Effects of air properties on flow filed characteristics of inflatable reentry decelerator

Air properties are very important for predicting the flow filed characteristics of aircraft. At present, Sutherland formula is always used to predict the flow filed characteristics of inflatable reentry decelerator. However, high temperature can be observed in high speed reentry flow around inflatab...

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Main Authors: HE Qingsong, WANG Guangxing, WANG Qi, ZHANG Zhang, WANG Liwu, JIA He
Format: Article
Language:zho
Published: EDP Sciences 2022-02-01
Series:Xibei Gongye Daxue Xuebao
Subjects:
Online Access:https://www.jnwpu.org/articles/jnwpu/full_html/2022/01/jnwpu2022401p158/jnwpu2022401p158.html
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author HE Qingsong
WANG Guangxing
WANG Qi
ZHANG Zhang
WANG Liwu
JIA He
author_facet HE Qingsong
WANG Guangxing
WANG Qi
ZHANG Zhang
WANG Liwu
JIA He
author_sort HE Qingsong
collection DOAJ
description Air properties are very important for predicting the flow filed characteristics of aircraft. At present, Sutherland formula is always used to predict the flow filed characteristics of inflatable reentry decelerator. However, high temperature can be observed in high speed reentry flow around inflatable reentry decelerator, thus the Sutherland formula is not suitable for reentry flow simulation of inflatable reentry decelerator. In order to investigate the effect of the air properties on the flow filed characteristics of inflatable reentry decelerator, and provides the theoretical references for the inflatable reentry decelerator design, the Gupta fitting formula and Sutherland formula are used to describe the air properties, respectively, for studying the flow filed characteristics of inflatable reentry decelerator. The results show that the reentry flow temperature with Gupta fitting formula used is lower than that with Sutherland formula used, and the temperature difference is more obvious in the high inflow Mach number and temperature cases. The results in the windward of inflatable reentry decelerator show that the Sutherland formula underestimates the heat flux and pressure, and the heat flux difference is much more obvious. Such as case 5, the peak heat flux obtained by Gupta fitting formula is by 29% higher than that obtained by Sutherland formula.
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spelling doaj.art-bd34a002b5ee436abaf54a86aee4b85d2023-10-02T07:41:18ZzhoEDP SciencesXibei Gongye Daxue Xuebao1000-27582609-71252022-02-0140115816610.1051/jnwpu/20224010158jnwpu2022401p158Effects of air properties on flow filed characteristics of inflatable reentry deceleratorHE Qingsong0WANG Guangxing1WANG Qi2ZHANG Zhang3WANG Liwu4JIA He5Beijing Institute of Space Mechanics & ElectricityBeijing Institute of Space Mechanics & ElectricityBeijing Institute of Space Mechanics & ElectricityBeijing Institute of Space Mechanics & ElectricityBeijing Institute of Space Mechanics & ElectricityBeijing Institute of Space Mechanics & ElectricityAir properties are very important for predicting the flow filed characteristics of aircraft. At present, Sutherland formula is always used to predict the flow filed characteristics of inflatable reentry decelerator. However, high temperature can be observed in high speed reentry flow around inflatable reentry decelerator, thus the Sutherland formula is not suitable for reentry flow simulation of inflatable reentry decelerator. In order to investigate the effect of the air properties on the flow filed characteristics of inflatable reentry decelerator, and provides the theoretical references for the inflatable reentry decelerator design, the Gupta fitting formula and Sutherland formula are used to describe the air properties, respectively, for studying the flow filed characteristics of inflatable reentry decelerator. The results show that the reentry flow temperature with Gupta fitting formula used is lower than that with Sutherland formula used, and the temperature difference is more obvious in the high inflow Mach number and temperature cases. The results in the windward of inflatable reentry decelerator show that the Sutherland formula underestimates the heat flux and pressure, and the heat flux difference is much more obvious. Such as case 5, the peak heat flux obtained by Gupta fitting formula is by 29% higher than that obtained by Sutherland formula.https://www.jnwpu.org/articles/jnwpu/full_html/2022/01/jnwpu2022401p158/jnwpu2022401p158.htmlair transport propertiesgupta fitting formulasutherland formulainflatable reentry deceleratorsimulation
spellingShingle HE Qingsong
WANG Guangxing
WANG Qi
ZHANG Zhang
WANG Liwu
JIA He
Effects of air properties on flow filed characteristics of inflatable reentry decelerator
Xibei Gongye Daxue Xuebao
air transport properties
gupta fitting formula
sutherland formula
inflatable reentry decelerator
simulation
title Effects of air properties on flow filed characteristics of inflatable reentry decelerator
title_full Effects of air properties on flow filed characteristics of inflatable reentry decelerator
title_fullStr Effects of air properties on flow filed characteristics of inflatable reentry decelerator
title_full_unstemmed Effects of air properties on flow filed characteristics of inflatable reentry decelerator
title_short Effects of air properties on flow filed characteristics of inflatable reentry decelerator
title_sort effects of air properties on flow filed characteristics of inflatable reentry decelerator
topic air transport properties
gupta fitting formula
sutherland formula
inflatable reentry decelerator
simulation
url https://www.jnwpu.org/articles/jnwpu/full_html/2022/01/jnwpu2022401p158/jnwpu2022401p158.html
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AT wangqi effectsofairpropertiesonflowfiledcharacteristicsofinflatablereentrydecelerator
AT zhangzhang effectsofairpropertiesonflowfiledcharacteristicsofinflatablereentrydecelerator
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