Hideaki Aiso
National Aerospace Laboratory
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Featured researches published by Hideaki Aiso.
Nuclear Physics B - Proceedings Supplements | 1997
Hideaki Aiso; J. Fromm; Masahiro Fukuda; Toshiyuki Iwamiya; Atsushi Nakamura; Takashi Nakamura; M. Stingl; Masahiro Yoshida
Abstract We report large scale numerical simulation data for gluon propagators together with an analysis based on the generalized Feynman rules of an extended perturbation scheme. Zwanzigers stochastic gauge fixing algorithm is employed to limit the path integration inside the Gribov region. Obtained propagators do not show a simple physical pole behavior, rather complex-conjugate pairs of singularities in the p2 plain.
arXiv: High Energy Physics - Lattice | 1996
Atsushi Nakamura; Hideaki Aiso; Masahiro Fukuda; Toshiyuki Iwamiya; Takashi Nakamura; Masahiro Yoshida
We present SU(3) gluon propagators calculated on 48*48*48*N_t lattices at beta=6.8 where N_t=64 (corresponding the confinement phase) and N_t=16 (deconfinement) with the bare gauge parameter,alpha, set to be 0.1. In order to avoid Gribov copies, we employ the stochastic gauge fixing algorithm. Gluon propagators show quite different behavior from those of massless gauge fields: (1) In the confinement phase, G(t) shows massless behavior at small and large t, while around 5<t<15 it behaves as massive particle, and (2) effective mass observed in G(z) becomes larger as z increases. (3) In the deconfinement phase, G(z) shows also massive behavior but effective mass is less than in the confinement case. In all cases, slope masses are increasing functions of t or z, which can not be understood as addtional physical poles.We present SU(3) gluon propagators calculated on 48*48*48*N_t lattices at beta=6.8 where N_t=64 (corresponding the confinement phase) and N_t=16 (deconfinement) with the bare gauge parameter,alpha, set to be 0.1. In order to avoid Gribov copies, we employ the stochastic gauge fixing algorithm. Gluon propagators show quite different behavior from those of massless gauge fields: (1) In the confinement phase, G(t) shows massless behavior at small and large t, while around 5<t<15 it behaves as massive particle, and (2) effective mass observed in G(z) becomes larger as z increases. (3) In the deconfinement phase, G(z) shows also massive behavior but effective mass is less than in the confinement case. In all cases, slope masses are increasing functions of t or z, which can not be understood as addtional physical poles.
Journal of Computational and Applied Mathematics | 2003
Rossitza S. Marinova; Tadayasu Takahashi; Hideaki Aiso; Christo I. Christov; Tchavdar T. Marinov
This work is concerned with the conservation properties of a new vectorial operator splitting scheme for solving the incompressible Navier-Stokes equations. It is proven that the difference approximation of the advection operator conserves square of velocity components and the kinetic energy as the differential operator does, while pressure term conserves only the kinetic energy. Some analytical requirements necessary to be satisfied of difference schemes for incompressible Navier-Stokes equations are formulated and discussed. The properties of the methods are illustrated with results from numerical computations for lid-driven cavity flow.
Nuclear Physics B - Proceedings Supplements | 1995
Hideaki Aiso; Masahiro Fukuda; Toshiyuki Iwamiya; Masashi Mizutani; Atsushi Nakamura; Takashi Nakamura; Masahiro Yoshida
We report the first QCD calculations on a parallel vector computer, NWT, which has the peak performance of 236 GFLOPS and 35 GByte memory. After discussing its architecture, our parallel programming strategy, and QCD code performance, we present gluon propagators on a 48 3 × 64 lattice at β = 6.8, which shows the large deviation from the behavior of free massless gauge particles.
Archive | 2003
Jérôme Breil; Jean Paul Caltagirone; Eric Giraud; Hideaki Aiso; Tadayasu Takahashi
Dramatically viscous fluids are required to fill missiles, rockets and the boosters of the Ariane V Rocket. Such a rocket engine is called solid propellant engine, since the dynamic viscosity of the casted material increases in the course of time. At the end of the operation, the propellant becomes solid. Since the geometries we deal with are relatively complex, we solve the three-dimensional Navier-Stokes equations together with the transport of the fluid interface. The rheological behavior of the fluid involved, (the propellant, modelled as a fluid) is Newtonian.
Progress of Theoretical Physics Supplement | 1996
Hideaki Aiso; Masahiro Fukuda; Toshiyuki Iwamiya; Atsushi Nakamura; Takashi Nakamura; Masahiro Yoshida
Archive | 2001
Rossitza S. Marinova; Takashi Takahashi; Hideaki Aiso
Archive | 2004
Hideaki Aiso; Tadayasu Takahashi; Moustafa Abouziarov
Archive | 2004
Moustafa Abouziarov; Hideaki Aiso; Tadayasu Takahashi
Parallel Computational Fluid Dynamics 2002#R##N#New Frontiers and Multi-disciplinary Applications | 2003
Jerome Breil; Rossitza S. Marinova; Hideaki Aiso; Tadayasu Takahashi