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Accession number:
20150500465112
Title: Influence of swirling air on ignition and combustion characteristics in boron-based ducted rocket
Authors:    Wang, Hong-Yuan1 Email author why_cool76@126.com; Xu, Yi-Hua1 Email author xuyihua2003@163.com; Hu, Xu1 Email author huxu_hx@126.com; Zeng, Zhuo-Xiong1 Email author zengzhx@163.com
Author affiliation: 1 School of Aircraft Engineering, Nanchang Hangkong University, Nanchang, China
Corresponding author:    Xu, Yi-Hua
Source title: Applied Mechanics and Materials
Abbreviated source title: Appl. Mech. Mater.
Volume: 684
Issue date: 2014
Publication year: 2014
Pages: 76-82
Language: English
ISSN:    16609336
E-ISSN:    16627482
ISBN-13:    9783038353225
Document type: Conference article (CA)
Conference name: 2014 International Conference on Mechanics and Mechanical Engineering, MME 2014
Conference date: September 13, 2014 - September 14, 2014
Conference location: Wuhan, China
Conference code:    110769
Sponsor: International Standard Recording Code; Trans Tech Publications Inc.
Publisher: Trans Tech Publications Ltd
Abstract: Three-dimensional two-phase flow in the typical double downside 90°afterburning chamber of boron based ducted rocket is numerically simulated by means of Realizable k -Ε turbulence model, one-step eddy-dissipation combustion mode1 and the ignition and combustion mode of boron particles of KING with considering the film moving effect in the high-speed flow. The results show that co-swirl and counter-swirl air in the double side of inlet enters into afterburning chamber to make mixture of air and gas more fully and combustion efficiency increases with the increase of swirl number. Boron particles and total combustion efficiency with co-swirl is higher than counter-swirl when the swirl number is less than 0.179. On the contrary, the counter-swirl is higher than co-swirl when the swirl number greater than 0.385, the co-swirl is balance to the counter-swirl when the swirl number is about 0.2; the ignition time of boron particles is reduced with swirling air, its minimum can be attained when swirl number is 0.385. © (2014) Trans Tech Publications, Switzerland.
Number of references: 11
Main heading:    Two phase flow
Controlled terms:    Boron  -  Combustion  -  Ignition  -  Propulsion  -  Rockets  -  Turbulence models
Uncontrolled terms:    Afterburning chamber  -  Combustion characteristics  -  Combustion efficiencies  -  Ducted rocketed  -  Eddy dissipation  -  High speed flows  -  Propulsion system of aviation and aerospaces  -  Secondary combustion
Classification code:    404.1 Military Engineering -  521.1 Fuel Combustion -  549.3 Nonferrous Metals and Alloys excluding Alkali and Alkaline Earth Metals -  631.1 Fluid Flow, General -  682 Railroad Rolling Stock
DOI: 10.4028/www.scientific.net/AMM.684.76
Database: Compendex
Compilation and indexing terms, © 2015 Elsevier Inc.