高超声速飞行器新型热防护机制研究进展

Wei Liang; Hua Jin; Song He Meng; Qiang Yang; Qing Xuan Zeng; Cheng Hai Xu

doi:10.3873/j.issn.1000-1328.2021.04.002

高超声速飞行器新型热防护机制研究进展

Translated title of the contribution: Research Progress on New Thermal Protection Mechanism of Hypersonic Vehicles

Wei Liang
, Hua Jin^*
, Song He Meng
, Qiang Yang
, Qing Xuan Zeng
, Cheng Hai Xu

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology

Research output: Contribution to journal › Review article › peer-review

32 Scopus citations

Abstract

Starting from the source of aerodynamic thermal load, the principles and progress of a new thermal protection mechanism based on the physical mechanism of flow control, optical radiation control, atomic reorganization, and electron dissipation are introduced. The active control of convection heat, chemical heat and radiant heat is realized from the aspects of regulating environment and materials, the characteristics and shortcomings of the development of a new thermal protection mechanism for hypersonic vehicles are further analyzed, and the suggestions on the key directions of future research in this field are put forward.

Translated title of the contribution	Research Progress on New Thermal Protection Mechanism of Hypersonic Vehicles
Original language	Chinese (Traditional)
Pages (from-to)	409-424
Number of pages	16
Journal	Yuhang Xuebao/Journal of Astronautics
Volume	42
Issue number	4
DOIs	https://doi.org/10.3873/j.issn.1000-1328.2021.04.002
State	Published - 30 Apr 2021

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title = "高超声速飞行器新型热防护机制研究进展",

abstract = "Starting from the source of aerodynamic thermal load, the principles and progress of a new thermal protection mechanism based on the physical mechanism of flow control, optical radiation control, atomic reorganization, and electron dissipation are introduced. The active control of convection heat, chemical heat and radiant heat is realized from the aspects of regulating environment and materials, the characteristics and shortcomings of the development of a new thermal protection mechanism for hypersonic vehicles are further analyzed, and the suggestions on the key directions of future research in this field are put forward.",

keywords = "Chemical heat, Convective heat, Hypersonic vehicle, Radiant heat, Thermal protection mechanism",

author = "Wei Liang and Hua Jin and Meng, \{Song He\} and Qiang Yang and Zeng, \{Qing Xuan\} and Xu, \{Cheng Hai\}",

year = "2021",

month = apr,

day = "30",

doi = "10.3873/j.issn.1000-1328.2021.04.002",

language = "繁体中文",

volume = "42",

pages = "409--424",

journal = "Yuhang Xuebao/Journal of Astronautics",

issn = "1000-1328",

publisher = "Chinese Society of Astronautics",

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TY - JOUR

T1 - 高超声速飞行器新型热防护机制研究进展

AU - Liang, Wei

AU - Jin, Hua

AU - Meng, Song He

AU - Yang, Qiang

AU - Zeng, Qing Xuan

AU - Xu, Cheng Hai

PY - 2021/4/30

Y1 - 2021/4/30

N2 - Starting from the source of aerodynamic thermal load, the principles and progress of a new thermal protection mechanism based on the physical mechanism of flow control, optical radiation control, atomic reorganization, and electron dissipation are introduced. The active control of convection heat, chemical heat and radiant heat is realized from the aspects of regulating environment and materials, the characteristics and shortcomings of the development of a new thermal protection mechanism for hypersonic vehicles are further analyzed, and the suggestions on the key directions of future research in this field are put forward.

AB - Starting from the source of aerodynamic thermal load, the principles and progress of a new thermal protection mechanism based on the physical mechanism of flow control, optical radiation control, atomic reorganization, and electron dissipation are introduced. The active control of convection heat, chemical heat and radiant heat is realized from the aspects of regulating environment and materials, the characteristics and shortcomings of the development of a new thermal protection mechanism for hypersonic vehicles are further analyzed, and the suggestions on the key directions of future research in this field are put forward.

KW - Chemical heat

KW - Convective heat

KW - Hypersonic vehicle

KW - Radiant heat

KW - Thermal protection mechanism

UR - https://www.scopus.com/pages/publications/85107204273

U2 - 10.3873/j.issn.1000-1328.2021.04.002

DO - 10.3873/j.issn.1000-1328.2021.04.002

M3 - 文献综述

AN - SCOPUS:85107204273

SN - 1000-1328

VL - 42

SP - 409

EP - 424

JO - Yuhang Xuebao/Journal of Astronautics

JF - Yuhang Xuebao/Journal of Astronautics

IS - 4

ER -

高超声速飞行器新型热防护机制研究进展

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