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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- Partial requirement for: M.S., Arizona State University, 2010Note typethesis
- Includes bibliographical references (p. 69-70)Note typebibliography
- Field of study: Mechanical engineering