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Thermal effect curling of concrete pavements on U.S. 23 test road (DEL 23-17.28Goldsberry, Benjamin M. January 1998 (has links)
Thesis (M.S.)--Ohio University, June, 1998. / Title from PDF t.p.
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A new theory of the spalling of fireclay products with relation to thermal expansionStone, Robert LeGrande. January 1934 (has links) (PDF)
Thesis (B.S.)--University of Missouri, School of Mines and Metallurgy, 1934. / The entire thesis text is included in file. Typescript. Title from title screen of thesis/dissertation PDF file (viewed June 2, 2010) Includes bibliographical references (p. 53-54).
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Investigation of dynamic temperature response of pressure transducersIyer, Ramalingam Subramanyam, January 1970 (has links)
Thesis (M.S.)--University of Wisconsin--Madison, 1970. / eContent provider-neutral record in process. Description based on print version record. Includes bibliographical references.
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Thermal buckling of laminated composite platesSimelane, Philemon Sphiwe January 1998 (has links)
Thesis (MTech (Mechanical Engineering))--Peninsula Technikon, 1998 / However, studies were also conducted for the buckling of composite laminates
involving temperature distribution. Chen and Chen (1991) studied thermal buckling
of laminated plates under uniform and nonuniform temperature distribution using the
eight-node Serendipity finite element. Mathew, Singh and Rao (1992) investigated
thermal buckling of antisymmetric cross-ply composite laminates with a onedimensional
furite element having two nodes and six degrees of freedom.
Chandrashekhara (1992) accounted for transverse shear flexibility by using the
thermo-elastic version of the first-order shear deformation theory. This will also be
the case in this report. Literature on buckling and laminated composites abounds.
Brush and Aimroth (1975) published a book on Buckling of Bars, Plates, and Shells,
while Bushnell (1985) surveyed the Methods and Modes of Behaviour in Static
Collapse. The foundation for the study of composite materials was based on the
references [8], [10], [15] and [18]. The use of the Finite Element Method to analyse
the buckling behaviour of laminated structures comes from references [I], [4]. [I2].
[16], [24] and [32]. Reference [14] provided the basis for the formulation of the
variation of the governing equations. Most of the ideas in this report are based on
these publications and references.
Chapter I of this report introduces the concept of a composite. the formation of a
composite and a brief overview of the elements of a composite material. This chapter
also presents the concept of buckling that will form the basis of the development of
this project. At the end of this chapter the choice of the element that is used in this
study is justified. Chapter 2 provides the fundamentals of elasticity that relate to the
deformation of a loaded body. In this Chapter the stresses and strains are defined and
the temperature terms are introduced. In Chapter 3 the Mindlin plate theory is
presented with a view to laying the foundation for the analysis of laminated plates,
and as a starting point in the formulation of thermal buckling behaviour of laminated
plates. In Chapter 4 the elements of a composite material are discussed and the
constitutive equations of a laminated composite plate are built. Also the idea of
lamination is introduced and the various simplifications that can be introduced as a
result of lamination are discussed. The non-linear equilibrium equations and the
stability analysis of a composite plate are formulated in Chapter 5 using the
conventional anal}1ical method. The resulting equations justify the use of the Finite
Element Method as introduced in Chapter 6 and it is the method by which the
governing equations will be solved in ABAQUS computer analysis. The results for
various computer runs are presented for a normal plate, a plate with a square hole, and
the plate ""ith a circular cut-out in Chapter 7. Also in chapter 7 a comparison is made
between the laminate "ith a central hole and a normal plate to study the effect of a
cut-out on a critical buckling temperature. Appendices A deals the transverse shear in
plates, and Appendix B deals with the transformation of the laminate elastic constants
form the principal material direction to the general Cartesian co-ordinates. Also in
Appendix B the laminate stiffness matrices and these matrices are briefly evaluated
analytically. Appendix C is about the governing equations of laminated composites,
while Appendix D gives a full representation of the abbreviated finite element
equations of Chapter 6. Appendix E presents the list of ABAQUS input files that
were used in the computer simulation of Chapter 7.
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Thermoelastic stress and displacement in a thin rod due to an instantaneous heat sourceSiang, Hwang Hwei January 2011 (has links)
Digitized by Kansas Correctional Industries
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Finite element analysis of thermal stresses in semiconductor devicesDuerr, Joachim Karl Wilhelm 01 January 1990 (has links)
The failure of integrated circuit due to Silicon fracture is one of the problems associated with the production of a semiconductor device. The thermal stresses, which result in die cracking, are for the most part induced during the cooling process after attaching the die with Gold-Silicon solder. Major factors for stress generation in material systems are commonly large temperature gradients and substantial difference in coefficients of thermal expansion.
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An assessment of thermal hydraulic analysis methods for pressurized thermal shock evaluationsYoung, Eric P. 01 May 2002 (has links)
Improved methods of determining temperature transients in reactor systems are
desired because of recent interest in Pressurized Thermal Shock (PTS) issues.
The research presented herein was performed in support of the Nuclear Regulatory
Commission's effort to re-evaluate its existing PTS rules. These rules are
particularly important to the re-licensing of aging nuclear power plants. The much advanced
computational power available to industry may offer a tool that allows
the accurate calculation of temperatures inside the reactor vessel while not being
inaccessibly expensive. It is proposed that an off-the-shelf Computational Fluid
Dynamic (CFD) code, STAR-CD, can be a competitive tool in solving the thermal
hydraulic domain of a reactor system. A comparison of the methodology and
accuracy of the code types that have been previously used in PTS and one that has
not been used extensively, CFD, is provided.
A review of the literature shows that computer codes have been validated
for solving PTS scenarios. The highly specialized program, REMIX, has been
utilized extensively from 1986 to 1991 to interpret accident scenarios in reactor
systems. Other programs are also available that can calculate downcomer
temperatures including system and CFD type codes. Three codes representing the
three different types of programs available are described in detail in the literature
review section.
Data appropriate for assessing a program's ability to calculate the response
of a system to a PTS scenario is available from the current matrix of PTS tests
being completed at the APEX-CE facility of the Oregon State University Nuclear
Engineering department. The facility is a reduced scale integral test facility
originally built for modeling the then-proposed AP-600 plant designed by
Westinghouse. For the current test series, the facility was modified to model the
Palisades nuclear power plant, a Combustion Engineering Pressurized Water
Reactor (PWR). Two of the tests were chosen for their PTS typical conditions to
compare with calculations of STAR-CD, REMIX, and RELAP.
The computer models in each of the programs were either created, modified
from a previous version, or the calculations for the comparisons were contributed.
The downcomer temperatures at several locations and cold leg temperature
gradients, where available, were extracted from the data and calculations and
compared. Comparisons are presented in chapter 5 with graphs, along with some
interpretation of the comparisons. It was found that STAR-CD agreed best with the
data set in the downcomer and is the only program that calculated the temperature
gradient in the cold legs. The agreement of STAR-CD with the cold leg data is also
very good. REMIX and RELAP calculations agreement with data for downcomer
temperatures are found to be good for all comparisons made, qualitatively more
than quantitatively when contrasted with the STAR-CD calculations. / Graduation date: 2002
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Effect of thermal residual stresses on the stress-strain behavior of metal-matrix composites.Sims, John D. January 1990 (has links) (PDF)
Thesis (M.S. in Mechanical Engineering)--Naval Postgraduate School, September 1990. / Thesis Advisor(s): Dutta, I. Second Reader: Salinas, David. "September 1990." Description based on title screen as viewed on December 21, 2009. DTIC Identifier(s): Metal matrix composites, Thermal stresses, Residual stress, Stress strain relations, Fiber reinforced composites, Finite element analysis, Mathematical models, Aluminum alloys, Theses, Mechanical properties. Author(s) subject terms: Thermal Stresses, Composites, Finite Element. Includes bibliographical references (p. 57-59). Also available in print.
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Characterization of cryogenic microcracking in carbon fiber/epoxy composite materials /Timmerman, John Francis, January 2003 (has links)
Thesis (Ph. D.)--University of Washington, 2003. / Vita. Includes bibliographical references (leaves 119-128).
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Underfill adhesion characteristics, residual stresses and analysis of thermal stresses in flip chip packages /Sham, Man-Lung. January 2003 (has links)
Thesis (Ph. D.)--Hong Kong University of Science and Technology, 2003. / Includes bibliographical references. Also available in electronic version. Access restricted to campus users.
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