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Modeling Particle-Laden Compressible Flows with Application to Plume-Surface Interactions

Speaker: Jesse Capecelatro, University of Michigan

Presentation

Seminar Slide Deck (PDF-39MB)

Abstract

The interactions between rocket exhaust plumes and the surface of extraterrestrial bodies during spacecraft landings involve complex multiphase flow dynamics that pose significant risk to space exploration missions. The two-phase flow associated with plume-surface interactions (PSI) is characterized by high Reynolds number transonic conditions with particle concentrations ranging from dilute to close-packing. In this talk, an Eulerian-Lagrangian framework for simulating gas-solid compressible flows under conditions relevant to PSI is presented. Simulations of underexpanded jets impinging on granular beds are performed to investigate the role of nozzle pressure ratio on crater morphology and particle ejecta.

Biography

Photo of Jesse Capecelatro
Jesse Capecelatro is an Assistant Professor in the Departments of Mechanical Engineering and Aerospace Engineering at the University of Michigan. His research group develops numerical methods and data-driven models for turbulent multiphase flows. Prior to joining Michigan in 2016, Capecelatro was a research scientist at the Center for Exascale Simulation of Plasma-Coupled Combustion (XPACC) at the University of Illinois. He received his B.S. from SUNY Binghamton in 2009, his M.S. from the University of Colorado Boulder in 2011, and his Ph.D. from Cornell in 2014.