Optimization and synchronization of programmable quantum communication channels

Quantum applications transmit and receive data through quantum and classical communication channels. Channel capacity, the distance and the photon path between transmitting and receiving parties and the speed of the computation links play an essential role in timely synchronization and delivery of information using classical and quantum channels. In this study, we analyze and optimize the parameters of the communication channels needed for the quantum application to successfully operate. We also develop algorithms for synchronizing data delivery on classical and quantum channels.Comment: 7 pages, 2 figure

Information retrieval system

Generalized information storage and retrieval system capable of generating and maintaining a file, gathering statistics, sorting output, and generating final reports for output is reviewed. File generation and file maintenance programs written for the system are general purpose routines

Effect of Boundary Layer Thickness and Entropy Layer on Boundary Layer Combustion

This project investigates the possibilities of scramjet combustor performance enhancement by reducing the skin friction through boundary layer combustion. Experiments were conducted in the T4 Stalker tube to investigate the influence of boundary layer thickness and entropy layers on the ignition of a hydrogen air mixture near the wall of a constant area duct. The hydrogen was injected tangentially from a slot of annular cross section after an “injector” of constant area captured flow from a Mach 4 nozzle. Injectors of two different lengths and nose radii were employed to vary the thickness of the boundary layer at the injection location as well as the temperature of the gas near the walls and within the entropy layer created by the leading edge shocks of blunted leading edges. Results are presented of CFD simulations of the injector as well as experimentally measured pressure coefficient profiles along the combustor wall. It is shown that a thicker boundary layer will promote combustion but that heating the gas near the walls through a leading edge shock is more effective for ignition. However, the shocks generated by the leading edge may also influence the core flow of the constant area combustor and possibly cause some main stream mixing

Scramjets and Shock Tunnels: The Queensland Experience

This article reports on the use of a shock tunnel to study the operation of scramjet powered configurations at sub-orbital velocities above 2 km/s. Thrust, as given by a net thrust equation, is used as a figure of merit throughout the study. After a short description of the shock tunnel used and its operating characteristics, experiments on the combustion release of heat in a constant area duct with hydrogen fuel are reviewed. The interaction between heat release in the combustion wake and the walls of the duct produced pressure distributions which followed a binary scaling law, and indicated that the theoretically expected heat release could be realized in practice, albeit with high pressure or long combustion ducts. This heat release, combined with attainable thrust nozzle characteristics and a modest level of configuration drag, indicated that positive thrust levels could be obtained well into the sub-orbital range of velocities. Development of a stress wave force balance for use in shock tunnels allowed the net thrust generated to be measured for integrated scramjet configurations and, although the combination of model size and shock tunnel operating pressure prevented complete combustion of hydrogen, the cruise condition of zero net thrust was achieved at 2.5 km/s with one configuration, while net thrust was produced with another configuration using an ignition promoter in hydrogen fuel. Nevertheless, the combination of boundary layer separation induced inlet choking and limited operating pressure levels prevented realization of the thrust potential of the fuel. This problem may be alleviated by recent increases in the shock tunnel operating pressures, and by promising research involving inlet injection of the fuel. Research on the drag component of the net thrust equation resulted from the development of a fast response skin friction gauge. It was found that existing theories of turbulent boundary skin friction predicted the skin friction when combustion of hydrogen occurred outside the boundary layer, but combustion within the boundary layer dramatically reduced the skin friction. Finally, for the first time in the world, supersonic combustion was produced in a free flight experiment. This experiment validated shock tunnel results at stagnation enthalpies near 3 MJ/k

Comparison of drag measurements of two axisymmetric scramjet models at Mach 6

Axial forces on quasi-axisymmetric scramjet models designed for operation at Mach 6 and Mach 8 were measured in the T4 Stalker tube at The University of Queensland using a single component stress wave force balance. A Mach 6 nozzle was used. The nozzle supply enthalpy was varied from 3 to 9 MJ/kg and the nozzle supply pressure from 35 to 45 MPa. As the conditions varied, the Mach number varied from 5.7 to 6.7. For both test models, the drag coefficients decreased with increasing Mach number. However, significant differences between the models were not observed over a range of free stream Mach numbers. A theoretical procedure to calculate the drag coefficient was found to give good agreement with experiments when appropriate account was taken of flow spillage at the intake

Using the 'myVolcano' mobile phone app for citizen science in St. Vincent and the Grenadines : a pilot study

The British Geological Survey (BGS) has been working with Caribbean partners on the role of citizen science in increasing resilience to natural hazards. The work has largely focused on the potential use of the myVolcano smartphone app, which was developed by the BGS following the 2010 Eyafjallajökull and 2011 Grímsvötn eruptions in Iceland. During these eruptions the BGS asked the UK public to collect particle samples, subsequently analysing these for ash presence to map the distribution of ash fallout across the UK. These requests led to the development of the myVolcano app, which was designed to capture transboundary and distal observations of volcanic ash and emissions. The observations are made visible to other users via an interactive map built into the app. The map interface has global coverage and the data collection methods (free-text descriptions and photographs) are such that information about any natural hazard, anywhere in the world, can be captured. In 2015, BGS carried out an ESRC-DfID-NERC funded scoping study in collaboration with the University of the West Indies’ Seismic Research Centre (UWI SRC), to test the potential use of the app in environments affected by proximal volcanic hazards. The study focused on St. Vincent and the Grenadines and investigated the potential for capturing a wider variety of observations for use by the public, operational scientists and civil protection. The study, which included a combination of desk study and remote interviews, highlighted the potential for, and challenges of, using such an app for increasing resilience to natural hazards and the need for a follow-up study in St Vincent. In March 2017, a workshop and school activities were held in St. Vincent to collect feedback from potential users of myVolcano, hereafter referred to as the pilot study. Workshop participants came from across government, monitoring agencies, emergency response and telecommunications. As part of the workshop, a multi-hazard scenario was ‘played out’ to stimulate discussions on the usability of the app, data gathering and processing, and participants’ use of existing citizen science applications. Discussions developed around data validation and quality assurance, data sharing and presentation, local management of data by nominated scientists (e.g. to facilitate real-time decision making) and the associated need for a locally appropriate app (i.e. no one size fits all). This last point is particularly significant when considering the utility of an app in several countries – the user interface, at least, requires specific tailoring to the country’s needs. Using this feedback, the BGS Official Development Assistance (ODA) programme is currently funding collaborations with Caribbean partners in order to modify the app to meet the local requirements, including widening the multi-hazard application and enhancing two-way information sharing. Of particular importance is how best to share critical information with those making observations and how to make observations available to decision-makers and monitoring scientists in real-time (e.g. through local management of the app)

Exact solutions to the focusing nonlinear Schrodinger equation

A method is given to construct globally analytic (in space and time) exact solutions to the focusing cubic nonlinear Schrodinger equation on the line. An explicit formula and its equivalents are presented to express such exact solutions in a compact form in terms of matrix exponentials. Such exact solutions can alternatively be written explicitly as algebraic combinations of exponential, trigonometric, and polynomial functions of the spatial and temporal coordinates.Comment: 60 pages, 18 figure

Spin fluctuations in the quasi-two dimensional Heisenberg ferromagnet GdI_2 studied by Electron Spin Resonance

The spin dynamics of GdI_2 have been investigated by ESR spectroscopy. The temperature dependences of the resonance field and ESR intensity are well described by the model for the spin susceptibility proposed by Eremin et al. [Phys. Rev. B 64, 064425 (2001)]. The temperature dependence of the resonance linewidth shows a maximum similar to the electrical resistance and is discussed in terms of scattering processes between conduction electrons and localized spins.Comment: to be published in PR