Three‐dimensional heat‐flow effects in photoacoustic spectroscopy of solids

1979 ◽  
Vol 35 (1) ◽  
pp. 43-45 ◽  
Author(s):  
R. S. Quimby ◽  
W. M. Yen
2006 ◽  
Vol 129 (2) ◽  
pp. 212-220 ◽  
Author(s):  
Giovanna Barigozzi ◽  
Giuseppe Franchini ◽  
Antonio Perdichizzi

The present paper reports on the aerothermal performance of a nozzle vane cascade, with film-cooled end walls. The coolant is injected through four rows of cylindrical holes with conical expanded exits. Two end-wall geometries with different area ratios have been compared. Tests have been carried out at low speed (M=0.2), with coolant to mainstream mass flow ratio varied in the range 0.5–2.5%. Secondary flow assessment has been performed through three-dimensional (3D) aerodynamic measurements, by means of a miniaturized five-hole probe. Adiabatic effectiveness distributions have been determined by using the wide-band thermochromic liquid crystals technique. For both configurations and for all the blowing conditions, the coolant share among the four rows has been determined. The aerothermal performances of the cooled vane have been analyzed on the basis of secondary flow effects and laterally averaged effectiveness distributions; this analysis was carried out for different coolant mass flow ratios. It was found that the smaller area ratio provides better results in terms of 3D losses and secondary flow effects; the reason is that the higher momentum of the coolant flow is going to better reduce the secondary flow development. The increase of the fan-shaped hole area ratio gives rise to a better coolant lateral spreading, but appreciable improvements of the adiabatic effectiveness were detected only in some regions and for large injection rates.


1999 ◽  
Vol 121 (1) ◽  
pp. 198-204 ◽  
Author(s):  
Chao-Tsung Hsiao ◽  
Laura L. Pauley

The Rayleigh-Plesset bubble dynamics equation coupled with the bubble motion equation developed by Johnson and Hsieh was applied to study the real flow effects on the prediction of cavitation inception in tip vortex flows. A three-dimensional steady-state tip vortex flow obtained from a Reynolds-Averaged Navier-Stokes computation was used as a prescribed flow field through which the bubble was passively convected. A “window of opportunity” through which a candidate bubble must pass in order to be drawn into the tip-vortex core and cavitate was determined for different initial bubble sizes. It was found that bubbles with larger initial size can be entrained into the tip-vortex core from a larger window size and also had a higher cavitation inception number.


1999 ◽  
Vol 43 (03) ◽  
pp. 180-193 ◽  
Author(s):  
Odd M. Faltinsen

Water entry of a hull with wedge-shaped cross sections is analyzed. The stiffened platings between two transverse girders on each side of the keel are separately modeled. Orthotropic plate theory is used. The effect of structural vibrations on the fluid flow is incorporated by solving the two-dimensional Laplace equation in the cross-sectional fluid domain by a generalized Wagner's theory. The coupling with the plate theory provides three-dimensional flow effects. The theory is validated by comparison with full-scale experiments and drop tests. The importance of global ship accelerations is pointed out. Hydrodynamic and structural error sources are discussed. Systematic studies on the importance of hydroelasticity as a function of deadrise angle and impact velocity are presented. This can be related to the ratio between the wetting time of the structure and the greatest wet natural period of the stiffened plating. This ratio is proportional to the deadrise angle and inversely proportional to the impact velocity. A small ratio-means that hydroelasticity is important and a large ratio means that hydroelasticity is not important.


Water ◽  
2020 ◽  
Vol 12 (3) ◽  
pp. 638
Author(s):  
Zhenzhou Zhu ◽  
Xiaodong Lei ◽  
Nengxiong Xu ◽  
Dongyue Shao ◽  
Xingyu Jiang ◽  
...  

With the increasing demand for energy and the growing concern for atmospheric pollution in Beijing, China, the exploitation and utilization of geothermal resources are becoming more desirable. The study combined three-dimensional geological modeling with geothermal field analysis to make clear the potential and distribution of geothermal resources in the northwest of the Beijing plain, which could provide a scientific basis for rational utilization in the study area. Based on the analysis of the geological data and geothermal conditions, we created a 3D geological model of the study area, and then added isothermal surfaces into the model and analyzed the heat flow to enhance the understanding of the present geothermal field. After that, the volumes of different temperature intervals of heat reservoirs were calculated accurately and automatically by the integration of the model and the isothermal surfaces. Finally, the geothermal reserves were calculated by the improved volumetric method, and the distribution of resources was analyzed comprehensively. The results showed that, in the study area, the heat flow values ranged from 49 to 99 mW m−2, and the average elevations of 25 °C, 40 °C, and 60 °C isothermal surfaces were at −415 m, −1282 m, and −2613 m, respectively. The geothermal reserves were 5.42 × 1019 J and the volume of the heat reservoir was 4.88 × 1011 m3. The geothermal resources of the study area had good potential and could support local green development.


1998 ◽  
Vol 25 (1) ◽  
pp. 15-24 ◽  
Author(s):  
Eui Soo Yoon ◽  
Byung Nam Kim ◽  
Myung Kyoon Chung

1974 ◽  
Vol 14 (06) ◽  
pp. 573-592 ◽  
Author(s):  
K.H. Coats ◽  
W.D. George ◽  
Chieh Chu ◽  
B.E. Marcum

Coats, K.H., Member SPE-AIME, Intercomp Resource Development and Engineering, Inc., Houston, Texas George, W.D., Chu, Chieh, Member SPE-AIME, Getty Oil Co., Houston, Tx. Marcum, B.E., Member SPE-AIME, Getty Oil Co., Los Angeles, Calif. Abstract This paper describes a three-dimensional model for numerical simulation of steam injection processes. The model describes three-phase flow processes. The model describes three-phase flow of water, oil, and steam and heat flow in the reservoir and overburden. The method of solution simultaneously solves for the mass and energy balances and eliminates the need for iterating on the mass transfer (condensation) term.Laboratory data are reported for steamfloods of 5,780-cp oil in a 1/4 five-spot sand pack exhibiting three-dimensional flow effects. These experiments provide additional data for checking accuracy and provide additional data for checking accuracy and assumptions in numerical models. Comparisons of model results with several sets of experimental data indicate a need to account for effects of temperature on relative permeability. Calculated areal conformance of a steamflood in a confined five-spot depends strongly upon the alignment of the x-y grid axes relative to the diagonal joining injection and production wells. It has not been determined which, if either, of the two grid types yields the correct areal conformance.Model calculations indicate that steamflood pressure level strongly affects oil recovery. pressure level strongly affects oil recovery. Calculated oil recovery increases with decreasing pressure level. An example application illustrates pressure level. An example application illustrates the ability of the model formulation to efficiently simulate the single-well, cyclic steam stimulation problem. problem Introduction The literature includes many papers treating various aspects of oil recovery by steamflooding, hot waterflooding, and steam stimulation. The papers present laboratory experimental data, field papers present laboratory experimental data, field performance results, models for calculating fluid performance results, models for calculating fluid and heat flow, and experimental data regarding effects of temperature on relative permeability. The ultimate goal of all this work is a reliable engineering analysis to estimate oil recovery for a given mode of operation and to determine alternative operating conditions to maximize oil recovery.Toward that end, our study proposed to develop and validate an efficient, three-dimensional numerical model for simulating steamflooding, hot waterflooding, and steam stimulation. Laboratory steamflood experiments were conducted to provide additional data for validation. Desired model specifications included three-dimensional capability and greater efficiency than reported for previous models. Omitted from the specifications were temperature-dependent relative permeability and steam distillation effects.This paper describes the main features of the three-dimensional, steamflood model developed. Those features include a new method of solution that includes implicit water transmissibilities, that simultaneously solves for mass and energy balances, and that eliminates the need for iteration on the condensation term. Laboratory data are reported for steamfloods in a 1/4 five-spot model exhibiting three-dimensional flow effects. Numerical model applications described include comparisons with experimental data, a representative field-scale steamflood, and a cyclic steam stimulation example. REVIEW OF PREVIOUS WORK Early efforts in mathematical modeling of thermal methods concentrated on simulation of the heat flow and heat loss. Gottfried, in his analysis of in-situ combustion, initiated a series of models that solve fluid mass balances along with the energy balance. Davidson et al. presented an analysis for well performance during cyclic steam injection. Spillette and Nielsen treated hot waterflooding in two dimensions. Shutler described three-phase models for linears and two-dimensional steamflooding, and Abdalla and Coats treated a two-dimensional steamflood model using the IMPES method of solution. SPEJ P. 573


Three-dimensional (3D) linear stability properties are considered for steady and unsteady 2D or 3D boundary layers with significant non-parallelism present. Two main examples of such non-parallel flows whose stability is of interest are, firstly, steady motion, over roughness elements, in cross flow, or in large-scale separation and, secondly, unsteady 2D Tollmien-Schlichting (TS) motion, with its associated question of secondary instabilities. A high-frequency stability analysis is presented here. It is found that, for 2DTS or steady boundary layers, there is a swing in the direction of maximum TS spatial growth rate, from 0° for parallel flow towards 64.68° away from the free-stream direction, as the nonparallel flow effects increase. These effects then depend principally on, and indeed are proportional to, the local slope of the boundary-layer displacement. Cross flow can also have a profound impact on TS instabilities. Further implications for higher-amplitude and/or fasterscale disturbances, their secondary instability, and nonlinear interactions, are also discussed.


1989 ◽  
Vol 172 ◽  
Author(s):  
J. L. Adam ◽  
C. Ortiz ◽  
J. R. Salem ◽  
X. H. Zhang

AbstractWe have studied the effect of laser irradiation on Te-Se-Br thin films. The major effects were found to be dominated by changes in composition because of the complete loss of Br and variable loss of Se. These losses are measured by EIDS and are reasonable in view of the temperatures obtained from a heat flow calculation. The remaining Te-Se material can be made crystalline under specific conditions of laser pulse length and laser power (which determine the cooling rate). We have been able to establish that the crystallization starts with surface filamentary growth exhibiting fractal network formation. With higher laser energy it tends to coalesce to form three dimensional crystals.


Author(s):  
L. E. Wood ◽  
R. R. Jones ◽  
O. J. Pountney ◽  
J. A. Scobie ◽  
D. A. S. Rees ◽  
...  

Abstract The mainstream, or primary, flow in a gas turbine annulus is characteristically two-dimensional over the mid-span region of the blading, where the radial flow is almost negligible. Contrastingly, the flow in the endwall and tip regions of the blading is highly three-dimensional, characterised by boundary layer effects, secondary flow features and interaction with cooling flows. Engine designers employ geometric contouring of the endwall region in order to reduce secondary flow effects and subsequently minimise their contribution to aerodynamic loss. Such is the geometric variation of vane and blade profiles — which has become a proprietary art form — the specification of an effective endwall geometry is equally unique to each blade-row. Endwall design methods, which are often directly coupled to aerodynamic optimisers, are widely developed to assist with the generation of contoured surfaces. Most of these construction methods are limited to the blade-row under investigation, while few demonstrate the controllability required to offer a universal platform for endwall design. This paper presents a Geometry Generation Framework (GGF) for the generation of contoured endwalls. The framework employs an adaptable meshing strategy, capable of being applied to any vane or blade, and a versatile function-based approach to defining the endwall shape. The flexibility of this novel approach is demonstrated by recreating a selection of endwalls from the literature, which were selected for their wide-range of contouring approaches.


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