Date of Graduation
5-2026
Document Type
Thesis
Degree Name
Bachelor of Science in Mechanical Engineering
Degree Level
Undergraduate
Department
Mechanical Engineering
Advisor/Mentor
Dr. Keith Walters
Committee Member
Dr. Jim Leylek
Abstract
In modern gas turbine design, film cooling has become ubiquitous as a method for limiting heat transfer between high temperature gases post-combustion and the surface of downstream blades. This paper validates the use of various computational fluid dynamics techniques in recreating an experiment measuring adiabatic effectiveness over a surface downstream of a compound-angle N2 plenum jet incident on a turbulent-air boundary layer [1]. To do this, both RANS and Dynamic Hybrid RANS-LES (DHRL) methods are implemented and compared to previous research [2]. The latter method is then modified through implementation of a different subgrid scale (SGS) model and through addition of a statistically targeted synthetic turbulence forcing function upstream of the plenum inlet. Results are obtained for DHRL using the new SGS and forcing function and compared to experiment. It is found that at a high nitrogen-air blowing ratio, the addition of upstream synthetic turbulence has a negligible effect on adiabatic effectiveness, especially when compared to SGS model alteration. When at a lower blowing ratio, the comparative effect is more nuanced, with turbulence generation improving DHRL results by a noticeable amount compared to experiment.
Keywords
Film cooling; CFD; Hybrid RANS-LES; Subgrid Scale Model
Citation
McCallum, C. W. (2026). Turbulent Plenum Jet-Crossflow Validation Via Subgrid Scale Model Variation And Upstream Forcing Under Dynamic Hybrid RANS-LES. Mechanical Engineering Undergraduate Honors Theses Retrieved from https://scholarworks.uark.edu/meeguht/152
Included in
Aerodynamics and Fluid Mechanics Commons, Computational Engineering Commons, Fluid Dynamics Commons