نتایج جستجو برای: mach

تعداد نتایج: 7270  

2000
H. J. S. Dorren

For the first time an all optical flip-flop is demonstrated based on two coupled Mach-Zehnder interferometers which contain semiconductor optical amplifiers in their arms. The flip-flop operation is discussed and it is demonstrated using commercially available fiber pigtailed devices. Being based on Mach-Zehnder interferometers, the flip-flop has potential for very high speed operation. E-mail:...

In this study, turbulent compressible gas flow in a rectangular micro-channel is numerically investigated. The gas flow assumed to be in the subsonic regime up to Mach number about 0.7. Five low and high Reynolds number RANS turbulence models are used for modeling the turbulent flow. Two types of mesh are generated depending on the employed turbulence model. The computations are performed for R...

اسدی, رضا, خواجه, مهدی, دهقان نیری, هادی,

In this research, design and fabrication of an integrated heterodyne electrooptic modulator in lithium niobate have been presented. In this modulator, the waveguide is made by using proton exchange process; to exert two high frequency signals, deposited electrodes with Mach-Zender arms between them are used. In this method, every electrical signal is applied on one of the Mach-Zender arms, so t...

2009
Andrey E. Miroshnichenko Yuri S. Kivshar

We introduce a concept of the Mach–Zehnder–Fano interferometer by inserting a cavity exhibiting Fano resonance into a conventional interferometer. By employing the scattering-matrix approach, we demonstrate that the transmission becomes sensitive to a position of the cavity such that an asymmetric structure exhibits a series of narrow resonances with almost perfect reflection. We discuss how to...

2003
J. B. Bell M. S. Day C. A. Rendleman S. E. Woosley M. A. Zingale

We introduce a numerical model for the simulation of nuclear flames in Type Ia supernovae. This model is based on a low Mach number formulation that analytically removes acoustic wave propagation while retaining the compressibility effects resulting from nuclear burning. The formulation presented here generalizes low Mach number models used in combustion that are based on an ideal gas approxima...

2006
G. L. Ma S. Zhang Y. G. Ma H. Z. Huang X. Z. Cai J. H. Chen Z. J. He J. L. Long W. Q. Shen X. H. Shi J. X. Zuo

In a framework of a multi-phase transport model with both partonic and hadronic interactions, azimuthal correlations between trigger particles and associated scattering particles (3 < p T < 6 GeV/c and 0.15 < p T < 3 GeV/c (soft), or 2.5 < p trig T < 4 GeV/c and 1 < p assoc T < 2.5 GeV/c (hard)) in Au + Au collisions at √ sNN = 200 GeV have been studied by the mixing-event technique, and Mach-l...

2010
Jeffrey Haack Shi Jin Jian-Guo Liu

The computation of compressible flows becomes more challenging when the Mach number has different orders of magnitude. When the Mach number is of order one, modern shock capturing methods are able to capture shocks and other complex structures with high numerical resolutions. However, if the Mach number is small, the acoustic waves lead to stiffness in time and excessively large numerical visco...

Journal: :Japanese journal of pharmacology 1990
Y Kitamura S Hayashi Y Nomura

Effects of 4-aminomethyl-1-benzylpyrrolidin-2-one-hemifumarate (WEB 1881 FU), a novel pyrrolidinone nootropic, on acetylcholine (ACh) receptors and adrenoceptors were investigated using crude membranes of the rat brain. The affinity order of WEB 1881 FU was: M1-muscarinic (m) ACh receptor greater than M2-mACh receptor greater than alpha 2-adrenoceptor greater than beta-adrenoceptor greater than...

2011
Saeed Farokhi

The effects of a typical glaze ice accretion shape on the performance of the M2129 S-duct inlet are computationally investigated for a range of flight Mach numbers. A Reynolds-Averaged Navier-Stokes (RANS) code with k-o> turbulence model is used to simulate the compressible viscous flow in the S-duct inlet. The glaze ice accretion on the cowl lip is modeled on a steady-state basis f rom N A S A...

2003
Shishir A. Pandya Sankaran Venkateswaran Thomas H. Pulliam

Preconditioning methods have become the method of choice for the solution of flowfields involving the simultaneous presence of low Mach number flow and transonic flow regions. It is well known that these methods are important for insuring accurate numerical discretization as well as convergence efficiency over various operating conditions such as low Mach number, low Reynolds number and high St...

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