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Research Article | Publishing Language: Chinese | Open Access

Numerical simulation of hypersonic magnetofluid control based on non-linear coupling constitutive relation

Hao Shi1Hong Xiao1( )Li Zhou1,2Zhanxue Wang1
School of Power and Energy, Northwestern Polytechnical University, Xi'an 710129, China
Collaborative Innovation Center for Advanced Aero-Engine, Beijing 100191, China
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Abstract

To address the complex nonlinear flow mechanisms of high-speed plasma in magnetic fields, the conventional‌ Navier-Stokes (N-S) equations based on continuum theory fail to provide accurate predictions. Therefore, a novel framework was developed by‌ coupling the nonlinear coupling constitutive relations (NCCR) with Maxwell's electromagnetic field governing equations, augmented with the Park's TTv two-temperature model and the Park 11-component chemical reaction model. This integration established‌ a numerical simulation method and code for hypersonic magnetohydrodynamic (MHD) thermochemical non-equilibrium under‌ low magnetic Reynolds numbers conditions‌. Numerical simulations of high-speed plasma flow past a spherical body were conducted to investigate the influence mechanism of a dipole magnetic field on high-speed MHD control, with particular focus on‌ the effects of magnetic field existence‌ and its induction strength on plasma flow field structures. The results show that the presence of a magnetic field significantly alters high-speed plasma flow structures, with stronger magnetic fields inducing greater Lorentz forces on charged particles and consequently increasing bow shock detachment distances (e.g., a 452.38% increment observed at B0 = 3.0 T). Stagnation point heat flux variations exhibit dependence on multiple factors including magnetic induction strength, inflow altitude, and Mach number, showing a notable 45.55% reduction at H = 80 km after magnetic field introduction. Furthermore, the magnetic field induces prominent thermochemical non-equilibrium effects, primarily enhancing N2 dissociation in post-shock regions while modifying recombination reactions near walls, yet exerting minimal influence on O2 dissociation dynamics.

CLC number: V231;V411.4;O361.3 Document code: A Article ID: 0258-1825(2026)02-0068-13

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Acta Aerodynamica Sinica
Pages 68-80

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Cite this article:
Shi H, Xiao H, Zhou L, et al. Numerical simulation of hypersonic magnetofluid control based on non-linear coupling constitutive relation. Acta Aerodynamica Sinica, 2026, 44(2): 68-80. https://doi.org/10.7638/kqdlxxb-2024.0160

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Received: 22 October 2024
Revised: 10 February 2025
Published: 22 May 2025
© The journal of Acta Aerodynamica Sinica.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).