Design And Stress Analysis Of Turbine Blade Of Turbocharger

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@article{1701558,
      author = {Dr. Htay Htay Win, Tin Ni Lar Win},
      title = {Design And Stress Analysis Of Turbine Blade Of Turbocharger},
      journal = {Iconic Research And Engineering Journals},
      year = {2019},
      volume = {3},
      number = {2},
      pages = {481-486},
      issn = {2456-8880},
      url = {https://www.irejournals.com/formatedpaper/1701558.pdf},
      abstract = {The objective of this paper is to to analyze the stress on the turbine blade of turbocharger which is used in automotive diesel engine (118 kW). The turbocharger is failure due to high rotational speed, temperature and pressure. The volume flow rate of this turbine is 0.1 m3/s and the speed is 9500 rpm. The calculation of turbine design consists of pressure, number of blades, blade width, input and output turbine blade angles, mass flow rate, tangential force and radial force on turbine blade. The result comes out turbine inlet and outlet blade angles are 86 degree and 25 degree, the tangential force on turbine is 31N, radial force on turbine is 15N and number of blades is 13 blades. The ANSYS 17.0 software is used for modeling and analysis of the turbine blade of turbocharger. The stress on turbine blade is calculated by theoretically and numerically. The suitable material is Structural Steel. The minimum von-Mises stress and effective strain are found in blade numbers 13},
      keywords = {Turbine, Turbine Blade, Turbocharger, Stress analysis, Rotational Speed},
      month = {August},
  }