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知网期刊论文(3940)
在“
Elsevier电子期刊
”中,
命中:
354
条,耗时:小于0.01 秒
在所有数据库中总计命中:
5,910
条
1.
CFD simulations of turbulent nonreacting and reacting flows for
rocket
engine
applications
作者:
Martin J. Seidl
a
;
martin-janos-seidl@web.de
;
Manfred Aigner
a
;
Roman Keller
b
;
Peter Gerlinger
b
关键词:
Real gas
;
Transcritical injection
;
Rocket
combustion chamber
;
CFD
;
DDES
;
Preconditioning
刊名:The Journal of Supercritical Fluids
出版年:2017
2.
Experimental and numerical investigation of combustion in a hydrocarbon and gaseous oxygen fuelled
rocket
作者:
Tausif Shaikh
;
Lalit Patidar
;
Arindrajit Chowdhury
;
arindra@iitb.ac.in" class="auth_mail" title="E-mail the corresponding author
关键词:
Spray
;
Combustion
;
Rocket
;
Model
;
Specific impulse
;
n-Heptane
刊名:Applied Thermal
Engine
ering
出版年:2017
3.
Measurement of acoustic dissipation in an experimental combustor under representative conditions
作者:
Samuel Webster
a
;
samuel.webster@dlr.de
;
Justin Hardi
a
;
Michael Oschwald
a
;
b
关键词:
Thermoacoustics
;
Liquid
Rocket
Combustion
;
Injection Conditions
;
Damping
刊名:Journal of Sound and Vibration
出版年:2017
4.
Coupled heat transfer analysis of thrust chambers with recessed shear coaxial injectors
作者:
Jiawen Song
;
Bing Sun
;
sunbing@buaa.edu.cn
关键词:
Liquid
rocket
engine
;
Turbulent combustion
;
Regenerative cooling
;
Thrust chamber
;
Injector recess
;
Heat transfer
刊名:Acta Astronautica
出版年:2017
5.
Erratum to “Combustion oscillation study in a kerosene fueled
rocket
-based combined-cycle
engine
combustor” [Acta Astronaut. 129 (2016) 260-270]
作者:
Zhi-Wei Huang
;
Guo-Qiang He
;
Fei Qin
qinfei@nwpu.edu.cn
;
Rui Xue
;
Xiang-Geng Wei
;
Lei Shi
刊名:Acta Astronautica
出版年:2017
6.
Yuzhnoye's new liquid
rocket
engine
s as enablers for space exploration
作者:
Alexander Degtyarev
a
;
space@yuzhnoye.com" class="auth_mail" title="E-mail the corresponding author
;
Alexander Kushnaryov
b
;
space@yuzhnoye.com" class="auth_mail" title="E-mail the corresponding author
;
Vladimir Shulga
c
;
space@yuzhnoye.com" class="auth_mail" title="E-mail the corresponding author
;
Oleg Ventskovsky
d
;
oventskovsky@hotmail.com" class="auth_mail" title="E-mail the corresponding author
关键词:
Oxygen-kerosene LRE
;
Closed-cycle scheme
;
Main
rocket
engine
;
Thrust
;
Specific impulse
刊名:Acta Astronautica
出版年:2016
7.
Exploration of combustion instability triggering using Large Eddy Simulation of a multiple injector liquid
rocket
engine
作者:
A. Urbano
;
a
;
b
;
aurbano@imft.fr" class="auth_mail" title="E-mail the corresponding author
;
L. Selle
a
;
b
;
G. Staffelbach
c
;
B. Cuenot
c
;
T. Schmitt
d
;
S. Ducruix
d
;
S. Candel
d
关键词:
Combustion instabilities
;
Liquid
rocket
engine
s
;
LES
刊名:Combustion and Flame
出版年:2016
8.
Experimental investigation of transcritical methane flow in
rocket
engine
cooling channel
作者:
Raffaele Votta
a
;
Francesco Battista
a
;
Vito Salvatore
a
;
Marco Pizzarelli
b
;
marco.pizzarelli@uniroma1.it" class="auth_mail" title="E-mail the corresponding author
;
Giuseppe Leccese
b
;
Francesco Nasuti
b
;
Scott Meyer
c
关键词:
Liquid
rocket
engine
;
Regenerative cooling
;
Transcritical methane
;
Heated channel
;
Nusselt number correlation
;
Channel roughness
刊名:Applied Thermal
Engine
ering
出版年:2016
9.
Preliminary Design Method of a Turbopump Feed System for Liquid
Rocket
Engine
Expander Cycle
作者:
Angelo Leto
a
;
a.leto@cira.it
;
Raffaele Votta
a
;
Aldo Bonfiglioli
b
关键词:
Centrifugal Pump
;
Methane
;
Liquid
Rocket
Engine
刊名:Energy Procedia
出版年:2016
10.
Extinction-reignition superiority in a single-stage sounding hybrid
rocket
作者:
Kazuhisa Chiba
a
;
kazchiba@uec.ac.jp" class="auth_mail" title="E-mail the corresponding author
;
Hideyuki Yoda
b
;
Masahiro Kanazaki
b
;
Toru Shimada
c
关键词:
Hybrid
rocket
engine
;
Extinction&ndash
;
reignition
;
Single-stage sounding launch vehicle
;
Design informatics
;
Multidisciplinary design optimization
刊名:Aerospace Science and Technology
出版年:2016
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