Integration of Arc-jet in Impulse Facility for Hypervelocity Aerothermal Testing with Ablation

被引:3
作者
Chang, Eric Won Keun [1 ]
Joglekar, Chinmay [1 ]
McGilvray, Matthew [1 ]
Hermann, Tobias A. [1 ]
机构
[1] Univ Oxford, Oxford Thermofluids Inst, Dept Engn Sci, Oxford OX2 0ES, England
来源
AIAA SCITECH 2023 FORUM | 2023年
关键词
RADIATIVE HEATING UNCERTAINTY; HYPERBOLIC EARTH ENTRY; REENTRY;
D O I
10.2514/6.2023-2334
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Arc-jets and impulse facilities have been extensively used to investigate the flow physics of planetary re-entry, but they each address different aspects of re-entry flow-fields. This work presents a conceptual design of a dual-facility setup, utilising an arc-jet as a model preheating device in the impulse test facility. This novel preheating apparatus will replicate realistic ablation coupling effects in hypervelocity flows. This paper outlines the major challenges and key considerations for the system integration of arc-jet in the T6 Stalker Tunnel. A small-scale arc-jet facility, OPG1, is currently being developed at the University of Oxford to test the plasma generator, model movement system, and sub-components for the expansion tube testing. Analyses were performed to examine the thermal and structural loads on the model movement system exposed to both plasma and hypervelocity flow. The results showcased that the model movement system will effectively serve dual-facility operations.
引用
收藏
页数:15
相关论文
共 50 条
[1]   Plasma generators for re-entry simulation [J].
AuweterKurtz, M ;
Kurtz, JL ;
Laure, S .
JOURNAL OF PROPULSION AND POWER, 1996, 12 (06) :1053-1061
[2]  
Balter-Peterson A., 1992, 4th Symposium on Multidisciplinary Analysis and Optimization, 1992, DOI DOI 10.2514/6.1992-5041
[3]   Time resolved quantitative imaging of charring in materials at temperatures above 1000 K [J].
Bohrk, Hannah ;
Jemmali, Raouf .
REVIEW OF SCIENTIFIC INSTRUMENTS, 2016, 87 (07)
[4]  
Buquet M., 2022, 9 INT WORKSHOP RAD H
[5]  
Caristia S., 2003, 54 INT ASTR C, DOI [10.2514/6.IAC-03-I.3.04, DOI 10.2514/6.IAC-03-I.3.04]
[6]  
Chang E. W. K., 2022, 9 INT WORKSH RAD HIG
[7]   Hypersonic shock impingement studies on a flat plate: flow separation of laminar boundary layers [J].
Chang, Eric Won Keun ;
Chan, Wilson Y. K. ;
McIntyre, Timothy J. ;
Veeraragavan, Ananthanarayanan .
JOURNAL OF FLUID MECHANICS, 2022, 951
[8]   Hypersonic shock impingement on a heated flat plate at Mach 7 flight enthalpy [J].
Chang, Eric Won Keun ;
Chan, Wilson Y. K. ;
McIntyre, Timothy J. ;
Veeraragavan, Ananthanarayanan .
JOURNAL OF FLUID MECHANICS, 2021, 908
[9]   Electrically-heated flat plate testing in a free-piston driven shock tunnel [J].
Chang, Eric Won Keun ;
Chan, Wilson Y. K. ;
Hopkins, Keill J. ;
McIntyre, Timothy J. ;
Veeraragavan, Ananthanarayanan .
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 103
[10]   Development and commissioning of the T6 Stalker Tunnel [J].
Collen, Peter ;
Doherty, Luke J. ;
Subiah, Suria D. ;
Sopek, Tamara ;
Jahn, Ingo ;
Gildfind, David ;
Geraets, Rowland Penty ;
Gollan, Rowan ;
Hambidge, Christopher ;
Morgan, Richard ;
McGilvray, Matthew .
EXPERIMENTS IN FLUIDS, 2021, 62 (11)