Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Wen-xiang Cai"'
Publikováno v:
In Energy Procedia November 2016 100:248-252
Publikováno v:
Journal of Physics: Conference Series. 2235:012087
Performance of boron-based solid rocket ramjet was carried out by the ground direct connection test rig. Through SEM and EDS analysis of condensed products on the insulation wall of the second combustion chamber, the change of carbonization structure
Publikováno v:
Journal of Physics: Conference Series. 2235:012045
In order to accurately analyze the characteristics of flashboard distortion generator, flow field with different structure and aerodynamic parameters was studied by numerical simulation.Then distribiton of Mach on the AIP interface behind the flashbo
Autor:
Wen-xiang Cai
Publikováno v:
8th AIAA Theoretical Fluid Mechanics Conference.
Publikováno v:
Proceedings of the 2015 International Conference on Communications, Signal Processing, and Systems ISBN: 9783662498293
A microstrip-fed planar ultra-wideband (UWB) monopole antenna with two added tunable bands is presented. The proposed antenna consists of a heptagon radiating patch that covers the 3.1–10.6 GHz (UWB) and two added arms which form the frequency band
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5e587524e8cb7b9e89dbc513a97a8e51
https://doi.org/10.1007/978-3-662-49831-6_46
https://doi.org/10.1007/978-3-662-49831-6_46
Publikováno v:
Applied Mechanics and Materials. :592-596
The meridional channel has an important effect on the flow properties of centrifugal compressor. High performance meridional channel can be obtained by determining Bezier curves, which can realize local optimization to the airfoil expediently. Three
Publikováno v:
Int. J. Turbo Jet-Engines. 30
Publikováno v:
2009 International Conference on Computational Intelligence and Software Engineering.
Flowfield in aero combustor is simulated in three- dimensional curvilinear coordinate system. RNG k-e turbulence model, EBU-SOM turbulence combustion model is used to consider turbulent viscosity and reaction rate in gas phase flow, respectively. In
Publikováno v:
2009 International Conference on Computational Intelligence and Software Engineering.
Based on the combustor model and experimental data of Ref.2, numerical simulations of three different combustor geometries presenting three situations with solid fuel regression were conducted using FLUENT software. The combustor inlet airflow had a
Publikováno v:
2009 International Conference on Computational Intelligence and Software Engineering.
optimization of the pulsejet mainly depends on expensive and difficult experiment measurement. With the development of computer technology and Computational Fluid Dynamics (CFD) [5-7], numerical simulation is utilized to recognize complicated two-pha