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
Collections this item is in
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