.1002   0.03098   0.02128  -0.0392   0.2968   1.0000
   7.250   1.1074   0.03167   0.02226  -0.0366   0.2699   1.0000
   7.500   1.1139   0.03247   0.02333  -0.0339   0.2346   1.0000
   7.750   1.1141   0.03353   0.02417  -0.0306   0.1832   1.0000
   8.000   1.1064   0.03544   0.02561  -0.0268   0.1528   1.0000
   8.250   1.1011   0.03780   0.02781  -0.0240   0.1329   1.0000
   8.500   1.0962   0.04034   0.03029  -0.0216   0.1200   1.0000
   8.750   1.0916   0.04299   0.03294  -0.0197   0.1102   1.0000
   9.000   1.0899   0.04555   0.03562  -0.0182   0.1015   1.0000
   9.250   1.0858   0.04839   0.03848  -0.0171   0.0950   1.0000
   9.500   1.0867   0.05100   0.04124  -0.0161   0.0896   1.0000
   9.750   1.0873   0.05370   0.04406  -0.0153   0.0852   1.0000
  10.000   1.0868   0.05656   0.04693  -0.0148   0.0813   1.0000
  10.250   1.0883   0.05940   0.04999  -0.0144   0.0762   1.0000
  10.500   1.0881   0.06240   0.05303  -0.0142   0.0722   1.0000
  10.750   1.0910   0.06522   0.05593  -0.0138   0.0687   1.0000
  11.000   1.0932   0.06831   0.05924  -0.0136   0.0648   1.0000
  11.250   1.0948   0.07135   0.06235  -0.0136   0.0611   1.0000
  11.500   1.1029   0.07398   0.06501  -0.0127   0.0577   1.0000
  11.750   1.1008   0.07807   0.06945  -0.0132   0.0553   1.0000
  12.000   1.0966   0.08247   0.07413  -0.0140   0.0531   1.0000
  12.250   1.0905   0.08715   0.07902  -0.0153   0.0511   1.0000
  12.500   1.0848   0.09196   0.08403  -0.0167   0.0496   1.0000
  12.750   1.0784   0.09699   0.08923  -0.0183   0.0484   1.0000
  13.000   1.0764   0.10147   0.09378  -0.0193   0.0467   1.0000
  13.250   1.0659   0.10761   0.10004  -0.0216   0.0459   1.0000
  13.500   1.0481   0.11513   0.10777  -0.0258   0.0459   1.0000
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