135,491 research outputs found
The specific heat jump at the superconducting transition and the quantum critical nature of the normal state of Pnictide superconductors
Recently it was discovered that the jump in the specific heat at the
superconducting transition in pnictide superconductors is proportional to the
superconducting transition temperature to the third power, with the
superconducting transition temperature varying from 2 to 25 Kelvin including
underdoped and overdoped cases. Relying on standard scaling notions for the
thermodynamics of strongly interacting quantum critical states, it is pointed
out that this behavior is consistent with a normal state that is a quantum
critical metal undergoing a pairing instability.Comment: 4 pages 1 figur
The origin of phase in the interference of Bose-Einstein condensates
We consider the interference of two overlapping ideal Bose-Einstein
condensates. The usual description of this phenomenon involves the introduction
of a so-called condensate wave functions having a definite phase. We
investigate the origin of this phase and the theoretical basis of treating
interference. It is possible to construct a phase state, for which the particle
number is uncertain, but phase is known. However, how one would prepare such a
state before an experiment is not obvious. We show that a phase can also arise
from experiments using condensates in Fock states, that is, having known
particle numbers. Analysis of measurements in such states also gives us a
prescription for preparing phase states. The connection of this procedure to
questions of ``spontaneously broken gauge symmetry'' and to ``hidden
variables'' is mentioned.Comment: 22 pages 4 figure
Research pressure instrumentation for NASA Space Shuttle main engine, modification no. 5
The objective of the research project described is to define and demonstrate methods to advance the state of the art of pressure sensors for the space shuttle main engine (SSME). Silicon piezoresistive technology was utilized in completing tasks: generation and testing of three transducer design concepts for solid state applications; silicon resistor characterization at cryogenic temperatures; experimental chip mounting characterization; frequency response optimization and prototype design and fabrication. Excellent silicon sensor performance was demonstrated at liquid nitrogen temperature. A silicon resistor ion implant dose was customized for SSME temperature requirements. A basic acoustic modeling software program was developed as a design tool to evaluate frequency response characteristics
Electronic structure of strongly correlated d-wave superconductors
We study the electronic structure of a strongly correlated d-wave
superconducting state. Combining a renormalized mean field theory with direct
calculation of matrix elements, we obtain explicit analytical results for the
nodal Fermi velocity, v_F, the Fermi wave vector, k_F, and the momentum
distribution, n_k, as a function of hole doping in a Gutzwiller projected
d-wave superconductor. We calculate the energy dispersion, E_k, and spectral
weight of the Gutzwiller-Bogoliubov quasiparticles, and find that the spectral
weight associated with the quasiparticle excitation at the antinodal point
shows a non monotonic behavior as a function of doping. Results are compared to
angle resolved photoemission spectroscopy (ARPES) of the high temperature
superconductors.Comment: final version, comparison to experiments added, 4+ pages, 4 figure
Supporting development for the preliminary design of an intermediate water recovery system
Supporting development of experimental design for water recovery syste
Generic Connectivity-Based CGRA Mapping via Integer Linear Programming
Coarse-grained reconfigurable architectures (CGRAs) are programmable logic
devices with large coarse-grained ALU-like logic blocks, and multi-bit
datapath-style routing. CGRAs often have relatively restricted data routing
networks, so they attract CAD mapping tools that use exact methods, such as
Integer Linear Programming (ILP). However, tools that target general
architectures must use large constraint systems to fully describe an
architecture's flexibility, resulting in lengthy run-times. In this paper, we
propose to derive connectivity information from an otherwise generic device
model, and use this to create simpler ILPs, which we combine in an iterative
schedule and retain most of the exactness of a fully-generic ILP approach. This
new approach has a speed-up geometric mean of 5.88x when considering benchmarks
that do not hit a time-limit of 7.5 hours on the fully-generic ILP, and 37.6x
otherwise. This was measured using the set of benchmarks used to originally
evaluate the fully-generic approach and several more benchmarks representing
computation tasks, over three different CGRA architectures. All run-times of
the new approach are less than 20 minutes, with 90th percentile time of 410
seconds. The proposed mapping techniques are integrated into, and evaluated
using the open-source CGRA-ME architecture modelling and exploration framework.Comment: 8 pages of content; 8 figures; 3 tables; to appear in FCCM 2019; Uses
the CGRA-ME framework at http://cgra-me.ece.utoronto.ca
Research pressure instrumentation for NASA Space Shuttle main engine, modification no. 5
The purpose of Modification No. 5 of this contract is to expand the scope of work (Task C) of this research study effort to develop pressure instrumentation for the SSME. The objective of this contract (Task C) is to direct Honeywell's Solid State Electronics Division's (SSED) extensive experience and expertise in solid state sensor technology to develop prototype pressure transducers which are targeted to meet the SSME performance design goals and to fabricate, test and deliver a total of 10 prototype units. SSED's basic approach is to effectively utilize the many advantages of silicon piezoresistive strain sensing technology to achieve the objectives of advanced state-of-the-art pressure sensors in terms of reliability, accuracy and ease of manufacture. More specifically, integration of multiple functions on a single chip is the key attribute of this technology which will be exploited during this research study
Research pressure instrumentation for NASA space shuttle main engine
The breadboard feasibility model of a silicon piezoresistive pressure transducer suitable for space shuttle main engine (SSME) applications was demonstrated. The development of pressure instrumentation for the SSME was examined. The objective is to develop prototype pressure transducers which are targeted to meet the SSME performance design goals and to fabricate, test and deliver a total of 10 prototype units. Effective utilization of the many advantages of silicon piezoresistive strain sensing technology to achieve the objectives of advanced state-of-the-art pressure sensors for reliability, accuracy and ease of manufacture is analyzed. Integration of multiple functions on a single chip is the key attribute of the technology
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