Experimental and numerical study on measuring solid-propellant pressure-coupled response using an improved rotary valve-Reference-Cited by-同舟云学术

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Experimental and numerical study on measuring solid-propellant pressure-coupled response using an improved rotary valve

Published:2021-03 Issue: Volume:180 Page:155-169
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Xi Yunzhi,Wang Ningfei,Li Junwei,Ma Baoyin,Zhang Zhihui,Han Lei

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference33 articles.

1. Historical perspective of combustion instability in motors - case studies;Blomshield,2001

2. Segmented SRM pressure oscillation demonstrator;Mastrangelo,2011

3. Combustion instabilities in propulsion systems;Culick,1996

4. Unsteady Motions in Combustion Chambers for Propulsion Systems, NATO RTO-AG-AVT-039;Culick,2006

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1. Experimental investigation of solid propellants combustion response to pressure oscillations using advanced high-resolution diagnostics;Applied Energy;2025-01

2. Hexahedral mesh generation for configurations sharing the same topology with solid torus;2023-12-21

3. AP/HTPB combustion response simulation with a new equivalent linear system method;Combustion and Flame;2023-01

4. In situ monitoring of solid propellants under compressive load by MWCNT piezoresistive sensor;Journal of Mechanics of Materials and Structures;2022-12-10

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