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内部出版物
院士团队服务(3)
在“
Elsevier电子期刊
”中,
命中:
14,109
条,耗时:0.0129924 秒
在所有数据库中总计命中:
3
条
1.
Effects of the
inlet
angle on the collection efficiency of a cyclone with helical-roof
inlet
作者:
Dzmitry Misiulia
;
1
;
dzmitry.misiulia@ltu.se
;
Anders Gustav Andersson
anders.g.andersson@ltu.se
;
T. Staffan Lundströ
;
m
staffan.lundstrom@ltu.se
关键词:
Cyclone
;
Inlet
angle
;
Large Eddy Simulation
;
Cut size
;
Collection efficiency
刊名:Powder Technology
出版年:2017
2.
Heat transfer in a two-
inlet
rotating wedge-shaped channel with various locations of the second
inlet
作者:
Hongwu Deng
a
;
denghw@buaa.edu.cn
;
Yancun Cheng
a
;
chengyancun@buaa.edu.cn
;
Yang Li
a
;
buaalzw@126.com
;
Bin Ni
b
;
mechanist@126.com
;
Lu Qiu
a
;
qiulu@buaa.edu.cn
关键词:
Gas turbine heat transfer
;
Rotor blades trailing edge
;
Rotating
;
Multiple
inlet
s
刊名:International Journal of Heat and Mass Transfer
出版年:2017
3.
The concept of double
inlet
-double outlet right ventricle: a distinct congenital heart disease
作者:
Veronica Spadotto
a
;
Carla Frescura
a
;
Siew Yen Ho
b
;
Gaetano Thiene
a
;
gaetano.thiene@unipd.it
关键词:
AV
;
atrioventricular
;
CHD
;
congenital heart disease
;
DIRV
;
double
inlet
right ventricle
;
DORV
;
double outlet right ventricle
;
DI-DORV
;
double
inlet
-double outlet right ventricle
;
LV
;
left ventricle
;
RV
;
right ventricle
;
VA
;
ventriculo-arterial
;
VSD
;
ventricular septal defect
刊名:Cardiovascular Pathology
出版年:2017
4.
Experimental and numerical investigation of smooth turbine-based combined-cycle
inlet
mode transition
作者:
Jun Liu
;
Huacheng Yuan
;
yuan_hch7@sina.com
;
Zhengxu Hua
;
Wenfang Chen
;
Ning Ge
关键词:
Air-breathing hypersonic propulsion system
;
Turbine-based combined-cycle
;
Inlet
mode transition
;
Wind tunnel test
刊名:Aerospace Science and Technology
出版年:2017
5.
Numerical study on hypersonic nozzle-
inlet
starting characteristics in a shock tunnel
作者:
Xiaoliang Jiao
a
;
b
;
jiao_xiaoliang@126.com
;
Juntao Chang
a
;
c
;
changjuntao@hit.edu.cn
;
Zhongqi Wang
a
;
b
;
wang_zhongqi@yeah.net
;
Daren Yu
a
;
b
;
yudaren@hit.edu.cn
关键词:
Hypersonic
inlet
;
Nozzle
;
Shock tunnel
;
Pulse-starting
;
High Mach number
;
Local unstart
刊名:Acta Astronautica
出版年:2017
6.
Effect of
inlet
conditions on swirling turbulent reacting flows in a solid fuel ramjet engine
作者:
Omer Musa
a
;
b
;
omer.musa1@hotmail.com
;
Chen Xiong
a
;
Zhou Changsheng
a
;
Weixuan Li
a
关键词:
Regression rate
;
Swirl flow
;
Solid fuel ramjet
;
Inlet
conditions
;
Combustion
刊名:Applied Thermal Engineering
出版年:2017
7.
A kinetic
inlet
model for CFD simulation of large-scale bubble columns
作者:
Weibin Shi
a
;
b
;
Ning Yang
a
;
nyang@ipe.ac.cn
;
Xiaogang Yang
b
关键词:
CFD modelling
;
Bubble columns
;
DBS drag model
;
Gas distributor
;
New
inlet
model
;
Large-scale
刊名:Chemical Engineering Science
出版年:2017
8.
Transfer matrix methods for sound attenuation in resonators with perforated intruding
inlet
s
作者:
Rong Guo
;
guorong@tongji.edu.cn" class="auth_mail" title="E-mail the corresponding author
;
Wen-bo Tang
关键词:
Perforated intruding
inlet
;
Transfer matrix method
;
Transmission loss
;
Acoustic performance
刊名:Applied Acoustics
出版年:2017
9.
Heat transfer characteristics in a rotating trailing edge internal cooling channel with two coolant
inlet
s
作者:
Yang Li
;
Hongwu Deng
;
denghw@buaa.edu.cn" class="auth_mail" title="E-mail the corresponding author
;
Zhi Tao
;
Guoqiang Xu
;
Yanan Chen
关键词:
Blade trailing edge
;
Two-
inlet
inflow
;
Rotating heat transfer
;
Wedge-shaped channel
刊名:International Journal of Heat and Mass Transfer
出版年:2017
10.
Effect of the
inlet
manifold on the performance of a hollow fiber membrane module-A CFD study
作者:
Liwei Zhuang
a
;
zlwdml3344@hotmail.com
;
Hanfei Guo
b
;
Gance Dai
a
;
Zhen-liang Xu
a
;
chemxuzl@ecust.edu.cn
关键词:
Hollow fiber membrane module
;
Inlet
manifold
;
Three-dimensional CFD simulation
;
Energy consumption
;
Fluid flow distribution
刊名:Journal of Membrane Science
出版年:2017
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