Mechanism of Composite Propellant Combustion at High Acceleration

A. H. Hassan; Junxue Ren; Yu Liu

Mechanism of Composite Propellant Combustion at High Acceleration

A. H. Hassan^*
, Junxue Ren
, Yu Liu

^*此作品的通讯作者

宇航学院

Beihang University

科研成果: 会议稿件 › 论文 › 同行评审

摘要

An analytic model is developed to calculate the burning rate augmentation of metallized composite propellant in acceleration field based on BDP multiple flame model. The assumption that heat transfers from the hot particle to the burning surface uniformly is adopted. The behavior of the particles flying off the burning surface which may influence the burning rate is also considered. A calculation sample in the case of uniform flow field and results induced are given.

源语言	英语
页	802-807
页数	6
出版状态	已出版 - 2003
活动	Proceedings of the 2003 International Autumn Seminar on Propellants, Explosives and Pyrotechnics (2003 IASPEP) - Theory and Practice of Energetic Materials - Guilin, 中国期限: 15 10月 2003 → 18 10月 2003

会议

会议	Proceedings of the 2003 International Autumn Seminar on Propellants, Explosives and Pyrotechnics (2003 IASPEP) - Theory and Practice of Energetic Materials
国家/地区	中国
市	Guilin
时期	15/10/03 → 18/10/03

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引用此

@conference{94b15326bbf6473bb21aec764010809b,

title = "Mechanism of Composite Propellant Combustion at High Acceleration",

abstract = "An analytic model is developed to calculate the burning rate augmentation of metallized composite propellant in acceleration field based on BDP multiple flame model. The assumption that heat transfers from the hot particle to the burning surface uniformly is adopted. The behavior of the particles flying off the burning surface which may influence the burning rate is also considered. A calculation sample in the case of uniform flow field and results induced are given.",

keywords = "Acceleration, BDP model, Burning rate, Composite propellant",

author = "Hassan, \{A. H.\} and Junxue Ren and Yu Liu",

year = "2003",

language = "英语",

pages = "802--807",

note = "Proceedings of the 2003 International Autumn Seminar on Propellants, Explosives and Pyrotechnics (2003 IASPEP) - Theory and Practice of Energetic Materials ; Conference date: 15-10-2003 Through 18-10-2003",

}

TY - CONF

T1 - Mechanism of Composite Propellant Combustion at High Acceleration

AU - Hassan, A. H.

AU - Ren, Junxue

AU - Liu, Yu

PY - 2003

Y1 - 2003

N2 - An analytic model is developed to calculate the burning rate augmentation of metallized composite propellant in acceleration field based on BDP multiple flame model. The assumption that heat transfers from the hot particle to the burning surface uniformly is adopted. The behavior of the particles flying off the burning surface which may influence the burning rate is also considered. A calculation sample in the case of uniform flow field and results induced are given.

AB - An analytic model is developed to calculate the burning rate augmentation of metallized composite propellant in acceleration field based on BDP multiple flame model. The assumption that heat transfers from the hot particle to the burning surface uniformly is adopted. The behavior of the particles flying off the burning surface which may influence the burning rate is also considered. A calculation sample in the case of uniform flow field and results induced are given.

KW - Acceleration

KW - BDP model

KW - Burning rate

KW - Composite propellant

UR - https://www.scopus.com/pages/publications/2342577488

M3 - 论文

AN - SCOPUS:2342577488

SP - 802

EP - 807

T2 - Proceedings of the 2003 International Autumn Seminar on Propellants, Explosives and Pyrotechnics (2003 IASPEP) - Theory and Practice of Energetic Materials

Y2 - 15 October 2003 through 18 October 2003

ER -

Mechanism of Composite Propellant Combustion at High Acceleration

摘要

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