Numerical Investigations on the Aerodynamic Performance of Turbine Stage with Nonaxisymmetric End Wall Profiling[J]. 2013, 47(7): 29-35.
DOI:
Numerical Investigations on the Aerodynamic Performance of Turbine Stage with Nonaxisymmetric End Wall Profiling[J]. 2013, 47(7): 29-35.DOI: 10.7652/xjtuxb201307006.
Numerical Investigations on the Aerodynamic Performance of Turbine Stage with Nonaxisymmetric End Wall Profiling
Nonaxisymmetric end wall profiling of a high loaded and low aspect ratio turbine stage was designed by the two control curves method. The characteristics of the initial axisymmetric end wall profiling turbine stage and the nonaxisymmetric end wall profiling turbine stage with high load and low aspect ratio were numerically investigated using the Reynolds-averaged Navier-Stokes(RANS)and the SST turbulent model with transition effects. The numerical results for the axisymmetric turbine stage and the nonaxisymmetric turbine stage were compared and analyzed. The results show that the nonaxisymmetric end wall reduces the circumferential pressure gradient and the secondary loss
and the efficiency of the end wall profiling stage increases by 0.16%
compared with that of the axisymmetric end wall stage. In addition
the inlet condition of the rotor changes due to the change in the stator flow field
resulting in the increase in the rotor inlet pressure and the reaction degree.
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references
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