Estimation of Wire Length Distribution for Evaluating Performance Improvement of Three-Dimensional LSI

2005 ◽  
Author(s):  
Jun Deguchi ◽  
Yoshihiro Nakatani ◽  
Takeaki Sugimura ◽  
Takafumi Fukushima ◽  
Mitsumasa Koyanagi
2006 ◽  
Vol 45 (4B) ◽  
pp. 3260-3265 ◽  
Author(s):  
Jun Deguchi ◽  
Takeaki Sugimura ◽  
Yoshihiro Nakatani ◽  
Takafumi Fukushima ◽  
Mitsumasa Koyanagi

1997 ◽  
Vol 473 ◽  
Author(s):  
J. A. Davis ◽  
J. D. Meindl

ABSTRACTOpportunities for Gigascale Integration (GSI) are governed by a hierarchy of physical limits. The levels of this hierarchy have been codified as: 1) fundamental, 2) material, 3) device, 4) circuit and 5) system. Many key limits at all levels of the hierarchy can be displayed in the power, P, versus delay, td, plane and the reciprocal length squared, L-2, versus response time, τ, plane. Power, P, is the average power transfer during a binary switching transition and delay, td, is the time required for the transition. Length, L, is the distance traversed by an interconnect that joins two nodes on a chip and response time, τ, characterizes the corresponding interconnect circuit. At the system level of the hierarchy, quantitative definition of both the P versus td and the L-2 versus τ displays requires an estimate of the complete stochastic wiring distribution of a chip.Based on Rent's Rule, a well known empirical relationship between the number of signal input/output terminals on a block of logic and the number of gate circuits with the block, a rigorous derivation of a new complete stochastic wire length distribution for an on-chip random logic network is described. This distribution is compared to actual data for modern microprocessors and to previously described distributions. A methodology for estimating the complete wire length distribution for future GSI products is proposed. The new distribution is then used to enhance the critical path model that determines the maximum clock frequency of a chip; to derive a preliminary power dissipation model for a random logic network; and, to define an optimal architecture of a multilevel interconnect network that minimizes overall chip size. In essence, a new complete stochastic wiring distribution provides a generic basis for maximizing the value obtained from a multilevel interconnect technology.


Author(s):  
Jie Gao ◽  
Chunde Tao ◽  
Dongchen Huo ◽  
Guojie Wang

Marine, industrial, turboprop and turboshaft gas turbine engines use nonaxisymmetric exhaust volutes for flow diffusion and pressure recovery. These processes result in a three-dimensional complex turbulent flow in the exhaust volute. The flows in the axial turbine and nonaxisymmetric exhaust volute are closely coupled and inherently unsteady, and they have a great influence on the turbine and exhaust aerodynamic characteristics. Therefore, it is very necessary to carry out research on coupled axial turbine and nonaxisymmetric exhaust volute aerodynamics, so as to provide reference for the high-efficiency turbine-volute designs. This paper summarizes and analyzes the recent advances in the field of coupled axial turbine and nonaxisymmetric exhaust volute aerodynamics for turbomachinery. This review covers the following topics that are important for turbine and volute coupled designs: (1) flow and loss characteristics of nonaxisymmetric exhaust volutes, (2) flow interactions between axial turbine and nonaxisymmetric exhaust volute, (3) improvement of turbine and volute performance within spatial limitations and (4) research methods of coupled turbine and exhaust volute aerodynamics. The emphasis is placed on the turbine-volute interactions and performance improvement. We also present our own insights regarding the current research trends and the prospects for future developments.


Author(s):  
Mohanad Alayedi ◽  
Abdelhamid Cherifi ◽  
Abdelhak Ferhat Hamida ◽  
Boubakar Seddik Bouazza ◽  
Syed Alwee Aljunid

2019 ◽  
Vol 37 (4) ◽  
pp. 281-296 ◽  
Author(s):  
Zhiwei Wang ◽  
Minyoung Suh

In the current research, we aimed to investigate whether customized 3-D underwires improve bra performance. The first experiment was designed to study whether customized 3-D printed underwires provide significant benefits over conventional wires. Customized 3-D underwires were produced following individual breast root shapes and compared with conventional underwires through wear trials. According to the empirical data, pressure was significantly reduced with the customized underwire, and performance improvement was more evident with wearing sensations of support and comfort. In the second experiment, we varied the length of the customized underwires and observed how the length of underwires influenced bra performance. More pressure was found in the outer region of the longest underwires than the medium-length wires but support and comfort sensations did not have noticeable changes depending on the wire length. As illustrated in this research, advanced 3-D technologies could contribute to product engineering and customization in the apparel industry.


2014 ◽  
Vol 137 (1) ◽  
Author(s):  
Saurya Ranjan Ray ◽  
Mehrdad Zangeneh

A robust mixing plane method satisfying interface flux conservation, nonreflectivity and retaining interface flow variation; valid at all Mach numbers and applicable for any machine configuration is formulated and implemented in a vertex based finite volume solver for flow analysis and inverse design. The formulation is based on superposing perturbed flow variables derived from the three-dimensional (3D) characteristics obtained along the flow direction on the exchanged mixed out averaged quantities. The method is extended for low speed applications using low Mach number preconditioning. Subsequently, inverse design runs over a single stage transonic low pressure (LP) turbine configuration conducted at a fixed mass flow boundary condition and spanwise loading condition similar to the baseline generates optimized configurations providing performance improvement while achieving prespecified target meridional load distribution.


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