京都大学 / 0048 / 新制・課程博士 / 博士(工学) / 甲第21748号 / 工博第4565号 / 新制||工||1712(附属図書館) / 京都大学大学院工学研究科都市社会工学専攻 / (主査)教授 大津 宏康, 准教授 PIPATPONGSA Thirapong, 教授 三村 衛 / 学位規則第4条第1項該当 / Doctor of Philosophy (Engineering) / Kyoto University / DFAM

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MODCONV is a FORTRAN Computer code using the primitive form of the conservation equations for natural convection in porous medium to calculate the velocity and temperature distribution in the moderator of a typical CANDU reactor under normal and shut down operations, as well as postulated LOCA for which the rupture in the system is external to the core. Appropriate velocities are imposed at the boundary walls so that the free convection equations set can be used to model a mixed convection problem. Purely explicit, donor cell finite differencing scheme is used. A heat exchanger model using NTU method is also included to give a realistic inflow temperature for the moderator. The heat load distribution is calculated according to a channel power map, but can be redefined through input. / Thesis / Master of Engineering (MEngr)

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Clinical ultrasound imaging techniques can be greatly improved by the use of ultrasound contrast agents (UCAs). While microbubbles (MBs) without shell are unstable and cannot be used for practical applications,a shell produced from biocompatible polyvinylalcohol (PVA) significantly improves chemical versatility and stability. The oscillation characteristics of a UCA are strongly dependent on concentration, applied pressure and viscoelastic parameters of the shell. Modifications in the shell as incorporation of antibodies or targeted molecules affect the bubble oscillation and resonance frequency of the MB suspension. In this presented work a tool for systematic characterization of UCAs is developed. Linear acoustic behaviour of PVA shelled MBs is examined. The acoustic driving pressure is kept below 100 kPa. The MB concentration is 1·10^{6} ml^{-1}. Attenuation and phase velocity profiles of ultrasound waves propagating through the UCA are measured using six narrow-band single crystal transducers that cover a frequency range between 1 and 15 MHz. The oscillation of a single bubble is modeled as a linear oscillator adapting HOFF’s model suitable for allshell thicknesses. The suspension is modeled through superposition of single bubbles. Knowing all parameters the resonance frequency of a MB suspension can be predicted. The model is fitted to experimental data to determine the viscoelastic shell parameters. The shell thickness is challenging to determine exactly and assumed to be either proportional to the outer shell radius or constant. Assuming a proportional shell thickness the calculated resulting shell parameters were shear modulus G_s = 14.5 MPa, shear viscosity η_s = 0.322 Pa·s and shell thickness d_s = 16 % of the outer radius. When instead assuming a constant shell thickness the determined parameters were in similar order of magnitude. Resonance frequency of the suspension was determined to 11.6 MHz. The developed tool can be used to characterize MBs with a modified shell independently of shell thickness and to predict resonance frequency of gas or air filled UCAs with known shell parameters.

Air velocity and fuel concentration data have been collected throughout the flow fields of two gas turbine mixers in an effort to better understand the mixing of fuel and air in gas turbine mixers. The two gas turbine mixers consisted of an annular flow profile and incorporated swirl vanes to produce a swirling flow to promote fuel/air mixing. The fuel was injected into the bulk flow from the pressure side of the swirl vanes. The first mixer had a swirl angle of 45°, while the second had a swirl angle of 55°. In order to examine the effect of the swirl angle on the mixing of fuel and air as the flow progressed through gas turbine mixers, axial and tangential air velocity data was taken using a laser Doppler velocimeter (LDV). Also, fuel concentration data was taken separately using a hydrocarbon concentration probe with methane diluted with air as the fuel. The data were taken at varying axial and varying angular locations in an effort to capture the spatial development of the fuel and velocity profiles. The spectra of the data were analyzed as well in an effort to understand the turbulence of the flow. It was found that the 55° swirler exhibited smaller variations in both velocity and fuel concentration values and that the fuel reached a uniform concentration at axial locations further upstream in the 55° degree mixer than in the 45° mixer. The RMS values of the velocity, which were influenced by the swirl vanes, were higher in the 55° mixer and likely contributed to the better mixing performance of the 55° mixer. The fuel concentration spectrum data showed that the spectra of the two mixers were similar, and that the fluctuations in fuel concentration due to flow emanating from the swirl vanes were seen throughout the length of the two mixers.

This dissertation will investigate electron beam induced current (EBIC) for determining semiconductor material and device parameters. While previous experimental work on PN junction delineation using EBIC with the scanning electron microscope has resulted in resolution to approximately 10 nm, theoretical study shows the potential use of EBIC for higher resolution (nanometer) PN junction and FET channel length delineation using the transmission electron microscope. Theoretical arguments using computer simulations of electron beam generation volume, collection probability and EBIC were performed and are presented for the purpose of determining EBIC use in a 300 keV transmission electron microscope (TEM) for PN junction depth determination. Measured results indicate that by measuring thin semiconductor samples with high surface recombination velocity and by using a narrow, high-energy electron beam in the STEM mode of a transmission electron microscope, nanometer resolution may be possible. The practical and experimental limits of beam energy and semiconducting material thermal damage will be discussed.