| 查看: 2317 | 回复: 19 | |||
[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？？
|
|||
| 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？？ |
回复此楼» 猜你喜欢
售SCI一区文章，我:8.O.55.1.O.54,科目齐全,可伽急
已经有6人回复
-
售SCI一区T0P文章，我:8O.55.1.O.54,科目全,可伽急
已经有6人回复
-
售SCI文章，我:8O5.5.1.O.54,科目齐全,可+急
已经有6人回复
-
这样的filecode谁见过
已经有7人回复
-
售SCI一区T0P文章，我:8.O.55.1.O54,科目全,可伽急
已经有5人回复
-
售SCI一区文章，我:8.O.55.1.O.54,科目齐全,可伽急
已经有4人回复
-
售SCI一区T0P文章，我:8O.55.1.O.5.4,科目齐全,可+急
已经有5人回复
-
售SCI-T0P文章，我:8O.5.5.1.O.54,科目齐全,可+急
已经有5人回复
-
售SCI一区文章，我:8.O.55.1.O.54,科目齐全,可伽急
已经有5人回复
-
国基金的申报应该改成非等额制，评价高的钱多评价低的钱少，但是增加资助率
已经有5人回复
» 本主题相关价值贴推荐，对您同样有帮助:
- 咨询AMM能检索到第几卷
已经有12人回复
- 请问TTP公司的AMM检索到第几卷了。
已经有3人回复
» 抢金币啦！回帖就可以得到:
-
【火热征稿中！】2026年土木建筑与水利工程国际会议（ICCHE 2026）
+1/181
-
三(三甲基硅基)硼酸酯（CAS：4325-85-3）
+1/87
-
1,3,2-Dioxaphospholane, 2-(2,2,3,3,3-pentafluoropropoxy)-
+1/86
-
1-甲基-1,2-双(三甲基硅氧基)乙烷（CAS：17887-27-3）
+1/86
-
2-氯-1,3,2-二氧磷杂环戊烷（CAS：822-39-9）
+1/86
-
具身智能机器人公司招聘机械结构岗位（工程师、专家、负责人均可）薪酬最高150万
+1/80
-
南京大学医工交叉方向薛璐璐团队招聘脂质纳米材料与RNA递送方向博士后1-2名
+1/73
-
同济大学环境学院肖倩课题组2026年补充招收推免生
+1/30
-
中国科学院西双版纳热带植物园人事处招聘
+1/29
-
哈工大（深圳）何自开团队诚招化学工程与技术专业博士生
+1/27
-
北京理工大学-集成电路与电子学院杰青团队-招博士后
+1/26
-
夏尽秋来，蓄力沉淀，静待硕果成文
+1/8
-
瑞典林雪平大学 高峰课题组 诚聘 氮化物基无机材料方向 博士后1名
+1/7
-
天津大学张小岩教授团队招收2027级推免生（光电子能源、热管理材料与器件、微纳传感）
+1/7
-
有合作举办scopus会议的吗？
+1/6
-
香港理工大学殷骏课题组诚聘1 名博士后以及2 名博士生
+1/5
-
北理工集成电路杰青团队 | 诚招科助理
+1/4
-
请大家抽空欣赏一下我们网站的配图
+1/3
-
北理工集成电路杰青团队 | 诚招科助理
+1/3
-
POSTDOCTORAL POSITION in Structural Virology at the University of Minnesota
+1/1
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
|
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. |
17楼2015-04-02 20:30:21
18楼2015-04-02 20:30:39
20楼2015-04-14 11:07:52
简单回复
kinple2楼
2015-03-11 17:25
回复
The-Autumn(金币+1): 谢谢参与
2015-03-11 17:57
回复
The-Autumn(金币+1): 谢谢参与
2015-03-11 20:54
回复
The-Autumn(金币+1): 谢谢参与
lsp15195楼
2015-03-11 21:04
回复
The-Autumn(金币+1): 谢谢参与
2015-03-11 22:51
回复
The-Autumn(金币+1): 谢谢参与
lsp15198楼
2015-03-12 10:30
回复
caucola10楼
2015-03-13 10:20
回复
