Experimental study of Al agglomeration on solid propellant burning surface and condensed combustion products-Reference-Cited by-同舟云学术

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Experimental study of Al agglomeration on solid propellant burning surface and condensed combustion products

Published:2022-06 Issue: Volume: Page:
ISSN:2214-9147
Container-title:Defence Technology
language:en
Short-container-title:Defence Technology

Author:

Tu Cheng-yin,Chen Xiong,Li Ying-kun^ORCID,Zhang Bei-chen,Zhou Chang-sheng

Funder

National Natural Science Foundation of China

Six Talent Peaks Project in Jiangsu Province

Fundamental Research Funds for the Central Universities

Six Talent Climax Foundation of Jiangsu

Publisher

Elsevier BV

Subject

Metals and Alloys,Mechanical Engineering,Ceramics and Composites,Computational Mechanics

Reference60 articles.

1. Progress in oxidation mechanism and combustion theory of aluminum particles;Zhou;Ordnance Material Sci Eng,2017

2. Research status of solid rocket motor condensed phase particle distribution;Zhang;J Solid Rocket Technol,2000

3. Characterization of the initial agglomerates of aluminized composite propellants;Liu;Acta Astronaut,2021

4. Flow inside a solid rocket motor with relation to nozzle inlet ablation;Shimada;AIAA J,2007

5. Aluminum combustion driven instabilities in solid rocket motors;Gallier;J Propul Power,2009

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