Description
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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Contributors
- Balasubramanian, Jagdish Harihara (Author)
- Roy, Ramendra P (Thesis advisor)
- Lee, Taewoo (Committee member)
- Phelan, Patrick (Committee member)
- Arizona State University (Publisher)
Date Created
The date the item was original created (prior to any relationship with the ASU Digital Repositories.)
2010
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Note
- Partial requirement for: M.S., Arizona State University, 2010Note typethesis
- Includes bibliographical references (p. 69-70)Note typebibliography
- Field of study: Mechanical engineering
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Jagdish Harihara Balasubramanian