Hypersonic Vehicle Analyses: The Needs and Challenges of Multidisciplinary Simulations - presented by Prof. Iain Boyd

Hypersonic Vehicle Analyses: The Needs and Challenges of Multidisciplinary Simulations

Prof. Iain Boyd

Prof. Iain Boyd
Slide at 15:06
CENTER FOR
NATIONAL
Modeling Of
SECURITY INITIATIVES
Hypersonic Gas Flow
LeMANS:
T[K]
3D Navier-Stokes Equations
5500
4500 3500
2500
Nonequilibrium thermochemistry
1500 500
Internal energy equation(s)
- Species continuity equations
Weakly ionized plasma
Point/line implicit, parallelized
Coupled via surface chemistry
to material response
Benchmarked against other codes
Validated using laboratory and
flight measurements
University of Colorado
Boulder
Be Boulder.
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Summary (AI generated)

To build models of hypersonic vehicles and understand the coupling between systems, the first step is modeling the hypersonic flow. This is essential as it forms the basis for everything else, such as special materials and structures. In our work, we use a hypersonic flow code called LeMANS, which solves the three-dimensional Navier-Stokes equations and includes nonequilibrium thermochemistry, vibrational energy relaxation, chemical reactions, and plasma considerations. The code is efficient on high-performance computing systems and is coupled with surface chemistry for material response.

LeMANS has been benchmarked and validated against other similar codes using laboratory and flight data, providing a solid foundation for our analysis. This chart illustrates the range of activities involved in developing a reliable hypersonic code for analysis and design.