Thermal non-equilibrium nonlinear coupled constitutive relations for hypersonic rarefied diatomic gas flows

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Shuhua Zeng , Junyuan Yang , Wenwen Zhao , Jiaqi An , Wanshu Li , Weifang Chen
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引用次数: 0

Abstract

The generalized hydrodynamic theory and its derived nonlinear coupled constitutive relations (NCCR) model have proven effective in simulating a range of typical hypersonic rarefied non-equilibrium flows, particularly in regimes where traditional Navier-Stokes (NS) equations are inadequate. However, the treatment of bulk viscosity has been limited, serving primarily as an approximation for rotational non-equilibrium effects, and lacking an explicit framework for energy exchange between different modes within the NCCR model. To address this limitation, this study introduces a thermal non-equilibrium NCCR model that operates without bulk viscosity, incorporating the Landau-Teller-Jeans relaxation model to facilitate explicit energy exchange between translational and rotational modes. The model's accuracy has been rigorously validated through a series of classical numerical cases, including analyzing nitrogen shock structures, supersonic flow over a flat plate, and hypersonic flows past blunt and flat-headed cylinders. The results demonstrate a significant improvement in alignment with experimental data and direct simulation Monte Carlo (DSMC) solutions compared to those derived from the NS equations and the original NCCR model lacking bulk viscosity. Furthermore, the proposed model enhances the predictive capability over the original NCCR framework and elucidates the mechanisms of non-equilibrium energy exchange between modes. These findings underscore the potential of the thermal non-equilibrium NCCR model as a robust and accurate tool for the simulation of hypersonic rarefied diatomic gas flows.
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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