collaborators

10 papers

physics.plasm-ph2026

Simulation Study of Coupling Effects Between a Hall Thruster and a Power Processing Unit

Zirui Fan, Yinjian Zhao, Jingjing Li +4

The complex and nonlinear load characteristics of Hall thrusters remain a key challenge in the design of propulsion power-supply output stages. In existing power-supply simu-lation…

physics.plasm-ph2026

Semi-local Floquet theory for active azimuthal magnetic modulation of Hall-thruster high-frequency instabilities

Yinjian Zhao, Changzheng Hu

A semi-local Floquet extension of a uniform-field kinetic electron drift instability (EDI) dispersion relation is developed to assess prescribed azimuthal magnetic-field modulation…

physics.plasm-ph2026

Test Particle Study of EDI Driven Electron Transport in a Hall Thruster Using PIC Derived Electric Fields

Zhongping Zhao, Kunpeng Zhong, Yinjian Zhao

Electron transport in a Hall thruster is investigated at the test particle level using prescribed electric fields derived from the electron drift instability (EDI) resolving three…

physics.plasm-ph2026

Free-Molecular Face-Flux Preprocessing for Reduced Neutral-Continuity Modeling in Hall Thrusters: Particle-Based Reference and Deterministic SN-DFEM Realization

Yingjie Chen, Xi Chen, Yinjian Zhao

Neutral gas transport directly affects the ionization source, propellant utilization, and low-frequency discharge oscillations in Hall thrusters. High-fidelity particle-based neutr…

physics.plasm-ph2026

Conservative Charge and Current Deposition on Nonuniform 3D Cylindrical PIC Meshes with Residual Self-Field Diagnostics

Zhe Liu, Zhijun Zhou, Yinjian Zhao

Particle-in-cell simulations on nonuniform cylindrical meshes require deposition schemes that respect cylindrical metrics while controlling numerical self-fields. This work develop…

physics.plasm-ph2026

Full-gap kinetic limitation of thermionic-electron transport for electron transpiration cooling

Wushun Zhang, Weixing Zhou, Yinjian Zhao

Electron transpiration cooling (ETC) can reduce aerothermal loads on sharp hypersonic leading edges, but its performance is governed by whether thermionically emitted electrons esc…