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Improving Turbine Performance: A Contribution to the Understanding of Heat Transfer and Vortical Structures in Staggered Pin Fin Arrays
- Date Issued:
- 2019
- Abstract/Description:
- Through the comparison of flow structures, velocity contours, turbulence statistics, and additional flow quantities, the error sources of RANS are qualitatively described. The findings in this work will help gas turbine design engineers to tweak their turbulence models and give guidance on the interpretation of their results. The novelty is the application of the transient TLC method on this type of geometry as well as the near-wall PIV measurements. The advancements in additive manufacturing disrupt the classic turbine cooling development for casted airfoils. More and more complicated shapes and cooling schemes are possible. Nonetheless, a detailed physical understanding of fundamental cases - as provided in this study - is required for physics-based optimization of cooling designs.
Title: | Improving Turbine Performance: A Contribution to the Understanding of Heat Transfer and Vortical Structures in Staggered Pin Fin Arrays. |
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Name(s): |
Otto, Marcel, Author Kapat, Jayanta, Committee Chair Ahmed, Kareem, Committee Member Bhattacharya, Samik, Committee Member Kinzel, Michael, Committee Member Wiegand, Rudolf, Committee Member University of Central Florida, Degree Grantor |
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Type of Resource: | text | |
Date Issued: | 2019 | |
Publisher: | University of Central Florida | |
Language(s): | English | |
Abstract/Description: | Through the comparison of flow structures, velocity contours, turbulence statistics, and additional flow quantities, the error sources of RANS are qualitatively described. The findings in this work will help gas turbine design engineers to tweak their turbulence models and give guidance on the interpretation of their results. The novelty is the application of the transient TLC method on this type of geometry as well as the near-wall PIV measurements. The advancements in additive manufacturing disrupt the classic turbine cooling development for casted airfoils. More and more complicated shapes and cooling schemes are possible. Nonetheless, a detailed physical understanding of fundamental cases - as provided in this study - is required for physics-based optimization of cooling designs. | |
Identifier: | CFE0007848 (IID), ucf:52803 (fedora) | |
Note(s): |
2019-12-01 Ph.D. Engineering and Computer Science, Mechanical and Aerospace Engineering Doctoral This record was generated from author submitted information. |
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Subject(s): | Heat Transfer -- Gas Turbine -- Turbulence -- Pin Fin -- Wake Shedding | |
Persistent Link to This Record: | http://purl.flvc.org/ucf/fd/CFE0007848 | |
Restrictions on Access: | public 2019-12-15 | |
Host Institution: | UCF |