非接触声学法测定固体火箭发动机模型燃烧室压力

IF 0.9 4区工程技术 Q4 ENERGY & FUELS

Combustion, Explosion, and Shock Waves Pub Date : 2023-08-01 DOI:10.1134/s0010508223040093

K. E. Kovalev, D. A. Yagodnikov, A. N. Bobrov

引用次数: 0

摘要

本文章由计算机程序翻译，如有差异，请以英文原文为准。

Non-Contact Acoustic Method for Determining the Pressure in the Combustion Chamber of a Model Solid Rocket Motor

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Non-Contact Acoustic Method for Determining the Pressure in the Combustion Chamber of a Model Solid Rocket Motor

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来源期刊

Combustion, Explosion, and Shock Waves 工程技术-材料科学：综合

CiteScore

1.60

自引率

16.70%

发文量

审稿时长

5.7 months

期刊介绍： Combustion, Explosion, and Shock Waves a peer reviewed journal published in collaboration with the Siberian Branch of the Russian Academy of Sciences. The journal presents top-level studies in the physics and chemistry of combustion and detonation processes, structural and chemical transformation of matter in shock and detonation waves, and related phenomena. Each issue contains valuable information on initiation of detonation in condensed and gaseous phases, environmental consequences of combustion and explosion, engine and power unit combustion, production of new materials by shock and detonation waves, explosion welding, explosive compaction of powders, dynamic responses of materials and constructions, and hypervelocity impact.