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Efficient performance of gas turbines depends, among several parameters, on the mainstream gas entry temperature. At the same time, transport of this high temperature gas into the rotor-stator cavities of turbine stages affects the durability of rotor disks.

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    Date Created
    2010
    Resource Type
  • Text
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    Note
    • Partial requirement for: M.S., Arizona State University, 2010
      Note type
      thesis
    • Includes bibliographical references (p. 69-70)
      Note type
      bibliography
    • Field of study: Mechanical engineering

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    Jagdish Harihara Balasubramanian

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