Computational Modelling of Hypersonic Nozzle Flows in Thermochemical Non-equilibrium

Join us for an insightful seminar presented by Odelma Teixeira, a Ph.D. candidate in Mechanical Engineering at the University of Beira Interior and a researcher at C-MAST - Center for Mechanical and Aerospace Science and Technology. Recorded on May 22nd, 2024, this presentation delves into the fascinating world of hypersonic nozzle flows and their significance in aerospace engineering.
About the Presenter:
Odelma Teixeira is a dedicated Ph.D. candidate in Mechanical Engineering and an active researcher at C-MAST. With a strong foundation in Aerospace Engineering, her research focuses on fluid dynamics, thermochemical, and electromagnetic phenomena in hypersonic flows.
Abstract:
In this seminar, Odelma explores the computational modelling techniques used to study hypersonic nozzle flows in thermochemical non-equilibrium. She highlights the importance of understanding these complex flows for aerospace applications, especially for re-entry vehicles in space missions. Due to the high costs and practical challenges of space experiments, computational modelling serves as a crucial tool for investigating these phenomena. Odelma discusses how hypersonic wind tunnels, represented computationally by convergent-divergent nozzles, simulate the conditions experienced by re-entry vehicles.
Key Highlights:
Detailed exploration of hypersonic nozzle flows
Importance of computational simulations in aerospace research
Role of hypersonic wind tunnels in replicating re-entry conditions
Insights into thermochemical and electromagnetic phenomena in hypersonic flows
Event Details:
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