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A major concern in the operation of present-day gas turbine engines is the ingestion of hot mainstream gas into rotor-stator disk cavities of the high-pressure turbine stages. Although the engines require high gas temperature at turbine entry for good performance

A major concern in the operation of present-day gas turbine engines is the ingestion of hot mainstream gas into rotor-stator disk cavities of the high-pressure turbine stages. Although the engines require high gas temperature at turbine entry for good performance efficiency, the ingested gas shortens the lives of the cavity internals, particularly that of the rotor disks.

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    Date Created
    2010
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  • Text
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    Note
    • Partial requirement for: M.S., Arizona State University, 2010
      Note type
      thesis
    • Includes bibliographical references (p. 60-61)
      Note type
      bibliography
    • Field of study: Mechanical engineering

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    by Nihal Junnarkar

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