Design of Modular Test Section for High-Pressure Shock Tube to Enable Endwall Measurements and Imagery

被引：0
|
作者：
Klopp, Samuel Q. [1 ]
Albright, Marley A. [1 ]
McGaunn, Jonathan [1 ]
Pierro, Michael [1 ]
Dennis, Christopher W. [1 ]
Vasu, Subith S. [1 ]
机构：
[1] Univ Cent Florida, Dept Mech & Aerosp Engn, Ctr Adv Turbomachinery & Energy Res, Orlando, FL 32816 USA
来源：
AIAA SCITECH 2024 FORUM | 2024年
关键词：
IGNITION;
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper discusses the motivation behind, design of, and validation of a new test section for UCF's High-Pressure Shock Tube for Advanced Research (HiPER-STAR). The new test section allows for both pressure transducers and windows to be put in place of the endwall, enabling comparison of endwall and sidewall pressure measurements or endwall imaging during experiments up to at high pressures.
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页数：6
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