Description
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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Contributors
- Singh, Prashant (Author)
- Roy, Ramendra P (Thesis advisor)
- Mignolet, Marc (Thesis advisor)
- Lee, Taewoo (Committee member)
- Arizona State University (Publisher)
Date Created
The date the item was original created (prior to any relationship with the ASU Digital Repositories.)
2014
Resource Type
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Note
- Partial requirement for: M.S., Arizona State University, 2014Note typethesis
- Includes bibliographical references (p. 72-75)Note typebibliography
- Field of study: Mechanical engineering
Citation and reuse
Statement of Responsibility
by Prashant Singh