Dynamic Behaviour Analysis of Turbocharger Rotor-Shaft System in Thermal Environment Based on Finite Element Method

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left" colspan="2">Turbine side</td><td class="align_center" colspan="2">Compressor side</td></tr><tr class="thead"><td class="align_left" colspan="2">Medium (intensity = 5%)</td><td class="align_center" colspan="2">Medium (intensity = 5%)</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">Inlet mass flow</td><td class="align_center">0.074 kg/s</td><td class="align_center">Inlet total pressure</td><td class="align_center">99935.9 Pa</td></tr><tr><td class="align_left">Inlet total temperature</td><td class="align_center">872.97 K</td><td class="align_center">Inlet total temperature</td><td class="align_center">297.201 K</td></tr><tr><td class="align_left">Outlet static pressure</td><td class="align_center">96892.7 Pa</td><td class="align_center">Outlet static pressure</td><td class="align_center">127578 Pa</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>The boundary conditions for aerothermal analysis.</div>

Shock and Vibration

tab2

Table 2

Table 2: Dynamic Behaviour Analysis of Turbocharger Rotor-Shaft System in Thermal Environment Based on Finite Element Method 