Date of Award
4-2024
Degree Name
Master of Science in Engineering
Department
Mechanical and Aerospace Engineering
First Advisor
Tianshu Liu, Ph.D.
Second Advisor
William Liou, Ph.D.
Third Advisor
Javier Montefort, Ph.D.
Keywords
Finite base, heat flux, impinging jet, inverse heat transfer, self-similarity, temperature-sensitive paint
Access Setting
Masters Thesis-Open Access
Abstract
This study investigates the consistent features of heat flux patterns on surfaces impacted by jets at various Mach numbers, ranging from 0.1 to 1.0. It utilizes temperature-sensitive paint (TSP) analysis to examine how these patterns change. The research also explores the presence of self-similarity in both the fluctuation of heat flux and skin friction patterns, which are derived from temperature and heat flux data. A semi-empirical model is proposed to explain this self-similarity, suggesting that Mach number primarily affects heat flux patterns through the recovery temperature at the impact site.
Understanding the self-similarity of heat flux patterns across different Mach numbers in oblique jet impacts has significant implications for engineering applications. Additionally, it can contribute to the advancement of industrial processes involving heat transfer, such as the design of heat exchangers or cooling systems for high-speed machinery. Essentially, this study provides valuable insights into the underlying mechanisms governing heat transfer in complex flow configurations, with potential applications across various engineering disciplines.
Recommended Citation
Ragupathy, Thinnesh, "Obliquely Impinging Jet Heat Transfer Fields: Effects of Mach Number on Nozzle-to-Plate Distance" (2024). Masters Theses. 5408.
https://scholarworks.wmich.edu/masters_theses/5408