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内部出版物
在“
Elsevier电子期刊
”中,
命中:
189
条,耗时:小于0.01 秒
1.
The effect of kerosene injection on ignition probability of local ignition in a
scramjet
combustor
作者:
Heng Bao
;
baoheng1989@163.com
;
Jin Zhou
zj706@vip.sina.com
;
Yu Pan
scramjet
pan@hotmail.com
关键词:
Spark ignition
;
Kerosene
;
Scramjet
;
Ignition probability
刊名:Acta Astronautica
出版年:2017
2.
A conceptual design of shock-eliminating clover combustor for large scale
scramjet
engine
作者:
Ming-bo Sun
;
wind_flowcfd@163.com
;
Yu-xin Zhao
;
Guo-yan Zhao
;
Yuan Liu
关键词:
Large scale
scramjet
engine
;
Supersonic combustor
;
Circular-to-clover transition
;
Pressure loss
刊名:Acta Astronautica
出版年:2017
3.
Numerical simulation of the unstart process of dual-mode
scramjet
作者:
Ruoyu Deng
a
;
Yingzi Jin
b
;
Heuy Dong Kim
a
;
kimhd@andong.ac.kr" class="auth_mail" title="E-mail the corresponding author
关键词:
Dual-mode
scramjet
;
Isolator
;
Shock train
;
Throat area ratio
;
Unstart process
刊名:International Journal of Heat and Mass Transfer
出版年:2017
4.
Thermal investigation of an internally cooled strut injector for
scramjet
application at moderate and hot gas conditions
作者:
Nils C. Drö
;
ske
;
nils.droeske@itlr.uni-stuttgart.de
;
Felix J. Fö
;
rster
;
Bernhard Weigand
;
Jens von Wolfersdorf
关键词:
Supersonic flow
;
Conjugate heat transfer
;
Infrared thermography
;
Internally cooled strut injector
;
Laser-induced thermal acoustics
刊名:Acta Astronautica
出版年:2017
5.
Numerical investigation on shock train control and applications in a
scramjet
engine
作者:
Fei Xing
a
;
1
;
f.xing@xmu.edu.cn
;
Can Ruan
a
;
2
;
Yue Huang
a
;
3
;
Xiaoyuan Fang
a
;
4
;
Yufeng Yao
b
;
5
刊名:Aerospace Science and Technology
出版年:2017
6.
Characteristics of transverse hydrogen jet in presence of multi air jets within
scramjet
combustor
作者:
M. Barzegar Gerdroodbary
a
;
Keivan Fallah
b
;
keivan.fallah@gmail.com
;
H. Pourmirzaagha
c
关键词:
Supersonic flow
;
Numerical simulation
;
Transverse multi jets
;
Hydrogen jet
;
Micro air jet
刊名:Acta Astronautica
出版年:2017
7.
Computational simulation of multi-strut central lobed injection of hydrogen in a
scramjet
combustor
作者:
Gautam Choubey
;
gautam_dadaa@yahoo.com" class="auth_mail" title="E-mail the corresponding author
;
K.M. Pandey
kmpandey2001@yahoo.com" class="auth_mail" title="E-mail the corresponding author
;
Deepak Sharma
deep.cool.u@gmail.com" class="auth_mail" title="E-mail the corresponding author
;
Ajoy Debbarma
ajoy@debbarma.me" class="auth_mail" title="E-mail the corresponding author
关键词:
CFD
;
Scramjet
;
Combustion efficiency
;
Supersonic combustion
刊名:Perspectives in Science
出版年:2016
8.
The flow feature of transverse hydrogen jet in presence of micro air jets in supersonic flow
作者:
M. Barzegar Gerdroodbary
a
;
mbarzegarg@yahoo.com
;
Younes Amini
b
;
D.D. Ganji
c
;
M. Rahimi Takam
d
关键词:
Supersonic flow
;
Numerical simulation
;
Transverse multi jets
;
Hydrogen jet
;
Multi micro air jets
刊名:Advances in Space Research
出版年:2017
9.
Constant static-temperature heating for hydrogen fueled
scramjet
engine
作者:
Qingchun Yang
;
1
;
hcmsyang@163.com" class="auth_mail" title="E-mail the corresponding author
;
Youhai Zong
2
;
Wen Bao
3
关键词:
Hydrogen fueled
scramjet
;
Constant static-temperature heating
;
Material temperature limit
;
Cycle analysis
刊名:International Journal of Hydrogen Energy
出版年:2016
10.
A model of mode transition logic in dual-mode
scramjet
engines
作者:
Xinyue Hao
1
;
xinyueh_27@163.com" class="auth_mail" title="E-mail the corresponding author
;
Juntao Chang
;
2
;
changjuntao@hit.edu.cn" class="auth_mail" title="E-mail the corresponding author
;
Wen Bao
;
3
;
baowen@hit.edu.cn" class="auth_mail" title="E-mail the corresponding author
;
Zexu Zhang
4
;
zexuzhang@hit.edu.cn" class="auth_mail" title="E-mail the corresponding author
关键词:
Dual-mode
scramjet
engine
;
Mode transition logic
;
Simulation model
刊名:Aerospace Science and Technology
出版年:2016
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