A Survey of Drag and Heat Reduction Induced by Forward-Facing Cavity and Its Combinations

Thermal protection technology is a key technology in the design of hypersonic aircraft. In order to achieve more effective drag reduction and heat protection, scholars have proposed a variety of thermal protection schemes. The forward-facing cavity and its combinations is one of the most effective a...

Descripción completa

Guardado en:

Detalles Bibliográficos
Autor principal:	Zhang Jie, Xiao Feng, Huang Wei, Yan Li, Meng Yushan
Formato:	article
Lenguaje:	ZH
Publicado:	Editorial Office of Aero Weaponry 2021
Materias:	\|drag reduction\|thermal protection\|forward-facing cavity\|counterflowing jet\|energy deposition\|hypersonic vehicle\|thermal protection technology Motor vehicles. Aeronautics. Astronautics TL1-4050
Acceso en línea:	https://doaj.org/article/edc46b4fabf440efb1eb9ea84b8aa5c2
Etiquetas:	Agregar Etiqueta Sin Etiquetas, Sea el primero en etiquetar este registro!

id	oai:doaj.org-article:edc46b4fabf440efb1eb9ea84b8aa5c2
record_format	dspace
spelling	oai:doaj.org-article:edc46b4fabf440efb1eb9ea84b8aa5c22021-11-30T00:13:33ZA Survey of Drag and Heat Reduction Induced by Forward-Facing Cavity and Its Combinations1673-504810.12132/ISSN.1673-5048.2021.0020https://doaj.org/article/edc46b4fabf440efb1eb9ea84b8aa5c22021-08-01T00:00:00Zhttps://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/1631769540428-1049766306.pdfhttps://doaj.org/toc/1673-5048Thermal protection technology is a key technology in the design of hypersonic aircraft. In order to achieve more effective drag reduction and heat protection, scholars have proposed a variety of thermal protection schemes. The forward-facing cavity and its combinations is one of the most effective and promising active thermal protection schemes. This paper introduces the mechanism of single forward-facing cavity and its combination with counterflowing jet, energy deposition and divergent coding, and summarizes their research status. It puts forward the outlook for the future, especially to follow up and innovate the existing combination schemes, and conduct more ground tests to support the numerical simulation results, with a view to early application in the engineering practice.Zhang Jie, Xiao Feng, Huang Wei, Yan Li, Meng YushanEditorial Office of Aero Weaponryarticle\|drag reduction\|thermal protection\|forward-facing cavity\|counterflowing jet\|energy deposition\|hypersonic vehicle\|thermal protection technologyMotor vehicles. Aeronautics. AstronauticsTL1-4050ZHHangkong bingqi, Vol 28, Iss 4, Pp 16-23 (2021)
institution	DOAJ
collection	DOAJ
language	ZH
topic	\|drag reduction\|thermal protection\|forward-facing cavity\|counterflowing jet\|energy deposition\|hypersonic vehicle\|thermal protection technology Motor vehicles. Aeronautics. Astronautics TL1-4050
spellingShingle	\|drag reduction\|thermal protection\|forward-facing cavity\|counterflowing jet\|energy deposition\|hypersonic vehicle\|thermal protection technology Motor vehicles. Aeronautics. Astronautics TL1-4050 Zhang Jie, Xiao Feng, Huang Wei, Yan Li, Meng Yushan A Survey of Drag and Heat Reduction Induced by Forward-Facing Cavity and Its Combinations
description	Thermal protection technology is a key technology in the design of hypersonic aircraft. In order to achieve more effective drag reduction and heat protection, scholars have proposed a variety of thermal protection schemes. The forward-facing cavity and its combinations is one of the most effective and promising active thermal protection schemes. This paper introduces the mechanism of single forward-facing cavity and its combination with counterflowing jet, energy deposition and divergent coding, and summarizes their research status. It puts forward the outlook for the future, especially to follow up and innovate the existing combination schemes, and conduct more ground tests to support the numerical simulation results, with a view to early application in the engineering practice.
format	article
author	Zhang Jie, Xiao Feng, Huang Wei, Yan Li, Meng Yushan
author_facet	Zhang Jie, Xiao Feng, Huang Wei, Yan Li, Meng Yushan
author_sort	Zhang Jie, Xiao Feng, Huang Wei, Yan Li, Meng Yushan
title	A Survey of Drag and Heat Reduction Induced by Forward-Facing Cavity and Its Combinations
title_short	A Survey of Drag and Heat Reduction Induced by Forward-Facing Cavity and Its Combinations
title_full	A Survey of Drag and Heat Reduction Induced by Forward-Facing Cavity and Its Combinations
title_fullStr	A Survey of Drag and Heat Reduction Induced by Forward-Facing Cavity and Its Combinations
title_full_unstemmed	A Survey of Drag and Heat Reduction Induced by Forward-Facing Cavity and Its Combinations
title_sort	survey of drag and heat reduction induced by forward-facing cavity and its combinations
publisher	Editorial Office of Aero Weaponry
publishDate	2021
url	https://doaj.org/article/edc46b4fabf440efb1eb9ea84b8aa5c2
work_keys_str_mv	AT zhangjiexiaofenghuangweiyanlimengyushan asurveyofdragandheatreductioninducedbyforwardfacingcavityanditscombinations AT zhangjiexiaofenghuangweiyanlimengyushan surveyofdragandheatreductioninducedbyforwardfacingcavityanditscombinations
_version_	1718406897854316544

A Survey of Drag and Heat Reduction Induced by Forward-Facing Cavity and Its Combinations

Ejemplares similares