Code-Verification Techniques for Hypersonic Reacting Flow in Thermochemical Nonequilibrium
Author(s) -
Brian Freno,
Brian Carnes,
V. Gregory Weirs
Publication year - 2019
Publication title -
aiaa aviation 2019 forum
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2019-3705
Subject(s) - non equilibrium thermodynamics , code (set theory) , computer science , hypersonic flow , nuclear engineering , hypersonic speed , flow (mathematics) , aerospace engineering , mechanics , thermodynamics , programming language , physics , engineering , set (abstract data type)
The study of hypersonic flows and their underlying aerothermochemical reactions is particularly important in the design and analysis of vehicles exiting and reentering Earth’s atmosphere. Computational physics codes can be employed to simulate these phenomena; however, code verification of these codes is necessary to certify their credibility. To date, few approaches have been presented for verifying codes that simulate hypersonic flows, especially flows reacting in thermochemical nonequilibrium. In this paper, we present our code-verification techniques for verifying the spatial accuracy and thermochemical source term in hypersonic reacting flows in thermochemical nonequilibrium. We demonstrate the effectiveness of these techniques on the Sandia Parallel Aerodynamics and Reentry Code (SPARC).
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