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[交流]
AMM上周检索了656,……,629这几卷，说明接下是不是其他的卷也会开始检索了？？
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| 在AMM644-650上水了一篇文章，但是到现在还没有检索，去年6月的会议，已经过去9个月了，现在焦急的等待中，3月2号的时候查到了会议的信息了，各位了解接下来一个月左右检索的可能性大不？？ |
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12楼2015-03-18 14:52:53
19楼2015-04-02 21:55:09
6楼2015-03-11 21:27:39
9楼2015-03-13 10:16:03
11楼2015-03-13 11:30:52
13楼2015-03-18 15:27:24
14楼2015-03-18 19:18:10
15楼2015-03-29 15:53:22
16楼2015-03-30 09:26:40
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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. |
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kinple2楼
2015-03-11 17:25
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The-Autumn(金币+1): 谢谢参与
2015-03-11 17:57
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The-Autumn(金币+1): 谢谢参与
2015-03-11 20:54
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The-Autumn(金币+1): 谢谢参与
lsp15195楼
2015-03-11 21:04
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The-Autumn(金币+1): 谢谢参与
2015-03-11 22:51
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The-Autumn(金币+1): 谢谢参与
lsp15198楼
2015-03-12 10:30
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caucola10楼
2015-03-13 10:20
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