نتایج جستجو برای: supersonic separator

تعداد نتایج: 9704  

2013
Da Silva

Numerical study of two dimensional supersonic hydrogen-air mixing layer is performed to investigate the effect of turbulence and chemical additive on ignition distance. Chemical reaction is treated using detail kinetics. Advection upstream splitting method is used to calculate the fluxes and one equation turbulence model is chosen here to simulate the considered problem. Hydrogen peroxide is us...

2003
Hiromu SUGIYAMA Koichi FUKUDA Kazuhide MIZOBATA Liqun SUN Ryojiro MINATO

In order to investigate the supersonic internal flows with shock waves, a new supersonic wind tunnel (pressure-vacuum type, Mach 2.0 and 4.0) was designed and constructed in Muroran Institute of Technology. This paper describes firstly outlines of the new Mach 4 supersonic wind tunnel, and describes secondly the location, structure and characteristics of the Mach 2 and 4 pseudo-shock waves in a...

2018
S'ergio H. Nogueira Vinicius F. dos Santos

Chordal graphs are the graphs in which every cycle of length at least four has a chord. A set S is a vertex separator for vertices a and b if the removal of S of the graph separates a and b into distinct connected components. A graph G is chordal if and only if every minimal vertex separator is a clique. We study subclasses of chordal graphs defined by restrictions imposed on the intersections ...

2014
Shutian Yan Xinran Xiao Xiaosong Huang Xiaodong Li Yue Qi

Porous polypropylene (PP) is commonly used as separator materials for lithium ion batteries (LIB). Its mechanical properties, especially critical for abuse tolerance and durability of LIB, are subject to change in different environments. To capture the mechanical responses of a porous PP separator, its microstructure was mapped into separate atomistic models of bulk crystalline phases and orien...

Journal: :Optics express 2014
Yung-Chih Huang Jui-Wen Pan

In this paper, a novel light separator with contrast ratio enhancement but maintaining the optical efficiency of the DLP projection system is proposed. The main capability of the novel light separator is to direct the uncontrolled light away from the image system. The working theorem for the novel light separator is derived as well. Uncontrolled light is kept away from the image system by a tot...

2017

Understanding of the jet aerodynamics is vital to several areas of implementation of the fluid dynamic science. Due to the significant applications, supersonic under-expanded compressible jets have been investigated widely [1-3]. Also, because of many important physical phenomena, the starting flow fields of supersonic jets have been studied previously [4,5]. Moreover, interaction of the starti...

2003
E. Senocak

sonic Unsteady Lifting Surfaces," AIAA Journal, Vol. 22, No. 2, 1984, pp. 179-186. Tewari, A., "Nonplanar Doublet-Point Method in Supersonic Three-Dimensional, Unsteady Aerodynamics," M.S. Thesis, Univ. of Missouri-Rolla, Rolla, MO, 1988. Tewari, A., "New Acceleration Potential Method for Supersonic Unsteady Aerodynamics of Lifting Surfaces, Further Extension of the Nonplanar Doublet Point Meth...

2014
J. W. Nichols M. R. Jovanović

We use input-output analysis to examine subsonic and supersonic turbulent jet noise. For a supersonic jet, the leading input-output mode closely resembles wavepackets resulting from the parabolized stability equations (PSE). For a subsonic jet, however, input-output analysis produces several sub-optimal modes with nearly the same gain as the leading input-output mode. The sub-optimal modes depe...

2009
Markus Lazar

In this paper we present the equations of motion of a moving screw dislocation in the framework of the translation gauge theory of dislocations. In the gauge field theoretical formulation, a dislocation is a massive gauge field. We calculate the gauge field theoretical solutions of a uniformly moving screw dislocation. We give the subsonic and supersonic solutions. Thus, supersonic dislocations...

2010
Yuki UTSUMI

This paper discusses a multidisciplinary design optimization of a three-dimensional supersonic biplane. First, methods to evaluate the performance of a supersonic biplane are described. The methods include modified oblique shock wave equations, a modified Method of Characteristics, and the reference enthalpy method. Second, validations of the present methods are described. Finally, a multidisci...

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