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内部出版物
Springer电子图书(2)
SpringerLink电子期刊(96)
NATURE电子期刊(3)
Elsevier电子期刊(70)
在“
Elsevier电子期刊
”中,
命中:
70
条,耗时:0.0139933 秒
在所有数据库中总计命中:
171
条
1.
Cascade nonlinear feedforward-feedback control of stagnation pressure in a
supersonic
blowdown
wind
tunnel
作者:
Biljana Ilić
a
;
biljana.ilic@icloud.com
;
Marko Milo&scaron
;
b
;
Jovan Isaković
c
关键词:
Blowdown
wind
tunnel
;
Supersonic
flow control
;
Stagnation pressure
;
Mathematical model
;
Simulation
;
Cascade control
;
Feedforward control
;
Feedback control
刊名:Measurement
出版年:2017
2.
Flow characteristics of various three-dimensional rounded contour bumps in a Mach 1.3 freestream
作者:
Kin Hing Lo
;
kinhing.lo@glasgow.ac.uk" class="auth_mail" title="E-mail the corresponding author
;
Konstantinos Kontis
kostas.kontis@glasgow.ac.uk" class="auth_mail" title="E-mail the corresponding author
关键词:
Rounded contour bump
;
Supersonic
wind
tunnel
;
Flow control
;
Active blowing jet
刊名:Experimental Thermal and Fluid Science
出版年:2017
3.
RANS simulations of a tandem nozzle
supersonic
wind
tunnel
作者:
Jie Wu
a
;
b
;
j.wu@tu-bs.de" class="auth_mail" title="E-mail the corresponding author
;
wu.jie@ntu.edu.sg" class="auth_mail" title="E-mail the corresponding author
;
Xijin Liu
a
;
xijin.liu@tu-bs.de" class="auth_mail" title="E-mail the corresponding author
;
Rolf Radespiel
a
;
r.radespiel@tu-bs.de" class="auth_mail" title="E-mail the corresponding author
关键词:
Supersonic
wind
tunnel
;
Perforated plate
;
Flow quality
;
CFD
;
Settling chamber
刊名:Aerospace Science and Technology
出版年:2016
4.
Stagnation Pressure Transient Control in a
Supersonic
Blowdown
Wind
Tunnel
Test Facility
作者:
Biljana Ilić
a
;
biljana.ilic@icloud.com" class="auth_mail" title="E-mail the corresponding author
;
Mirko Milosavljević
a
;
Jovan Isaković
b
;
Marko Milo&scaron
;
c
关键词:
Supersonic
wind
tunnel
;
flow parameters
;
stagnation pressure
;
feedforward control
;
PI controller
刊名:Materials Today: Proceedings
出版年:2016
5.
Design and implementation of rigid-flexible coupling for a half-flexible single jack nozzle
作者:
Pengfei Chen
a
;
zhongguoren.cpf@qq.com
Author Vitae
;
Feng Wu
a
;
wufeng_my@qq.com
Author Vitae
;
Jinglei Xu
b
;
xujl@nuaa.edu.cn
Author Vitae
;
Xudong Feng
a
;
363166446@qq.com
Author Vitae
;
Qiao Yang
a
;
kubyka@126.com
Author Vitae
关键词:
Aerodynamic profile
;
Flow-field quality
;
Free jet
;
Nozzle
;
Rigid-flexible coupling
;
Variable Mach number
;
Wind
tunnel
刊名:Chinese Journal of Aeronautics
出版年:2016
6.
Hypervelocity ballistic reference models as experimental
supersonic
test cases
作者:
Dijana Damljanović
a
;
Bo&scaron
;
ko Ra&scaron
;
uo
b
;
brasuo@mas.bg.ac.rs" class="auth_mail" title="E-mail the corresponding author
;
Đorđe Vuković
a
;
Slobodan Mandić
a
;
Jovan Isaković
c
关键词:
Hypervelocity reference models
;
Experimental
supersonic
test cases
;
Model support sting limitations
;
Numerical software tools
刊名:Aerospace Science and Technology
出版年:2016
7.
Numerical modelling of Mars
supersonic
disk-gap-band parachute inflation
作者:
Xinglong Gao
1
;
happy1987long@gmail.com" class="auth_mail" title="E-mail the corresponding author
;
Qingbin Zhang
1
;
qingbinzhang@sina.com" class="auth_mail" title="E-mail the corresponding author
;
Qiangang Tang
;
441547742@qq.com" class="auth_mail" title="E-mail the corresponding author
关键词:
Mars entry
;
Supersonic
parachute
;
Fluid-structure interactions
;
Inflation dynamics
;
Arbitrary Lagrange Euler
;
Compressible flow
刊名:Advances in Space Research
出版年:2016
8.
The effects of cross section variations on the pressure distribution around a long axisymmetric body
作者:
Mohammad Reza Heidari
heidarimr@piau.ac.ir" class="auth_mail" title="E-mail the corresponding author
关键词:
Supersonic
flow
;
Pressure distribution
;
Boundary layer tripping
;
Cross section variation
;
Long axisymmetric body
;
Wind
Tunnel
Test
刊名:Aerospace Science and Technology
出版年:2016
9.
Control of flow separation on a contour bump by jets in a Mach 1.9 free-stream: An experimental study
作者:
Kin Hing Lo
;
kinhing.lo@glasgow.ac.uk" class="auth_mail" title="E-mail the corresponding author
;
Hossein Zare-Behtash
hossein.zare-behtash@glasgow.ac.uk" class="auth_mail" title="E-mail the corresponding author
;
Konstantinos Kontis
kostas.kontis@glasgow.ac.uk" class="auth_mail" title="E-mail the corresponding author
关键词:
Contour bump
;
Active jet
;
Supersonic
free-stream
刊名:Acta Astronautica
出版年:2016
10.
Experimental investigations on cavity-actuated under-expanded
supersonic
oscillating jet
作者:
Bo SunAuthor Vitae
;
Xiaochen Luo
;
luonuaa@163.com" class="auth_mail" title="E-mail the corresponding author
Author Vitae
;
Feng FengAuthor Vitae
;
Xiaosong WuAuthor Vitae
关键词:
Jet cavity interactions
;
Jet flipping
;
Oscillating jet
;
Supersonic
jet
;
Wind
-
tunnel
testing
刊名:Chinese Journal of Aeronautics
出版年:2015
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