×
验证码:
换一张
忘记密码?
记住我
CORC
首页
科研机构
检索
知识图谱
申请加入
托管服务
登录
注册
在结果中检索
科研机构
工程热物理研究所 [21]
力学研究所 [7]
清华大学 [3]
大连理工大学 [2]
北京大学 [1]
西安交通大学 [1]
更多...
内容类型
会议论文 [37]
发表日期
2017 [4]
2015 [4]
2014 [6]
2013 [2]
2012 [2]
2011 [2]
更多...
学科主题
Combustion... [4]
Combustion... [2]
Combustion... [2]
×
知识图谱
CORC
开始提交
已提交作品
待认领作品
已认领作品
未提交全文
收藏管理
QQ客服
官方微博
反馈留言
浏览/检索结果:
共37条,第1-10条
帮助
限定条件
内容类型:会议论文
已选(
0
)
清除
条数/页:
5
10
15
20
25
30
35
40
45
50
55
60
65
70
75
80
85
90
95
100
排序方式:
请选择
作者升序
作者降序
题名升序
题名降序
发表日期升序
发表日期降序
提交时间升序
提交时间降序
THE EFFECTS OF THE AIR-FUEL VELOCITY RATIO ON TURBULENT NON-PREMIXED BLUFF-BODY FLAMES
会议论文
Charlotte, NC, JUN 26-30, 2017
作者:
Yang T
;
Zhang J(张健)
;
Zhang, J (reprint author), Chinese Acad Sci, Inst Mech, LNM, Beijing 100190, Peoples R China.
收藏
  |  
浏览/下载:23/0
  |  
提交时间:2018/01/16
Large-eddy Simulation
Variable Approach
Disc Stabilizer
Combustion
Jet
Mechanisms
Burner
Flow
Development of zone flamelet model for scramjet combustor modeling
会议论文
Xiamen, China, 6-9 March 2017
作者:
Yao W(姚卫)
;
Fan XJ(范学军)
收藏
  |  
浏览/下载:17/0
  |  
提交时间:2018/01/16
Combustion
Cost Benefit Analysis
Costs
Mixtures
Spacecraft
Supersonic Aircraft
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection
会议论文
Xiamen, China, 6-9 March 2017
作者:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
收藏
  |  
浏览/下载:19/0
  |  
提交时间:2018/01/16
Combustion
Diesel Engines
Hydrogen
Large Eddy Simulation
Spacecraft
Stabilization
Supersonic Aircraft
Temperature Measurement
Wall Flow
Development of zone flamelet modelfor scramjet combustor modeling
会议论文
Xiamen, China, March 6, 2017 - March 9, 2017
作者:
Yao W(姚卫)
;
Fan XJ(范学军)
收藏
  |  
浏览/下载:30/0
  |  
提交时间:2018/11/08
Combustion
Cost benefit analysis
Costs
Mixtures
Ramjet engines
Supersonic aircraft
Computational costs
Equivalence ratios
Local flow conditions
Scramjet combustors
Statistics approaches
Supersonic combustion
Supersonic combustors
Turbulent combustion
Development and Validation of a Partially Coupled Soot Model for Turbulent Kerosene Combustion in View of Application to Gas Turbines
会议论文
ASME, 2015
作者:
Bijan Shahriari
;
Murray Thomson
;
Seth Dworkin
收藏
  |  
浏览/下载:11/0
  |  
提交时间:2016/01/25
A conceptual design of next generation hypersonic air-breathing airplanes with dual waveriders forebody
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:
Cui K(崔凯)
;
Hu SC(胡守超)
;
Li GL
;
Xiao Y(肖尧)
;
Situ M
收藏
  |  
浏览/下载:20/0
  |  
提交时间:2017/05/05
Aero
dynamic performance
Aerodynamic performance predictions
Design Methodology
Flight altitudes
Numerical results
Propulsion system
Turbulent models
Wing body aircraft
On the discrepancy in the reaction rate descriptions of turbulent premixed combustion in porous media at different scales
会议论文
12th International Conference on Combustion and Energy Utilisation (ICCEU), Lancaster, ENGLAND, 2014-05-25
作者:
Chen, Zhong-Shan
;
Xie, Mao-Zhao
;
Liu, Hong-Shen
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/09
premixed combustion
porous media
EDC model
weighted average method
A numerical investigation on characteristics of turbulent premixed flame in porous media
会议论文
12th International Conference on Combustion and Energy Utilisation (ICCEU), Lancaster, ENGLAND, 2014-05-25
作者:
Chen, Zhong-Shan
;
Xie, Mao-Zhao
;
Liu, Hong-Sheng
;
Yue, Meng
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/09
turbulent combustion
porous media
flame thickness
Damkohler number
EDC model
Flame Front Detection and Curvature Calculation Using Level Set
会议论文
11th World Congress on Intelligent Control and Automation (WCICA 2014), Shenyang, China, June 29 - July 4, 2014
作者:
Fan HJ(范慧杰)
;
Cong Y(丛杨)
;
Xia Y(夏泳)
;
Shao, Weiwei
;
Wang, Yue
收藏
  |  
浏览/下载:28/0
  |  
提交时间:2014/12/29
level set
flame shape
combustion
flame structure
Analysis of Turbulent Swirling Flow in an Isothermal Gas Turbine Combustor Model
会议论文
ASME, 2014
A. C. Benim
;
S. Iqbal
;
A. Nahavandi
;
W. Meier
;
A. Wiedermann
;
Franz Joos
收藏
  |  
浏览/下载:18/0
  |  
提交时间:2015/01/05
©版权所有 ©2017 CSpace - Powered by
CSpace