Unsteady Simulation on Aerodynamics Performance of Endwall Film Cooling under the influence of Upstream leakage Injection

Focus should be mainly on Introduction , Problem statement and Research methodology

The purpose of project is

To investigate the effect of the turbine cooling system by taking advantage of the upstream leakage which is bypassed from the
compressor side. In this study, the investigation will be conducted by numerical simulation by using comersial software, ANSYS CFX and the unsteady simulation URANS will be applied. Thus the unsteadiness of the flow structure near the endwall region can be seen

References should be above the year 2012

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