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In order to achieve higher gas turbine efficiency, the main gas temperature at turbine inlet has been steadily increased from approximately 900°C to about 1500°C over the last few decades. This temperature is higher than the maximum acceptable temperature for turbine internals.

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    Date Created
    2014
    Resource Type
  • Text
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    Note
    • Partial requirement for: M.S., Arizona State University, 2014
      Note type
      thesis
    • Includes bibliographical references (p. 72-75)
      Note type
      bibliography
    • Field of study: Mechanical engineering

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    by Prashant Singh

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