Towards Fully-Resolved Particulate-Induced Transition Simulations for High-Speed Boundary-Layers with an Immersed Boundary Method
Speaker: Oliver M. F. Browne, University of Kentucky
Presentation
Seminar Slide Deck (PDF-42.5MB)
Abstract
This talk will present a numerical approach to model particulate-induced transition in the upper atmosphere (stratosphere) relevant for high-speed (high supersonic/hypersonic) vehicles. Various types of particulates with different origins and a wide range of properties are present in the stratosphere and could provide the threshold disturbance energy to cause boundary-layer transition. Atmospheric particulates impinging on the surface of high-speed vehicles trigger a wavepacket inside the boundary layer which, based on the flow and particle conditions, can grow substantially and provide a path to turbulence.
In the first part of this presentation, our newly developed wavepacket tracking strategy coupled with a particle model will be presented. The wavepacket tracking approach, namely AMR-WPT (adaptive mesh refinement wavepacket tracking), relies on (1) the nonlinear disturbance flow formulation of the compressible Navier-Stokes equations, (2) a dual mesh overset approach, and (3) adaptive mesh refinement (AMR). The AMR-WPT approach has been demonstrated to result in significant computational savings when compared to conventional approaches for transition prediction. To model particulate-induced transition, AMR-WPT was initially coupled with a particle solver based on the particle-in-cell (PIC) approach. The second part of this talk will present a higher-fidelity approach by modeling the particle with a higher-order Immersed Boundary Method (IBM) and coupling it with the AMR-WPT method. Both methods will be validated for typical hypersonic transition prediction test cases.
Biography