An integral equation based numerical solution for nanoparticles illuminated with collimated and focused light

To address the large number of parameters involved in nanooptical problems, a more efficient computational method is necessary. An integral equation based numerical solution is developed when the particles are illuminated with collimated and focused incident beams. The solution procedure uses the method of weighted residuals, in which the integral equation is reduced to a matrix equation and then solved for the unknown electric field distribution. In the solution procedure, the effects of the surrounding medium and boundaries are taken into account using a Green’s function formulation. Therefore, there is no additional error due to artificial boundary conditions unlike differential equation based techniques, such as finite difference time domain and finite element method. In this formulation, only the scattering nano-particle is discretized. Such an approach results in a lesser number of unknowns in the resulting matrix equation. The results are compared to the analytical Mie series solution for spherical particles, as well as to the finite element method for rectangular metallic particles. The Richards-Wolf vector field equations are combined with the integral equation based formulation to model the interaction of nanoparticles with linearly and radially polarized incident focused beams

Linear laser diode arrays for improvement in optical disk recording for space stations

The design and fabrication of individually addressable laser diode arrays for high performance magneto-optic recording systems are presented. Ten diode arrays with 30 mW cW light output, linear light vs. current characteristics and single longitudinal mode spectrum were fabricated using channel substrate planar (CSP) structures. Preliminary results on the inverse CSP structure, whose fabrication is less critically dependent on device parameters than the CSP, are also presented. The impact of systems parameters and requirements, in particular, the effect of feedback on laser design is assessed, and techniques to reduce feedback or minimize its effect on systems performance, including mode-stabilized structures, are evaluated

Location of pattern-disturbing structures in the vicinity of an antenna Final report, Jun. 5, 1963 - Sep. 15, 1966

Location of radiation pattern disturbing structures in vicinity of satellite antenn

A nested hybridizable discontinuous Galerkin method for computing second-harmonic generation in three-dimensional metallic nanostructures

In this paper, we develop a nested hybridizable discontinuous Galerkin (HDG) method to numerically solve the Maxwell's equations coupled with the hydrodynamic model for the conduction-band electrons in metals. By means of a static condensation to eliminate the degrees of freedom of the approximate solution defined in the elements, the HDG method yields a linear system in terms of the degrees of freedom of the approximate trace defined on the element boundaries. Furthermore, we propose to reorder these degrees of freedom so that the linear system accommodates a second static condensation to eliminate a large portion of the degrees of freedom of the approximate trace, thereby yielding a much smaller linear system. For the particular metallic structures considered in this paper, the resulting linear system obtained by means of nested static condensations is a block tridiagonal system, which can be solved efficiently. We apply the nested HDG method to compute the second harmonic generation (SHG) on a triangular coaxial periodic nanogap structure. This nonlinear optics phenomenon features rapid field variations and extreme boundary-layer structures that span multiple length scales. Numerical results show that the ability to identify structures which exhibit resonances at $\omega$ and $2\omega$ is paramount to excite the second harmonic response.Comment: 31 pages, 7 figure

Fine Scale Simulation of Fractured Reservoirs: Applications and Comparison

Imperial Users onl

Employment of fine grain emulsions in aerial photography

Thesis (M.A.)--Boston UniversityThe general problem of this work is to determine the extent to which fine grain emulsions can be employed in aerial photography, with specific application to miniaturization. In such a study, the following factors become important: reduced scale, limited coverage, processing and enlargement technique, loss of speed through the use of finer grained emulsions. In this investigation, laboratory tests were made to study these factors. These tests were to study the relative performance of several systems (lens plus film) and to investigate methods of increasing the speed of fine grain emulsions without seriously affecting the grain size. Finally, flight tests were made to verify the results indicated by the laboratory tests. Miniaturization is defined as the use of 35 mm and 70 mm cameras in aerial photography. It has become important during the last few years because of increasing space limitations inside the aircraft. Besides the obvious saving in weight and space both in the plane and in the processing and storage of the photographs, the miniature camera has other advantages. Because of the short focal length of most miniature camera lenses, it is possible to construct a fast lens of high quality, reducing the exposure time, the time in which vibration and image motion can affect the image, and hence the degree of stabilization which the camera must maintain. On the negative side, the reduced scale necessitates the enlargement of all photographs before they can be used. This increases the relative effects of the grain of the emulsion and uneven development, as well as introducing an additional variable in the photographic process, enlargement. The camera used in this work was an Exacta VX, 35 mm, with an f/1.5 75 mm Biotar lens. This lens was chosen largely because of its wide aperture, but this could not be used under practical conditions because of serious vignetting at f/1.5. The film chosen for a standard of comparison was Aerographic Super XX with a standard development in D-19 to a gamma of 1.6 to 1.7. At the other extreme, with respect to speed and grain size, Microfile was chosen. This film is easily developed to gammas of 3 and 4, but for the purpose of this work, it was developed in D-23, diluted 1:1, to a gamma similar to Aero XX. As a compromise in speedand grain size, a German film, Perutz Pergrano, was chosen. This film has an ASA exposure index of 12 and medium grain. DevHopment was in D-19 to a gamma of 1.35. Because of the inherent low contrast of this film, the gammas of Aero XX and Microfile could not be attained. Extensive tests were run on the f/1.5 75 mm Biotar lens with all three types of film, low and high contrast resolution tar gets, and with and without a yellow filter. From the results of these tests, the area weighted average resolution, or AWAR, was calculated for each aperture-film combination. Then, under the conditions which would be used for the flight tests, the minimum shutter speed was calculated which would prevent the resolution from dropping below the AWAR because of image motion caused by the movement of the airplane with respect to the ground. Next a table was prepared showing the predicted maximum resolution obtained under varying illumination conditions, taking into account the effect on resolution of increasing the aperture or the exposure time. The results of this table, which were confirmed by the flight tests, were: 1) Microfile must be exposed at too wide an aperture to obtain any benefit from its small grain size, 2) Microfile which has been latensified by post-exposure to light (see below) produces the best results under good illumination, but also must be exposed at too wide an aperture under decreased illumination, and 3) Perutz Pergrano produces better results than Aero XX over a range of illumination of 32:1. Results of resolution tests on 2 tele-photo lenses were used to compare these lenses with the 75 mm Biotar. The best lens was the f/5.5 180 mm Tele-Xenar lens, which had a performance, in terms of ground detail resolved, equal to the Biotar lens. This result was verified by flight tests with the two lenses, and hence the use of tele-photo lenses is warranted in high altitude photography, where the decreased coverage can be overlooked. From previously unpublished data on four 50 mm lenses and one 58 mm lens, the AWAR was calculated and the results plotted and analyzed. The best of the 50 mm lenses was an f/1.5 Angenieux. When the f/2 58 mm Zeiss Biotar lens and the Angenieux lens were reduced to a common level by removing the scale, the two lenses were of approximately the same performance. Of the methods of increasing film speed before exposure (hypersensitization) and after exposure but before development (latensification), the best method tested was post-exposure to a dim light. For this purpose, a darkroom safelight with a yellow filter and reduced applied voltage was exposed to Microfile for 30 minutes at a distance of 18 feet. An increase in speed of 400% was obtained over its normal speed of 1 (because of underdevelopment). Equal treatment before exposure gave an increase of speed of only 15%. When the method was used under actual photographic conditions, post-exposure to light gave a somewhat greater increase in speed than 400%. Resolution tests showed a drop in resolution of 10%, but the resolving power was still greater than that of Perutz Pergrano. Other methods of hypersensitization and latensification which were tested were NaCl and Borax in solution, Mercury vapor, and combinations of ammonia and alcohol in solution. The maximum increase obtained from these methods was 50%. The increase in speed obtained on Microfile through post-exposure to light has brought the emulsion sensitivity to a minimum level for best results under normal illumination. Hence the grain size is also approximately at a minimum and this film, used in this way, provides maximum definition in terms of detail resolved. Then on the basis of X 8 enlargements of 35 mm negatives on Microfile which had been latensified in this manner, the conclusion is reached that 35 mm cameras may not be used as an unqualified substitute for aerial cameras. However they may prove valuable in some types of reconnaissance photography. The enlargement to 4 diameters of negatives on Microfile latensified and Perutz Pergrano produces good results. Since this is the amount of enlargement necessary to bring 70 mm negatives to approximately the size of a 9 X 9 inch photograph, 70 mm cameras may be used in connection with these films and others of similar characteristics to replace aerial cameras for many purposes. The major exceptions are in the production of photographs for use in surveying and photogammetric work, which require maximum definition at all levels of magnification. Aero XX is not recommended for use with miniature cameras in general because the lenses of these cameras are capable of higher resolution than this film can accomodate. At a drop in emulsion speled of 8 I from Aero XX, Perutz Pergrano may be used over an illumination range of 32:1, and still produce better results than would be obtained with Aero XX. This range might be extended even further through the use of hypersensitization and latensification methods, without seriously affecting the grain size of the emulsion. In conclusion, then, fine grain emulsions (i.e. finer grained than Aero XX) in connection with 70 mm cameras may be used to produce results satisfactory for many purposes in Aerial Photography. I would like to thank the following people for their contributions to the work involved in this thesis: Mr. Hutson Howell, Dr. F. Dow Smith, Mr. William Drumm, Mr. Hadrian Lechner, the staff of the Boston University Physical Research Laboratory, and Mrs. Jere Sanborn

Operations of and Future Plans for the Pierre Auger Observatory

Technical reports on operations and features of the Pierre Auger Observatory, including ongoing and planned enhancements and the status of the future northern hemisphere portion of the Observatory. Contributions to the 31st International Cosmic Ray Conference, Lodz, Poland, July 2009.Comment: Contributions to the 31st ICRC, Lodz, Poland, July 200

The Sunrise Mission

The first science flight of the balloon-borne \Sunrise telescope took place in June 2009 from ESRANGE (near Kiruna/Sweden) to Somerset Island in northern Canada. We describe the scientific aims and mission concept of the project and give an overview and a description of the various hardware components: the 1-m main telescope with its postfocus science instruments (the UV filter imager SuFI and the imaging vector magnetograph IMaX) and support instruments (image stabilizing and light distribution system ISLiD and correlating wavefront sensor CWS), the optomechanical support structure and the instrument mounting concept, the gondola structure and the power, pointing, and telemetry systems, and the general electronics architecture. We also explain the optimization of the structural and thermal design of the complete payload. The preparations for the science flight are described, including AIV and ground calibration of the instruments. The course of events during the science flight is outlined, up to the recovery activities. Finally, the in-flight performance of the instrumentation is briefly summarized.Comment: 35 pages, 17 figure