The state of the boundary layer on hypersonic vehicles has a large impact on heat transfer. Modeling boundary layer transition from laminar to turbulent flow is therefore critical for reducing design uncertainty. However, truly predictive models for transition do not yet exist. Increased physical understanding, as well as new computational tools, are required to bridge that gap. In this project, students will use computational tools (CFD and in-house stability models) to examine novel flow configurations and the impact of various parameters on boundary-layer transition at hypersonic speeds.
Name of research group, project, or lab
High-Speed Aerodynamics and Boundary Layer Transition Lab
Hypersonics is a critical research area with far-reaching applications from human spaceflight to national security. Our lab aims to advance engineering capabilities to reduce the costs and risks associated with hypersonic vehicle design.
2 sp. | 0 appl.
Hours per week
1 credit / 3-6 hours
Project categories
Aerospace and Mechanical Engineering
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