Large eddy simulation of high pressure turbine cascade

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Abstract/Contents

Abstract
In gas turbine engine design, better efficiency is achieved through higher turbine inlet temperature. As a result, the nozzle guide vanes and rotor blades of a High Pressure Turbine (HPT) are subject to an increasingly hostile thermal environment. High levels of turbulence and hot streaks from the upstream combustor impinge on the HPT blade rows. Heat transfer prediction of the thermally critical regions of a HPT is a vital element in the design of gas turbine engines. The effect of inlet turbulence on heat transfer and boundary layer development on a HPT vane cascade has been studied numerically using a high-order overset Large Eddy Simulation procedure. Numerical visualizations of instantaneous boundary layer flow show presence of long, meandering, streamwise oriented streaky structures on both the suction and pressure sides of the blade. Stretching of vortices from the inlet turbulence around the leading edge and subsequent transport of them into the blade passage produces these boundary layer streaks. Significant enhancement in laminar heat transfer, especially around the leading edge and on the pressure side is observed due to these structures. Backward jets are created in the fluctuation velocity field in the boundary layer, which interact with eddies in the turbine passage leading to bypass transition of the suction surface boundary layer. Simulations with organized spanwise disturbance show sensitivity of leading edge region heat transfer to the intensity and length scale of the inlet disturbance.

Description

Type of resource text
Form electronic; electronic resource; remote
Extent 1 online resource.
Publication date 2010
Issuance monographic
Language English

Creators/Contributors

Associated with Bhaskaran, Rathakrishnan
Associated with Stanford University, Department of Mechanical Engineering
Primary advisor Lele, Sanjiva K. (Sanjiva Keshava), 1958-
Thesis advisor Lele, Sanjiva K. (Sanjiva Keshava), 1958-
Thesis advisor Eaton, John K
Thesis advisor Moin, Parviz
Advisor Eaton, John K
Advisor Moin, Parviz

Subjects

Genre Theses

Bibliographic information

Statement of responsibility Rathakrishnan Bhaskaran.
Note Submitted to the Department of Mechanical Engineering.
Thesis Thesis (Ph. D.)--Stanford University, 2010.
Location electronic resource

Access conditions

Copyright
© 2010 by Rathakrishnan Bhaskaran

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