Researchers at the Department of Aerospace Engineering at The Grainger College of Engineering are using high-fidelity 3D simulations to study flow behaviors around cone-shaped bodies at hypersonic speeds.
The simulations conducted on Frontera supercomputer revealed previously unobserved 3D flow patterns and disruptions near the cone's tip at Mach 16 speeds.
Increasing Mach numbers intensify shock wave activity, leading to flow instabilities that impact hypersonic vehicle design.
Transitioning flows at hypersonic speeds are complex and inherently three-dimensional, challenging traditional understanding of flow dynamics.
Efficient use of in-house software capable of parallel processing accelerated computational processes and unveiled unprecedented insights into flow disruptions.
The research explores the relationship between flow behavior, surface characteristics, and speed variation to enhance future hypersonic vehicle designs.
Utilizing DSMC techniques enabled accurate tracking of individual air molecules, offering a stochastic perspective on gas behavior in the flow field.
Advanced computational methods and simulations provide essential insights for improving hypersonic vehicle performance and safety.
The research contributes to a deeper understanding of fluid mechanics essential for transforming hypersonic vehicle design and functionality.
Published in Physical Review Fluids, the study titled 'Loss of axial symmetry in hypersonic flows over conical shapes' demonstrates the significance of advancing aerospace engineering through cutting-edge research.