基于高温气体效应的磁流体流动控制研究进展
罗凯， 汪球， 李逸翔， 李进平， 赵伟 - 力学学报, 2021 - lxxb.cstam.org.cn
高超声速飞行器强激波后高温气体形成具有导电性的等离子体流场, 电离气体为磁场应用提供了
直接工作环境. 磁流体控制技术利用外加磁场影响激波后的离子或电子运动规律 …
直接工作环境. 磁流体控制技术利用外加磁场影响激波后的离子或电子运动规律 …
Magnetohydrodynamic aerobraking shock stand-off measurements with flight representative electrodynamic boundary conditions
DE Gildfind, D Smith, A Lefevre, PA Jacobs… - AIAA Journal, 2022 - arc.aiaa.org
This paper reports on an experimental study of magnetohydrodynamic aerobraking using an
expansion tube facility, which can generate the correct electrodynamic boundary conditions …
expansion tube facility, which can generate the correct electrodynamic boundary conditions …
A Conceptual Modeling Approach for Performance of Magnetohydrodynamic Drag During Planetary Entry
HK Ali, DN Nguyen, RD Braun - Journal of Spacecraft and Rockets, 2024 - arc.aiaa.org
Future higher-mass Mars missions present numerous engineering challenges and will
require significant technological development, particularly of the entry, descent, and landing …
require significant technological development, particularly of the entry, descent, and landing …
Research progress on magnetohydrodynamic flow control under test conditions with high temperature real gas effect
High speed and shock compression behind the bow shock of an aircraft head result in very
high temperature, which would subsequently lead to a conductivity plasma flowfield around …
high temperature, which would subsequently lead to a conductivity plasma flowfield around …
Heat transfer mitigation along superorbital reentry trajectories using magnetohydrodynamic aerobraking
DR Smith, YS Chia, D Gildfind - AIAA Aviation 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-3649. vid This paper investigates
the use of magnetohydrodynamic (MHD) aerobraking as a method for reducing heat loads …
the use of magnetohydrodynamic (MHD) aerobraking as a method for reducing heat loads …
Numerical Study of Plasma Characteristics Under Magnetohydrodynamic Flow Control in Mars Entry
K Tabuchi, T Fujino - Journal of Spacecraft and Rockets, 2024 - arc.aiaa.org
Magnetohydrodynamic flow control is an active thermal protection method for atmospheric
entry vehicles. This study examined the plasma characteristics under magnetohydrodynamic …
entry vehicles. This study examined the plasma characteristics under magnetohydrodynamic …
Coaxial Thermocouple Heat Flux Measurements in Heavily Ionized Flows with Magnetic Fields
A Lefevre, DE Gildfind, CM James - Journal of Thermophysics and Heat …, 2022 - arc.aiaa.org
KNOWLEDGE of heat flux to a vehicle's surface during plan-etary entry is essential to the
design of safe and structurally efficient heat shields. Heat loading will be particularly critical …
design of safe and structurally efficient heat shields. Heat loading will be particularly critical …
Experimental investigation of high velocity neutral flow interaction with a magnetized plasma
Plasma aerocapture is an orbit insertion method that leverages a magnetic dipole plasma to
generate drag by ionizing, capturing, and deflecting atmospheric flow. Key physical …
generate drag by ionizing, capturing, and deflecting atmospheric flow. Key physical …
Side plasma flow and stagnation of a conical blunt body vehicle under an axial dipole magnetic field
C Wang, Z Tian, S Li, Y Hao - Fluid Dynamics Research, 2023 - iopscience.iop.org
The study of plasma flow under the thermal protection magnetic field of reentry vehicle is
helpful to verify the magnetic control thermal protection technology and further understand …
helpful to verify the magnetic control thermal protection technology and further understand …
Theoretical analysis on hypersonic MHD shock stand-off distance of blunt body
High speed and shock compression behind the bow shock of an aircraft head result in very
high temperature, which would subsequently lead to a conductivity plasma flowfield around …
high temperature, which would subsequently lead to a conductivity plasma flowfield around …