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1

Fang, Zhibin Sun Wei. "Image-guided modeling, fabrication and micromechanical analysis of bone and heterogeneous structure /." Philadelphia, Pa. : Drexel University, 2005. http://dspace.library.drexel.edu/handle/1860/549.

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Shao, Changming 1959. "Implementation of DSC model for dynamic analysis of soil-structure interaction problems." Diss., The University of Arizona, 1998. http://hdl.handle.net/10150/282628.

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The Disturbed State Concepts (DSC) model, with simplified unloading/reloading formulation, is implemented in a nonlinear dynamic finite element program for porous media named DSC-DYN2D. It can perform static, two phase dynamic and consolidation analysis of soils and soil-structure interaction problems with the DSC model. The model and the computer procedure are verified by back predictions of laboratory tests of clay, steel-clay interfaces as well as a simulation of pile-soil interaction problem. The Disturbed State Concepts have been developed recently as a constitutive modeling approach. In the DSC, the material is assumed to transform continuously and randomly from the relatively intact state to the fully adjusted state under loading. Hence, the observed response of the material is expressed in terms of the response of relatively intact and fully adjusted states. In this dissertation, the Disturbed State Concept constitutive model is developed by using the HiSS model for the relative intact part and the critical state model for the fully adjusted part in the material. The general formulation for implementation is developed. New and simplified unloading/reloading schemes are proposed for cyclic loading. Then the DSC model with the unloading/reloading scheme are implemented in the dynamic finite element program based on the generalized Biot's theory. The procedure for determining the parameters of the DSC model and the unloading/reloading is discussed. The parameters for the steel-clay interface are found from the tests and used for the prediction of the tests. Consolidation and cyclic loading tests from the field load tests on a pile segment were numerically simulated using the finite element program DSC-DYN2D and compared with field measurements and those from the previous analysis with the HiSS model. The DSC predictions show improved agreement with the field behavior of the pile compared to those from the HiSS model. The unloading/reloading models proposed in the study are simple yet give the realistic prediction of unloading and reloading behavior of the geomaterials under cyclic loading. Overall, the computer procedure with the DSC allows improved and realistic simulation of the complex dynamic soil-structure interaction problems.
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3

Patel, Reena R. "Complex Network Analysis for Early Detection of Failure Mechanisms in Resilient Bio-Structures." Thesis, Mississippi State University, 2019. http://pqdtopen.proquest.com/#viewpdf?dispub=10979098.

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Bio-structures owe their remarkable mechanical properties to their hierarchical geometrical arrangement as well as heterogeneous material properties. This dissertation presents an integrated, interdisciplinary approach that employs computational mechanics combined with flow network analysis to gain fundamental insights into the failure mechanisms of high performance, light-weight, structured composites by examining the stress flow patterns formed in the nascent stages of loading for the rostrum of the paddlefish. The data required for the flow network analysis was generated from the finite element analysis of the rostrum. The flow network was weighted based on the parameter of interest, which is stress in the current study. The changing kinematics of the structural system was provided as input to the algorithm that computes the minimum-cut of the flow network. The proposed approach was verified using two classical problems – three- and four-point bending of a simply-supported concrete beam. The current study also addresses the methodology used to prepare data in an appropriate format for a seamless transition from finite element binary database files to the abstract mathematical domain needed for the network flow analysis. A robust, platform-independent procedure was developed that efficiently handles the large datasets produced by the finite element simulations. Results from computational mechanics using Abaqus and complex network analysis are presented. The complex network strategy successfully identified failure mechanisms in the bio-structure by identifying strain localization in regions of tension, and buckling/crushing in regions of compression. The transdisciplinary strategy used in this study identified the failure mechanisms early, when the material was still in the linearly elastic regime, thereby tremendously reducing the computational time and cost as compared to running a finite element analysis to failure. This work also developed five proof-of-concept, bio-inspired models with varying lattice complexity based on the rostrum. Performance of these bio-inspired models was analyzed with respect to the stress and deformation. Numerical experiments were carried out on one of the bio-inspired model to demonstrate the application of newly developed similitude laws for blast loading. This research has laid the groundwork for an efficient design-test-build cycle for rapid prototyping of novel bio-inspired structures by using flow network analysis, finite element analysis, and similitude laws.

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Gwon, Tae gyun. "Structural Analyses of Wind Turbine Tower for 3 kW Horizontal Axis Wind Turbine." DigitalCommons@CalPoly, 2011. https://digitalcommons.calpoly.edu/theses/600.

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Structure analyses of a steel tower for Cal Poly's 3 kW small wind turbine is presented. First, some general design aspects of the wind turbine tower are discussed: types, heights, and some other factors that can be considered for the design of wind turbine tower. Then, Cal Poly's wind turbine tower design is presented, highlighting its main design features. Secondly, structure analysis for Cal Poly's wind turbine tower is discussed and presented. The loads that are specific to the wind turbine system and the tower are explained. The loads for the static analysis of the tower were calculated as well. The majority of the structure analysis of the tower was performed using the finite element method (FEM). Using Abaqus, commercial FEM software, both static and dynamic structural analyses were performed. A simplified finite element model that represents the wind turbine tower was created using beam, shell, and inertia elements. An ultimate load condition was applied to check the stress level of the tower in the static analysis. For the dynamic analysis, the frequency extraction was performed in order to obtain the natural frequencies and the mode shapes of the tower. Using the results, the response spectrum analysis and the transient dynamic analysis, which are based on the modal superposition method, were performed in order to see the structure's response for earthquakes that are likely to happen at the wind turbine installation site.
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Mokashi, Prasad Shrikant. "Numerical modeling of homogeneous and bimaterial crack tip and interfacial cohesive zones with various traction-displacement laws." Columbus, Ohio : Ohio State University, 2007. http://rave.ohiolink.edu/etdc/view?acc%5Fnum=osu1180621217.

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6

Rubio, Jose Enrique. "Design, Manufacture, and Structural Dynamic Analysis of a Biomimetic Insect-Sized Wing for Micro Air Vehicles." ScholarWorks@UNO, 2017. https://scholarworks.uno.edu/td/2432.

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The exceptional flying characteristics of airborne insects motivates the design of biomimetic wing structures that can exhibit a similar structural dynamic behavior. For this purpose, this investigation describes a method for both manufacturing a biomimetic insect-sized wing using the photolithography technique and analyzing its structural dynamic response. The geometry of a crane fly forewing (family Tipulidae) is acquired using a micro-computed tomography scanner. A computer-aided design model is generated from the measurements of the reconstructed scanned model of the insect wing to design the photomasks of the membrane and the venation network required for the photolithography procedure. A composite material wing is manufactured by patterning the venation network using photoresist SU-8 on a Kapton film for the assembling of the wing. A single material artificial wing is fabricated using the photoresist SU-8 for both the membrane and the network of veins. Experiments are conducted using a modal shaker and a digital image correlation (DIC) system to determine the natural frequencies and the mode shapes of the artificial wing from the fast Fourier transform of the displacement response of the wing. The experimental results are compared with those from a finite element (FE) model of the wing. A numerical simulation of the fluid-structure interaction is conducted by coupling the FE model of the artificial wing with a computational fluid dynamics model of the surrounding airflow. From these simulations, the deformation response and the coefficients of drag and lift of the artificial wing are predicted for different freestream velocities and angles of attack. Wind-tunnel experiments are conducted using the DIC system to determine the structural deformation response of the artificial wing under different freestream velocities and angles of attack. The vibration modes are dominated by a bending and torsional deformation response. The deformation along the span of the wing increases nonlinearly from the root of the wing to the tip of the wing with Reynolds number. The aerodynamic performance, defined as the ratio of the coefficient of lift to the coefficient of drag, of the artificial wing increases with Reynolds number and angle of attack up to the critical angle of attack.
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7

Giardina, Ronald Joseph Jr. "General Nonlinear-Material Elasticity in Classical One-Dimensional Solid Mechanics." ScholarWorks@UNO, 2019. https://scholarworks.uno.edu/td/2666.

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We will create a class of generalized ellipses and explore their ability to define a distance on a space and generate continuous, periodic functions. Connections between these continuous, periodic functions and the generalizations of trigonometric functions known in the literature shall be established along with connections between these generalized ellipses and some spectrahedral projections onto the plane, more specifically the well-known multifocal ellipses. The superellipse, or Lam\'{e} curve, will be a special case of the generalized ellipse. Applications of these generalized ellipses shall be explored with regards to some one-dimensional systems of classical mechanics. We will adopt the Ramberg-Osgood relation for stress and strain ubiquitous in engineering mechanics and define a general internal bending moment for which this expression, and several others, are special cases. We will then apply this general bending moment to some one-dimensional Euler beam-columns along with the continuous, periodic functions we developed with regard to the generalized ellipse. This will allow us to construct new solutions for critical buckling loads of Euler columns and deflections of beam-columns under very general engineering material requirements without some of the usual assumptions associated with the Ramberg-Osgood relation.
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Rodriguez, George IV. "Finite Element Modeling of Delamination Damage in Carbon Fiber Laminates Subject to Low-Velocity Impact and Comparison with Experimental Impact Tests Using Nondestructive Vibrothermography Evaluation." DigitalCommons@CalPoly, 2016. https://digitalcommons.calpoly.edu/theses/1583.

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Carbon fiber reinforced composites are utilized in many design applications where high strength, low weight, and/or high stiffness are required. While composite materials can provide high strength and stiffness-to-weight ratios, they are also more complicated to analyze due to their inhomogeneous nature. One important failure mode of composite structures is delamination. This failure mode is common when composite laminates are subject to impact loading. Various finite element methods for analyzing delamination exist. In this research, a modeling strategy based on contact tiebreak definitions in LS-DYNA®was used. A finite element model of a low-velocity impact event was created to predict delamination in a composite laminate. The resulting delamination relative size and shape was found to partially agree with analytical and experimental results for similar impact events, while the force-time plot agreed well with experimental results. A small difference in contact time in the simulation compared to experimental testing is likely due to the omission of composite failure modes other than delamination. Experimental impact testing and subsequent vibrothermography analysis showed delamination damage in locations shown in previous research. This confirmed the validity of vibrothermography as a nondestructive evaluation technique for analyzing post-impact delamination.
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Cil, Kursad. "Free Flexural (or Bending) Vibrations Analysis Of Doubly Stiffened, Composite, Orthotropic And/or Isotropic Base Plates And Panels (in Aero-structural Systems)." Master's thesis, METU, 2003. http://etd.lib.metu.edu.tr/upload/2/1062256/index.pdf.

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In this Thesis, the problem of the Free Vibrations Analysis of Doubly Stiffened Composite, Orthotropic and/or Isotropic, Base Plates or Panels (with Orthotropic Stiffening Plate Strips) is investigated. The composite plate or panel system is made of an Orthotropic and/or Isotropic Base Plate stiffened or reinforced by adhesively bonded Upper and Lower Orthotropic Stiffening Plate Strips. The plates are assumed to be the Mindlin Plates connected by relatively very thin adhesive layers. The general problem under study is considered in terms of three problems, namely Main PROBLEM I Main PROBLEM II and Main PROBLEM III. The theoretical formulation of the Main PROBLEMS is based on a First Order Shear Deformation Plate Theory (FSDPT) that is, in this case, the Mindlin Plate Theory. The entire composite system is assumed to have simple supports along the two opposite edges so that the Classical Levy'
s Solutions can be applied in that direction. Thus, the transverse shear deformations and the rotary moments of inertia of plates are included in the formulation. The very thin, yet elastic deformable adhesive layers are considered as continua with transverse normal and shear stresses. The damping effects in the plates and the adhesive layers are neglected. The sets of the systems of equations of the Mindlin Plate Theory are reduced to a set of the Governing System of First Order Ordinary Differential Equations in the state vector form. The sets of the Governing System for each Main PROBLEM constitute a Two-Point Boundary Value Problem in the y-direction which is taken along the length of the plates. Then, the system is solved by the Modified Transfer Matrix Method (with Interpolation Polynomials and/or Chebyshev Polynomials)which is a relatively semi-analytical and numerical technique. The numerical results and important parametric studies of the natural modes and the corresponding frequencies of the composite system are presented.
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Kahraman, Engin. "Investigation Of The Dynamic Properties Of Plate-like Structures." Master's thesis, METU, 2011. http://etd.lib.metu.edu.tr/upload/12613703/index.pdf.

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This study presents the investigation and the verification of the modal parameters of a plate-like structure by using different modal analysis methods. A fin-like structure which is generally used in aircraft is selected as a subcategory of a plate-like test structure. In the first part of the thesis, the natural frequencies and the corresponding mode shapes of the fin are extracted by Finite Element Analysis method. Classical Modal Analysis and Testing methods comprising both impact hammer and modal shaker applications are then applied in order to obtain the modal parameters such as
resonance frequencies, mode shapes and damping ratios. In the second part, a recent modal analysis technique, Operational Modal Analysis, is also applied in the laboratory environment. Since Operational Modal Analysis method does not require any information of input forcing, the fin structure is tested under both mechanical and acoustical types of excitations without measuring the given input forces. Finally, Operational Modal Analysis and Testing is also performed under various flow conditions generated in the wind tunnel which may simulate the real operating environment for the fin structure. The modal parameters extracted under these flow conditions are then compared with the previously obtained Finite Element, Classical and Operational Modal Analyses results.
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11

Liu, Di. "VIBRATION OF STEEL-FRAMED FLOORS SUPPORTING SENSITIVE EQUIPMENT IN HOSPITALS, RESEARCH FACILITIES, AND MANUFACTURING FACILITIES." UKnowledge, 2015. http://uknowledge.uky.edu/ce_etds/34.

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Floors have traditionally been designed only for strength and deflection serviceability. As technological advances have been made in medical, scientific and micro-electronics manufacturing, many types of equipment have become sensitive to vibration of the supporting floor. Thus, vibration serviceability has become a routinely evaluated limit state for floors supporting sensitive equipment. Equipment vibration tolerance limits are sometimes expressed as waveform peak acceleration, and are more often expressed as narrowband spectral acceleration, or one-third octave spectral velocity. Current floor vibration prediction methods, such as those found in the American Institute of Steel Construction Design Guide 11, Floor Vibrations Due to Human Activity, the British Steel Construction Institute P354, Design of Floors for Vibration: a New Approach and the British Concrete Centre CCIP-016 A Design Guide for Footfall Induced Vibration of Structures, have limitations. It has been observed that non-structural components such as light-weight partitions could significantly change floor dynamic properties. Current prediction methods do not provide a fundamental frequency manual prediction method nor finite element modeling guidance for floors with non-structural components. Current prediction methods only predict waveform peak acceleration and do not provide predictions for frequency domain response including narrowband spectral acceleration or one-third octave spectral velocity. Also, current methods are not calibrated to provide a specific level of conservatism. This research project provides (1) a fundamental frequency manual prediction method for floors with lightweight partitions; (2) an improved finite element modeling procedure for floors with light-weight partitions; (3) a procedure to predict the vibration response in narrow-band spectrum and one-third octave band spectrum which can be directly compared with vibration tolerance limits; and (4) a simplified experimental procedure to estimate the floor natural frequencies. An experimental program including four steel-framed building floors and a concrete was completed. Modal tests were performed on two of the steel-framed buildings and the concrete building using an electrodynamic shaker. Experimental modal analysis techniques were used to estimate the modal properties: natural frequencies, mode shapes, and damping ratios. Responses to walking excitation were measured several times in each tested bay for individuals walking at different walking speeds. During each test, the walker crossed the middle of the bay using a metronome to help maintain the intended cadence. The proposed method was used to predict the modal properties and responses to walking. The measurements are used to assess the precision of the proposed methods and to calibrate the prediction methods to provide a specific probability that the actual response will exceed the predicted response. Comparison of measurements and predictions shows the proposed methods are sufficiently accurate for design usage.
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Giardina, Ronald J. Jr. "On The Ramberg-Osgood Stress-Strain Model And Large Deformations of Cantilever Beams." ScholarWorks@UNO, 2017. http://scholarworks.uno.edu/td/2377.

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In this thesis the Ramberg-Osgood nonlinear model for describing the behavior of many different materials is investigated. A brief overview of the model as it is currently used in the literature is undertaken and several misunderstandings and possible pitfalls in its application is pointed out, especially as it pertains to more recent approaches to finding solutions involving the model. There is an investigation of the displacement of a cantilever beam under a combined loading consisting of a distributed load across the entire length of the beam and a point load at its end and new solutions to this problem are provided with a mixture of numerical techniques, which suggest strong mathematical consistency within the model for all theoretical assumptions made. A physical experiment was undertaken and the results prove to be inaccurate when using parameters derived from tensile tests, but when back calculating parameters from the beam test the model has a 14.40% error at its extreme against the experimental data suggesting the necessity for further testing.
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Andraéy, Erik. "Development of verified FE simulation method on crimp joint with gasket : A combined experimental and numerical study." Thesis, Blekinge Tekniska Högskola, Institutionen för maskinteknik, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:bth-21924.

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When developing drivetrain cooling modules for commercial vehicles, the top priority is the strength of the products. The reason lays within the structural change that companies are undergoing where the warehouses are minimized and the companies are relying on the transportation of commercial vehicles. If a drivetrain cooling module would fail to maintain a targeted temperature range of the drivetrain, there is not long until the vehicle is forced to a stop. At worst, the downtime of commercial vehicles can cause companies to come to a halt as well. Therefore, developing verified FE simulation methods together with strength verification tests, are some of the core activities to ensure the strength of the cooling modules before implementation in vehicles. One of the methods that have not been sufficiently verified regards how to perform structural FEA on a crimp joint with a gasket. A crimp joint is established through a hemming process, where the aluminium header tabs are crimped over the polyamide tank, creating a watertight seal together with a gasket. The objective of this master’s thesis is to verify the existing simulation methods of the crimp joint and determine the margin of error with respect to strains. The objective of this thesis is also to develop a verified FE simulation method with a lower margin of error compared to the existing methods. The verification of the methods has been conducted through a comparison between numerical results and an experimental stress analysis, where the strain located on the header is measured with strain gauges in a pressure pulsation rig. The average margin of error found on the three existing methods of simulating the crimp joint was 39,7%, 13,4%, and 11,5% located on the outer bottom dimensioning radius of the crimp joint at a pressure of 100 kPa. However, the method used to determine the margin of error was found to be invalid, but the margin of error is only slightly affected by the verification method where the existing methods still are insufficiently representing the crimp joint. The method of determining the margin of error was then corrected for the development of the new method to represent the crimp joint in the FE model. The developed method in this thesis has an average margin of error of 6,9% at 100, 160, 220, and 260 kPa.
Vid utveckling av kylarmoduler för drivlinor som appliceras i kommersiella fordon, är högsta prioritet att säkerhetsställa hållfastheten hos produkterna. Anledningen ligger kring den strukturomvandling som företag genomgår där storleken på lagerlokaler minskar och företagen väljer att förlita sig på transporterna som utförs av kommersiella fordon istället. Ifall en kylarmodul inte skulle klara av att bibehålla ett bestämt temperaturintervall hos drivlinan så dröjer det inte länge förens fordonet tvingas att stanna. I värsta fall kan fordonets stillestånd påverka ett företag att tvingas stanna i väntan. Därför är utveckling av FE simuleringsmetoder tillsammans med utmattningstest, några av de kärnaktiviteter som utförs för att säkerhetsställa hållfastheten av kylarmodulerna innan de implementeras i fordon. En av de metoder som ännu inte blivit tillräckligt verifierat gäller hur man utför FEA på ett falsförband med packning. Falsförbandet skapas genom en falsningsprocess där ändplåten av aluminium falsas över polyamidtanken, vilket skapar ett vattentätt förband med hjälp av packningen. Omfattningen av detta examensarbete gäller att verifiera de existerande simuleringsmetoderna av falsförbandet och bestämma felmarginalen med avseende på töjningar. Omfattningen av examensarbetet innefattar även ett utvecklingsarbete av en ny FE simuleringsmetod med en lägre felmarginal jämfört med de existerande metoderna. Verifieringen av metoderna sker genom en jämförelse mellan de numeriska resultaten och en experimentell spänningsanalys där töjningen på ändplåten är uppmätt med hjälp av trådtöjningsgivare i en tryckpulsationsrigg. Den genomsnittliga felmarginalen av de tre existerande metoderna för att simulera falsförbandet var 37,9%, 13,4%, och 11,5% vid den nedre dimensionerande yttre radien på falsförbandet vid ett tryck på 100 kPa. Den använda metoden för att bestämma felmarginalen upptäcktes senare vara felaktig, men det resulterar endast i små förändringar av den bestämda felmarginalen, de existerande simuleringsmetoderna är fortfarande sedda som otillräckliga. Metoden för att bestämma felmarginalen korrigerades sedan inför utvecklandet av den nya FE simuleringsmetoden av falsförbandet. Den utvecklade metoden i detta examensarbete har en genomsnittlig felmarginal på 6,9% vid 100, 160, 220 och 260 kPa.
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Tuvehed, Petter. "Coupled structural acoustic analysis of chassis mounted fuel tanks." Thesis, Luleå tekniska universitet, Institutionen för teknikvetenskap och matematik, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-70052.

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15

Lea, Patrick D. "Fluid Structure Interaction with Applications in Structural Failure." Thesis, Northwestern University, 2014. http://pqdtopen.proquest.com/#viewpdf?dispub=3605735.

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Methods for modeling structural failure with applications for fluid structure interaction (FSI) are developed in this work. Fracture as structural failure is modeled in this work by both the extended finite element method (XFEM) and element deletion. Both of these methods are used in simulations coupled with fluids modeled by computational fluid dynamics (CFD). The methods presented here allow the fluid to pass through the fractured areas of the structure without any prior knowledge of where fracture will occur. Fracture modeled by XFEM is compared to an experimental result as well as a test problem for two phase coupling. The element deletion results are compared with an XFEM test problem, showing the differences and similarities between the two methods.

A new method for modeling fracture is also proposed in this work. The new method combines XFEM and element deletion to provide a robust implementation of fracture modeling. This method integrates well into legacy codes that currently have element deletion functionality. The implementation allows for application by a wide variety of users that are familiar with element deletion in current analysis tools. The combined method can also be used in conjunction with the work done on fracture coupled with fluids, discussed in this work.

Structural failure via buckling is also examined in an FSI framework. A new algorithm is produced to allow for structural subcycling during the collapse of a pipe subjected to a hydrostatic load. The responses of both the structure and the fluid are compared to a non-subcycling case to determine the accuracy of the new algorithm.

Overall this work looks at multiple forms of structural failure induced by fluids modeled by CFD. The work extends what is currently possible in FSI simulations.

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Sjöstrand, Edvin. "Structural Analysis of Underwater Detonations." Thesis, Luleå tekniska universitet, Institutionen för teknikvetenskap och matematik, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-85099.

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The knowledge how an object withstand an underwater detonation is critical within the defense industry. This is mostly done today with physicals test which are both time consuming and connected with high costs. The aim of this thesis is to provide recommendations and guidelines on how to model and analyze a structural response of underwater detonations. This investigation are focused on firstly investigate several theoretical simulation methods and thereafter develop a model of the chosen method.  The simulation method was decided to be the Multi-Material Arbitrary Lagrangian Euler(MMALE) using the software LS-Dyna. To receive a model with functionality to simulate an explosion a method of six steps is developed to increase the complexity. The final step is to be able to analyze a structural response of an object.  The validation phase contained several convergence studies of the two Equations of states and a varying element size compared to analytical equations. The plan was to perform a validation test but because of travel restrictions due to the Covid-19 situation an alternative validation method was used. This method involved two external reports with specified measurement data.  The aim to develop a model is reached as the model performs well against the cylinder in the validation phase, however the element size is the most important parameter in an accurate model. The developed model shows good agreement regarding the structural response of an object when compared to well defined and reported experiments.
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Drazin, Paul Luke. "Modeling and Analysis of Elements in Structural Mechanics." Thesis, University of California, Berkeley, 2017. http://pqdtopen.proquest.com/#viewpdf?dispub=10276506.

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The focus of this work is to advance the theoretical and modeling techniques for the fields of hybrid simulation and multi-slider friction pendulum systems (MSFPs). Hybrid Simulation is a simulation technique involving the integration of a physical system and a computational system with the use of actuators and sensors. This method has a strong foundation in the experimental mechanics community where it has been used for many years. The hybrid simulation experiments are performed with the assumption of an accurate result as long as the main causes of error are reduced. However, the theoretical background on hybrid testing needs to be developed in order validate these findings using this technique. To achieve this objective, a model for hybrid simulation is developed and applied to three test cases: an Euler-Bernoulli beam, a nonlinear damped, driven pendulum, and a boom crane structure. Due to the complex dynamics that these three test cases exhibit, L2 norms, Lyapunov exponents, and Lyapunov dimensions, as well as correlation exponents were utilized to analyze the error in hybrid simulation tests. From these three test cases it was found that hybrid simulations are highly dependent on the natural frequencies of the dynamical system as well as how and where the hybrid split is located. Thus, proper care must be taken when conducting a hybrid experiment in order to guarantee reliable results.

Multi-stage friction pendulum systems (MSFPs), such as the triple friction pendulum (TFP), are currently being developed as seismic isolators. However, all current analytical models are inadequate in modeling many facets of these devices. Either the model can only handle uni-directional ground motions while incorporating the kinetics of the TFP system, or the model ignores the kinetics and can handle bi-directional motion. And in all cases, the model is linearized to simplify the equations. The second part of this dissertation presents an all-in-one model that incorporates the full nonlinear kinetics of the TFP system, while allowing for bi-directional ground motion. In this way, the model presented here is the most complete single model currently available. It was found that the non-linear model can more accurately predict the experimental results for large displacements due to the nonlinear kinematics used to describe the system. The model is also able to successfully predict the experimental results for bi-directional ground motions.

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Ruparel, Tejas. "Multiple Grid Multiple Time-Scale (MGMT) Simulations in Linear Structural Dynamics." Thesis, The George Washington University, 2015. http://pqdtopen.proquest.com/#viewpdf?dispub=3669113.

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The work presented in this dissertation describes a general algorithm and its Finite Element (FE) implementation for performing concurrent multiple sub-domain simulations in linear structural dynamics. Using this approach one can solve problems in which the domain under analysis can be selectively discretized spatially and temporally, hence allowing the user to obtain a desired level of accuracy in critical regions whilst improving computational efficiency globally. The mathematical background for this approach is largely derived from the fundamental principles of Domain Decomposition Methods (DDM) and Lagrange Multipliers, used to obtain coupled equations of motion for distinct regions of a continuous domain. These methods when combined together systematically yield constraint forces that not only ensure conservation of energy, but also enforce continuity of field quantities across sub-domain interfaces. Multiple Grid (MG) coupling between conforming or non-conforming sub-domains is achieved in the form of linear multi-point constraints that are modeled using Mortar Finite Element Method (M-FEM); whereas coupled Multiple Time-scale (MT) equations are derived for the classical Newmark integration scheme and its constituent algorithms. A rigorous proof of stability is provided using Energy Method and necessary conditions for enforcing energy balance are discussed in reference with field variables that are selected to enforce sub-domain interface continuity. Fully discretized equations of motion for component sub-domains, augmented with an interface continuity condition are then solved using block elimination method and Crout factorization. A step-by-step solution approach, utilizing recursive black box sub-routines, is modeled in order to allow efficient implementation within existing finite element frameworks.

Proposed MGMT Method and corresponding solution algorithm is systematically implemented by using the finite element approach and programming in FORTRAN 90. Resulting in-house code - FEAPI (Finite Element Analysis Programming Interface) is capable of solving linear structural dynamics problems that are modeled using independently discretized sub-domains. Auxiliary sub-routines for defining pre simulation parameters and for viewing global/component sub-domain results are built into FEAPI and work in conjugation with GiD; a universal, adaptive and user-friendly pre and post-processor. Overall stability, numerical accuracy and computational efficiency of MGMT Method is evaluated and verified using a series of benchmark examples. Verification matrices take into consideration performance evaluation factors such as energy balance (at global and component-sub-domain levels), interface continuity, evolution/distribution of kinematic quantities and propagation of structural waves across connecting sub-domains. Assessment of computational efficiency is derived by comparing the size of respective FE problems (nodes, elements, number of equations, skyline storage requirements) and the required computation times (CPU solution time). Discussed examples highlight the greatest advantage of MGMT Method; which is significant gain in simulation speedups (at the cost of reasonably small errors).

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Nair, Arun Unnikrishnan. "Evolutionary numerical methods applied to minimum weight structural design and cardiac mechanics /." View online ; access limited to URI, 2005. http://0-wwwlib.umi.com.helin.uri.edu/dissertations/dlnow/3188843.

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20

Tran, Tuan H. "Landing-Gear Impact Response: A Non-linear Finite Element Approach." UNF Digital Commons, 2019. https://digitalcommons.unf.edu/etd/896.

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The primary objective of this research is to formulate a methodology of assessing the maximum impact loading condition that will incur onto an aircraft’s landing gear system via Finite Element Analysis (FEA) and appropriately determining its corresponding structural and impact responses to minimize potential design failures during hard landing (abnormal impact) and shock absorption testing. Both static and dynamic loading condition were closely analyzed, compared, and derived through the Federal Aviation Administration’s (FAA) airworthiness regulations and empirical testing data. In this research, a nonlinear transient dynamic analysis is developed and established via NASTRAN advanced nonlinear finite element model (FEM) to simulate the worst-case loading condition. Under the appropriate loading analysis, the eye-bar and contact patch region theory were then utilized to simulate the tire and nose wheel interface more accurately. The open geometry of the nose landing gear was also optimized to minimize the effect of stress concentration. The result of this research is conformed to the FAA’s regulations and bound to have an impact on the design and development of small and large aircraft’s landing gear for both near and distant future.
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21

Jang, Jae Won. "Characterization of live modeling performance boundaries for computational structural mechanics /." Thesis, Connect to this title online; UW restricted, 2007. http://hdl.handle.net/1773/10178.

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22

Gasparini, Riccardo. "Engineering Analysis in Imprecise Geometric Models." FIU Digital Commons, 2014. http://digitalcommons.fiu.edu/etd/1793.

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Engineering analysis in geometric models has been the main if not the only credible/reasonable tool used by engineers and scientists to resolve physical boundaries problems. New high speed computers have facilitated the accuracy and validation of the expected results. In practice, an engineering analysis is composed of two parts; the design of the model and the analysis of the geometry with the boundary conditions and constraints imposed on it. Numerical methods are used to resolve a large number of physical boundary problems independent of the model geometry. The time expended due to the computational process are related to the imposed boundary conditions and the well conformed geometry. Any geometric model that contains gaps or open lines is considered an imperfect geometry model and major commercial solver packages are incapable of handling such inputs. Others packages apply different kinds of methods to resolve this problems like patching or zippering; but the final resolved geometry may be different from the original geometry, and the changes may be unacceptable. The study proposed in this dissertation is based on a new technique to process models with geometrical imperfection without the necessity to repair or change the original geometry. An algorithm is presented that is able to analyze the imperfect geometric model with the imposed boundary conditions using a meshfree method and a distance field approximation to the boundaries. Experiments are proposed to analyze the convergence of the algorithm in imperfect models geometries and will be compared with the same models but with perfect geometries. Plotting results will be presented for further analysis and conclusions of the algorithm convergence
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23

Bulca, Ferhan. "The kinematics and workspace analysis of platform mechanisms /." Thesis, McGill University, 1998. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=34706.

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This thesis concerns parallel, platform mechanisms, consisting of two distal links that are connected to each other by a set of open kinematic chains, called legs. Particularly, mechanisms with redundant loops, kinematically quite challenging, are investigated. Existing methods of analysis and their shortcomings are outlined and alternatives which help to overcome them are developed.
Definitions and analyses of platform mechanisms, mobility and degree-of-freedom are reviewed. Kinematic analysis and workspace determination of platform mechanisms are thoroughly investigated.
An algebraic method, based on the functional matrix of mechanisms, as defined by Freudenstein, is applied to determine their degree of freedom (DOF). It is shown with examples that this method unambiguously yields the DOF for mechanisms where other methods fail.
The effects of extra legs, and hence, redundant loops, are discussed. The statics, differential and positional kinematics of these mechanisms are investigated. Kinematic-mapping techniques are used to analyze the constraints applied by individual legs to the platform. Current methods of workspace analysis of platform mechanisms are reviewed. A novel technique, which contains both position and orientation information, is introduced. It is shown that this method successfully treats platform mechanisms, with or without redundant loops. However, it may be computationally expensive for some mechanisms, such as spherical wrist mechanisms. An alternative technique, based on the Euler-Rodrigues parameters of a rotation, is also introduced for spherical mechanisms, of both serial and platform types.
The features of some of the methods introduced here are applied to a novel mechanism introduced elsewhere, namely, the double-tetrahedral mechanism (DTM), which it is a paradigm of closed-loop mechanisms with redundant loops.
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24

Walls, Kenneth Cline. "Multi-material contact for computational structural mechanics." Birmingham, Ala. : University of Alabama at Birmingham, 2008. https://www.mhsl.uab.edu/dt/2008m/walls.pdf.

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25

Li, Nan. "Development of real-time cellular impedance analysis system." Thesis, University of Sussex, 2014. http://sro.sussex.ac.uk/id/eprint/49706/.

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The cell impedance analysis technique is a label-free, non-invasive method, which simplifies sample preparation and allows applications requiring unmodified cell retrieval. However, traditional impedance measurement methods suffer from various problems (speed, bandwidth, accuracy) for extracting the cellular impedance information. This thesis proposes an improved system for extracting precise cellular impedance in real-time, with a wide bandwidth and satisfactory accuracy. The system hardware consists of five main parts: a microelectrode array (MEA), a stimulation circuit, a sensing circuit, a multi-function card and a computer. The development of system hardware is explored. Accordingly, a novel bioimpedance measurement method coined digital auto balancing bridge method, which is improved from the traditional analogue auto balancing bridge circuitry, is realized for real-time cellular impedance measurement. Two different digital bridge balancing algorithms are proposed and realized, which are based on least mean squares (LMS) algorithm and fast block LMS (FBLMS) algorithm for single- and multi-frequency measurements respectively. Details on their implementation in FPGA are discussed. The test results prove that the LMS-based algorithm is suitable for accelerating the measurement speed in single-frequency situation, whilst the FBLMS-based algorithm has advantages in stable convergence in multi-frequency applications. A novel algorithm, called the All Phase Fast Fourier Transform (APFFT), is applied for post-processing of bioimpedance measurement results. Compared with the classical FFT algorithm, the APFFT significantly reduces spectral leakage caused by truncation error. Compared to the traditional FFT and Digital Quadrature Demodulation (DQD) methods, the APFFT shows excellent performance for extracting accurate phase and amplitude in the frequency spectrum. Additionally, testing and evaluation of the realized system has been performed. The results show that our system achieved a satisfactory accuracy within a wide bandwidth, a fast measurement speed and a good repeatability. Furthermore, our system is compared with a commercial impedance analyzer (Agilent 4294A) in biological experiments. The results reveal that our system achieved a comparable accuracy to the commercial instrument in the biological experiments. Finally, conclusions are given and the future work is proposed.
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26

Bande, Gilbert. "A combined approach for analysis of single crystal nickel base superalloys /." Thesis, McGill University, 2001. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=37868.

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The purpose of this research is to develop a new tool for mechanical design and analysis of single crystal (SC) nickel base superalloys used in gas turbine engine components. The principle of this tool is based on the extension of the predictive models for isotropic material behavior to anisotropic materials such as SC nickel, base superalloys. This objective is achieved by combining the two main approaches used in the literature for SC materials development: the macroscopic approach and the microscopic approach. For that reason, this theory is designated as the "combined approach " (CA).
The structure of the CA theory requires two main elements: a viscoplastic model (that admits a yield function) and a slip factor. The viscoplastic model describes the behavior of the material in the macroscopic level. Conversely, the slip factor based on the crystallographic theory, accounts for the micro-slip state that dominates SC materials during deformation.
In order to determine the slip factor, a preliminary slip trace study of the crystal is established. Also to determine material constants from experimental data, a procedure has been developed to reduce the 3D basic equations into a one-dimensional form. The model has been evaluated for its predictive capability on SC material behavior including orientation dependence of the initial yielding, tension/compression asymmetry, stress-strain response, fully reversed cyclic response, creep response and relaxation response. In almost all the cases, good correlation has been observed between the predicted responses and experimental data, when available. Furthermore, it is believable that the CA can be successfully used for many other SC materials such as the body-centered-cubic (b.c.c) or the hexagonal-closed-packet (h.c.p). In view of all these results, the CA theory seems to offer the greatest promise in this regard. Limitations and future development needs are discussed.
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27

Khan, Arshad A. (Arshad Ahmad). "Concrete properties and thermal stress analysis of members at early ages." Thesis, McGill University, 1995. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=29060.

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This research program presents an experimental study on the mechanical and thermal properties of different types of concretes at very early ages, (i.e., during hydration). These properties are investigated for temperature-matched curing, sealed curing and air-dried curing. Three types of concretes are studied including normal-strength (30 MPa), medium-strength (70 MPa) and high-strength (100 MPa) concretes. About 300 cylinders and 175 flexural beams were tested to determine the early-age mechanical properties including compressive stress-strain responses, gain of compressive strength, change in elastic modulus and variation of tensile strength. Creep frames and measuring devices were built to enable the experimental determination of early-age creep, with unloaded, companion specimens giving the corresponding shrinkage strains. A temperature-matched curing bath was developed to measure the heat of hydration and to subject 15 cylinders and 12 flexural beams to temperature-matched curing. The thermal properties investigated included the heat of hydration, the thermal conductivity, the specific heat and the coefficient of thermal expansion. Expressions are proposed to predict the development of compressive strength, elastic modulus and modulus of rupture as a function of the type of concrete and the type of curing.
Sub-routines were developed for a finite element thermal analysis program "DETECT" to predict the variation of temperatures during hydration. Additional sub-routines, using the maturity concept, predicted the compressive strength, elastic modulus and tensile strength of each element, in the time domain. An experimental study was performed to observe the effect of different curing conditions and early-form stripping on the temperature and strain development in structural concrete members. Comparisons are made between the measured and predicted temperatures in large concrete columns and precast tee beams and slabs.
Sub-routines were developed to enable incremental stress analysis in the time domain to account for the rapidly changing material properties and the influence of creep. Predictions of the risk of cracking were made and compared with observations from experiments on concrete elements during hydration. Parametric analyses were carried out to determine the influence of key thermal properties, time of formwork removal, creep, and concrete strength on the thermal gradients developed and the risk of thermal cracking.
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28

Park, Inn-Joon 1965. "Disturbed state modeling for dynamic and liquefaction analysis." Diss., The University of Arizona, 1997. http://hdl.handle.net/10150/282577.

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Although a number of models have been proposed to characterize behavior of geological materials including elastic, plastic, and cyclic loading responses, few constitutive models have been developed for the behavior of fully saturated sands and interfaces including liquefaction under dynamic loading. Such realistic constitutive models play an important role in analyzing and predicting the response and design of soil-structure interaction systems. Also, in the engineering view of the complexity of the material behavior, it becomes necessary to develop and use computer procedure (finite element method) for the analysis and prediction of behavior of geotechnical problems. A general concept, called the disturbed state concept (DSC), that can characterize behavior of geological material is developed in this dissertation for the behavior of saturated sands and sand-steel interfaces. The DSC model is an unified approach and allows hierarchical use of the model for factors such as elastic and plastic strains, damage, and softening and stiffening. The model parameters for a saturated sand and a sand-steel interface are evaluated using data from comprehensive laboratory tests; truly triaxial test device for the saturated sand and cyclic multi-degree-of-freedom device (CYMDOF-P) for the interface. The laboratory test results are also used for the verification of DSC model. In general, the model predictions were found to provide satisfactory correlation with the test results. The DSC model with the foregoing parameters is implemented in a nonlinear dynamic finite element program(DSC-DYN2D). It is used to solve two boundary value problems-an axially loaded pile and a shaking table test-involving the interface behavior for pile and the liquefaction for shake table. A new and highly efficient method is used to determine the liquefaction in saturated materials. This method is based on the changing microstructure of the material and allows identification of liquefaction based on the critical disturbance, Dc which is the point where the curvature of the disturbance function is the minimum. Based on the results of this research, it can be stated that the DSC model is capable of characterizing the cyclic behavior of saturated sands and interfaces and the liquefaction instability under dynamic and earthquake loading.
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29

Yi, Jun 1959. "Stress compatible bimaterial interface elements with application to transient dynamic stress analysis." Thesis, McGill University, 1994. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=22842.

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Conventional displacement-based finite element programs do not yield unique values of stress components which ought to be continuous at element interfaces. The errors, being the differences from the correct unique values, become unacceptably large at a bimaterial interface when the moduli of the two materials are significantly different.
This thesis formulates and implements new finite elements for obtaining the correct values of the stress components, both continuous and discontinuous ones, at bimaterial interface points under general dynamic loading, assuming linear, isotropic, elastic material behaviour.
The constructed finite elements programs, suitable for analyzing two-dimensional and axisymmetric three-dimensional problems, have been validated by comparing the predicted responses with the exact analytical solutions of some non-trivial impact loading (wave-propagation) problems.
The work provides a necessary tool for analyzing and designing composite structures, for example prosthetic knee and hip joints in the biomechanics field.
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30

Barut, Atila 1966. "Nonlinear thermo-mechanical analysis of stiffened composite laminates by a new finite element." Diss., The University of Arizona, 1998. http://hdl.handle.net/10150/282754.

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A new stiffened shell element combining shallow beam and shallow shell elements is developed for geometrically nonlinear analysis of stiffened composite laminates under thermal and/or mechanical loading. The formulation of this element is based on the principal of virtual displacements in conjunction with the co-rotational form of the total Lagrangian description of motion. In the finite element formulation, both the shell and the beam (stiffener) elements account for transverse shear deformations and material anisotropy. The cross-section of the stiffener (beam) can be arbitrary in geometry and lamination. In order to combine the stiffener with the shell element, constraint conditions are applied to the displacement and rotation fields of the stiffener. These constraint conditions ensure that the cross-section of the stiffener remains co-planar with the shell section after deformation. The resulting expressions for the displacement and rotation fields of the stiffener involve only the nodal unknowns of the shell element, thus reducing the total number of degrees of freedom. Also, the discretization of the entire stiffened shell structure becomes more flexible.
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31

Harrell, Timothy M. "Application of Groebner bases to geometrically nonlinear analysis of axisymmetric circular isotropic plates." Thesis, Tennessee Technological University, 2014. http://pqdtopen.proquest.com/#viewpdf?dispub=1567200.

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This thesis demonstrates a new application of Groebner basis by finding an analytical solution to geometrically nonlinear axisymmetric isotropic circular plates. Because technology is becoming capable of creating materials that can perform materially in the linear elastic range while experiencing large deformation geometrically, more accurate models must be used to ensure the model will result in realistic representations of the structure. As a result, the governing equations have a highly nonlinear and coupled nature. Many of these nonlinear problems are solved numerically. Since analytic solutions are unavailable or limited to only a few simplified cases, their analysis has remained a challenging problem in the engineering community.

On the other hand, with the increasing computing capability in recent years, the application of Groebner basis can be seen in many areas of mathematics and science. However, its use in engineering mechanics has not been utilized to its full potential. The focus of this thesis is to introduce this methodology as a powerful and feasible tool in the analysis of geometrically nonlinear plate problems to find the closed form solutions for displacement, stress, moment, and transverse shearing force in the three cases defined in Chapter 4.

The procedure to determine the closed form solutions developed in the current study can be summarized as follows: 1) the von Kármán plate theory is used to generate nonlinear governing equations, 2) the method of minimum total potential energy combined with the Ritz methodology converts the governing equations into a system of nonlinear and coupled algebraic equations, 3) and Groebner Basis is employed to decouple the algebraic equations to find analytic solutions in terms of the material and geometric parameters of the plate. Maple 13 is used to compute the Groebner basis. Some examples of Maple worksheets and ANSYS log files for the current study are documented in the thesis.

The results of the present analysis indicate that nonlinear effects for the plates subjected to larger deformation are significant for predicting the deflections and stresses in the plates and necessary compared to those based on the linear assumptions. The analysis presented in the thesis further shows the potential of the Groebner basis methodology combined with the methods of Ritz, Galerkin, and similar approximation methods of weighted residuals which may provide a useful procedure of analysis to other nonlinear problems and a basis of preliminary design in engineering practice.

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32

Woo, Zhong-Zheng. "Dynamic analysis for nonlinear materials including strain-softening." Diss., The University of Arizona, 1991. http://hdl.handle.net/10150/185388.

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The implementation of the δ₀₊ᵣ model in a finite element program is discussed. The idea of considering damage as a structural performance helps to avoid singularity. Strategies in drift correction is considered. The generalized time finite element method (GTFEM) is also discussed and implemented. It shows improved accuracy and stability with highly non-linear material properties.
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33

Hu, Kai Xiong. "Stress and fracture analysis for systems with inhomogeneities." Diss., The University of Arizona, 1993. http://hdl.handle.net/10150/186588.

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The inhomogeneities situated in materials render the diversification of composite families, and can provide synergistic effects for tailoring materials to a specified and often hostile environment. The work presented here focuses on the fracture and stress analysis of systems with various inhomogeneities. In Chapter 1, interactions among cracks and rigid-line inclusions are investigated. Rigid-line inclusions are represented by a distribution of forces while cracks are modeled by the standard dislocation approach. Chapter 2 presents an analysis of composite systems with interacting cracks and a dilute distribution of inclusions. A damage analysis procedure is developed to evaluate the effective properties of such composites. Chapter 3 examines multiple void-crack interactions. The formulation is based on a mixture of dislocations and tractions. Chapter 4 presents an approach to modeling bridged crack systems. A fully regular integral equation formulation is developed and the approach is ideally suited for the analysis of systems with large number of closely spaced inhomogeneities. The integral equations of different forms, developed throughout the dissertation can also be utilized to evaluate and verify various micromechanical models. The possible future extensions and the major limitations of the present work are briefly discussed in Chapter 5.
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34

Sarker, Pratik. "Investigation of the Quenching Characteristics of Steel Components by Static and Dynamic Analyses." ScholarWorks@UNO, 2014. http://scholarworks.uno.edu/td/1942.

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Machine components made of steel are subjected to heat treatment processes for improving mechanical properties in order to enhance product life and is usually done by quenching. During quenching, heat is transferred rapidly from the hot metal component to the quenchant and that rapid temperature drop induces phase transformation in the metal component. As a result, quenching generates some residual stresses and deformations in the material. Therefore, to estimate the temperature distribution, residual stress, and deformation computationally; three-dimensional finite element models are developed for two different steel components – a spur gear and a circular tube by a static and a dynamic quenching analyses, respectively. The time-varying nodal temperature distributions in both models are observed and the critical regions are identified. The variations of stress and deformation after quenching along different pathways for both models are studied. The convergence for both models is checked and validations of the models are done.
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35

Vionnet, Carlos Alberto. "Analysis of lubricant flows within the microgap of rotary lip seals." Diss., The University of Arizona, 1993. http://hdl.handle.net/10150/186465.

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The study of a thin, incompressible Newtonian fluid layer trapped between two almost parallel, sliding surfaces has been actively pursued in the last decades. This subject includes lubrication applications such as slider bearings or the sealing of non-pressurized fluids with rotary lip seals. When a viscous lubricant flows between an elastic body and a rigid surface, the contact geometry may undergo substantial deformation affecting the flow field of the lubricant. Therefore, a coupled model between an elastic ring and the fluid film underneath it is proposed. Initially, a linear stability analysis is performed. Then, non-linear calculations are presented showing that the system deformations are able to induce mixing of lubricant throughout the sealed region. In the second part of this work, the flow of lubricant fluid through the micro-gap of rotary lip seals is analyzed theoretically and numerically from a different perspective. The study is carried out assuming that a 'small-gap' parameter δ attains an extreme value in the Navier-Stokes equations. The precise meaning of small-gap is achieved by the limit δ = 0, and the numerical solution of the resulting set of equations predicts transport of lubricant through the contact region due to centrifugal instabilities. Numerical results obtained with the finite element method are presented. In particular, the influence of inflow and outflow boundary conditions, and their importance in the simulated flow are discussed. To this aim, the penalty method for incompressible flows in presence of variable body forces is re-examined with the help of well-known examples, yielding a corrected formulation that is more accurate and faster than standard finite element methods found in the literature.
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36

Hong, Tayo Steve. "Analysis and fabrication of paraboloidal CFRP sandwich mirrors." Diss., The University of Arizona, 1991. http://hdl.handle.net/10150/185587.

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The low areal weight requirements of telescopes in aerospace applications has driven the study on composite mirrors for several years. For example, the primary parabolic mirror in a balloon-borne, Cassegrain telescope required an optical quality better than 30 microns in figure RMS error. A parametric study on composite sandwich mirrors was conducted by using finite element analysis as well as optical analysis. The factors covered the cell sizes, core materials, core thicknesses, face layups, and support configurations. Based on theoretical calculations, many high quality spherical composite sandwich mirrors were generated by using a non-heat curing process. The CFRP faces and Nomex core were chosen as the baseline materials for mirror fabrication due to their high strength and low weight. The proposed replication method applied an interface layer between face and surface coat to eliminate print-through problems. Many important goals have been realized in those mirror samples with optical laser interferometer testing. These include the figure RMS error less than 2 microns and the surface RMS error less than 0.05 micron. The areal weights of the mirror samples are less than 7 kg/m². The thermal stability of these mirrors was observed from the optical results with thermal cycling tests. The proposed 2-meter parabolic composite sandwich mirror, with an areal weight of less than 10 kg/m², would consist of either [0/90/45/-45](s) layup faces with an optimal 3'' core or (QC) layup faces with a total core thickness of 5 inches. Both a ring support around the equator and the 18-point Hindle-type support would lead to the best optical quality under both self weight and thermal loading.
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37

Lustig, Steven K. "Microstructural analysis of finite deformation in FCC polycrystals." Thesis, Georgia Institute of Technology, 1995. http://hdl.handle.net/1853/15916.

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38

Zhao, Zhengwei 1962. "Reliability analysis of fatigue under random loading considering modeling updating through inspection in the MARTA bridge system." Thesis, The University of Arizona, 1991. http://hdl.handle.net/10150/278070.

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Plan for the fatigue damage evaluation of the full-penetration butt welds bridges requires the development of reliability-based analysis, inspection and maintenance procedure. To account for the uncertainties in the material properties and environmental conditions, a stochastic fatigue crack growth model is proposed here. Recent calculations using the Monte-Carlo Simulation technique shows that the first-order reliability method gives very accurate result. The sensitivity and capability of ultrasonic inspection are investigated in this study. The reliability of inspections for various events is formulated. Efficient algorithms for updating the reliability model through inspection are proposed. A case study is conducted for MARTRA's steel bridges system. Analysis of results includes fatigue reliability index, inspection, repair, updating of random variables and inspection plan. Results indicate the proposed model gives an accurate and practical approach to the fatigue control in the steel structures.
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39

Ngwangwa, Harry Magadhlela. "Assessment of structural damage using operational time responses." Pretoria : [s.n.], 2004. http://upetd.up.ac.za/thesis/available/etd-01312006-141711.

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40

Lacy, Thomas E. Jr. "Distribution effects in damage mechanics." Diss., Georgia Institute of Technology, 1998. http://hdl.handle.net/1853/15937.

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41

Torng, Tony Yi. "Reliability analysis of maintained structural system vulnerable to fatigue and fracture." Diss., The University of Arizona, 1989. http://hdl.handle.net/10150/184955.

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Metallic structures dominated by tensile loads are vulnerable to fatigue and fracture. Fatigue is produced by oscillatory loads. Quasi-static brittle or ductile fracture can result from a "large" load in the random sequence. Moreover, a fatigue or fracture failure in a member of a redundant structure produces impulsive redistributed loads to the intact members. These transient loads could produce a sequence of failures resulting in progressive collapse of the system. Fatigue and fracture design factors are subject to considerable uncertainty. Therefore, a probabilistic approach, which includes a system reliability assessment, is appropriate for design purposes. But system reliability can be improved by a maintenance program of periodic inspection with repair and/or replacement of damaged members. However, a maintenance program can be expensive. The ultimate goal of the engineer is to specify a design, inspection, and repair strategy to minimize life cycle costs. The fatigue/fracture reliability and maintainability (FRM) process for redundant structure can be a complicated random process. The structural model considered series, parallel, and parallel/series systems of elements. Applied to the system are fatigue loads including mean stress, an extreme load, as well as impulsive loads in parallel member systems. The failure modes are fatigue, brittle and ductile fracture. A refined fatigue model is employed which includes both the crack initiation and propagation phases. The FRM process cannot be solved easily using recently developed advanced structural reliability techniques. A "hybrid" simulation method which combines modified importance sampling (MIS) with inflated stress extrapolation (ISE) is proposed. MIS and ISE methods are developed and demonstrated using numerous examples which include series, parallel and series/parallel systems. Not only reasonable estimates of the probability of system failure but also an estimate of the distribution of time to system failure can be obtained. The time to failure distribution can be used to estimate the reliability function, hazard function, conditional reliability given survival at any time, etc. The demonstration cases illustrate how reliability of a system having given material properties is influenced by the number of series and parallel elements, stress level, mean stress, and various inspection/repair policies.
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42

Pipkins, Daniel Scott. "Non-linear analysis of (i) wave propagation using transform methods and (ii) plates and shells using integral equations." Diss., Georgia Institute of Technology, 1992. http://hdl.handle.net/1853/20052.

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43

Wu, Jian Si. "Review and analysis on the influences of different factors on the shear strength of soil-structural interface." Thesis, University of Macau, 2018. http://umaclib3.umac.mo/record=b3950675.

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44

Svensson, Marcus. "Selection of a product component for topology optimization and additive manufacturing." Thesis, Jönköping University, JTH, Industriell produktutveckling, produktion och design, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:hj:diva-52791.

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This is a master thesis research on how to select the right components in a product, considering reducing the weight with topology optimization (TO) and adaption for additive manufacturing (AM). It is well established that manufacturing of complex structures can be achieved with AM, the possibility of integrating assembled components and improve features will therefore be investigated. The new component structure must still withstand the loads that it is subjected to during usage, to not permanently deform or break. In this research the studied product was a handheld Husqvarna chainsaw. Initially a feasibility study was conducted, where the product was disassembled and physically investigated for potential component cases. Additional knowledge was gathered with one semi structured interview per case, with experienced design engineers. Followed by one semi structured interview with AM experts, regarding available AM technique and similar material. Selection of case to continue with was based on the interviews information and Pughs decision matrix, with weighted criterions. TO were used for finding the optimal material distribution. The new component design was analyzed with linear finite element analysis to fulfill both the component and material stress requirements. Component orientation and support structure for AM was analyzed with computer aided engineering software. This resulted with integrating thirteen components for the engines cylinder into one component. The new design resulted in a weight reduction of 31%, while utilizing only 57% of the allowed stress limit. Also, the first 23 natural frequencies were improved with a new type of cooling fin structure, with an increased area of 15%. These results encourage the thesis workflow methodology usage for other products. In conclusion the established workflow of methods resulted in selecting a suitable case for integrating components with feature improvement and adaption of the new design with TO for AM, to reduce the weight.
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45

Liu, Yu. "The development of a systematic experimental method for damage identification." Thesis, This resource online, 1993. http://scholar.lib.vt.edu/theses/available/etd-06112009-063906/.

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46

Brookes, Briana O. "Load ratings using an in-service bridge monitoring system." Access to citation, abstract and download form provided by ProQuest Information and Learning Company; downloadable PDF file, 121 p, 2007. http://proquest.umi.com/pqdweb?did=1338919131&sid=4&Fmt=2&clientId=8331&RQT=309&VName=PQD.

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47

Katsanis, George R. Mr. "Transient Small Wind Turbine Tower Structural Analysis with Coupled Rotor Dynamic Interaction." DigitalCommons@CalPoly, 2013. https://digitalcommons.calpoly.edu/theses/960.

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Structural dynamics is at the center of wind turbine tower design - excessive vibrations can be caused by a wide range of environmental and mechanical sources and can lead to reduced component life due to fatigue, noise, and impaired public perception of system integrity. Furthermore, periodic turbulent wind conditions can cause system resonance resulting in significantly increased structural loads. Structural vibration issues may become exacerbated in small wind applications where the analytical and experimental resources for system verification and optimization are scarce. This study combines several structural analysis techniques and packages them into a novel and integrated form that can be readily used by the small wind community/designer to gain insight into tower/rotor dynamic interaction, system modal characteristics, and to optimize the design for reduced tower loads and cost. The finite element method is used to model the tower structure and can accommodate various configurations including fixed monopole towers, guy-wire supported towers, and gin-pole and strut supported towers. The turbine rotor is modeled using the Equivalent Hinge-Offset blade model and coupled to the tower structure through the use of Lagrange’s Equations. Standard IEC Aeroelastic load cases are evaluated and transient solutions developed using the Modal Superposition Method and Runge-Kutta 4th order numerical integration. Validation is performed through comparisons to theoretical closed form solutions, physical laboratory test results, and peer studies. Finally a case study is performed by using the tool to simulate the Cal Poly Wind Power Research Center Wind Turbine and Tower System. Included in the case study is an optimization for hypothetical guy-wire placement to minimize tower stresses and maximize the tower’s natural frequency.
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48

Warren, Joel Christian. "Structural Design Solver Development for Overhead Industrial Cranes: Equations-Of-State Solver Method." Case Western Reserve University School of Graduate Studies / OhioLINK, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=case1328021324.

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49

Leonard, Kevin Raymond. "Ultrasonic guided wave tomography of pipes: A development of new techniques for the nondestructive evaluation of cylindrical geometries and guided wave multi-mode analysis." W&M ScholarWorks, 2004. https://scholarworks.wm.edu/etd/1539616737.

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Abstract:
This dissertation concentrates on the development of two new tomographic techniques that enable wide-area inspection of pipe-like structures. By envisioning a pipe as a plate wrapped around upon itself, the previous Lamb Wave Tomography (LWT) techniques are adapted to cylindrical structures. Helical Ultrasound Tomography (HUT) uses Lamb-like guided wave modes transmitted and received by two circumferential arrays in a single crosshole geometry. Meridional Ultrasound Tomography (MUT) creates the same crosshole geometry with a linear array of transducers along the axis of the cylinder. However, even though these new scanning geometries are similar to plates, additional complexities arise because they are cylindrical structures. First, because it is a single crosshole geometry, the wave vector coverage is poorer than in the full LWT system. Second, since waves can travel in both directions around the circumference of the pipe, modes can also constructively and destructively interfere with each other. These complexities necessitate improved signal processing algorithms to produce accurate and unambiguous tomographic reconstructions. Consequently, this work also describes a new algorithm for improving the extraction of multi-mode arrivals from guided wave signals. Previous work has relied solely on the first arriving mode for the time-of-flight measurements. In order to improve the LWT, HUT and MUT systems reconstructions, improved signal processing methods are needed to extract information about the arrival times of the later arriving modes. Because each mode has different through-thickness displacement values, they are sensitive to different types of flaws, and the information gained from the multi-mode analysis improves understanding of the structural integrity of the inspected material. Both tomographic frequency compounding and mode sorting algorithms are introduced. It is also shown that each of these methods improve the reconstructed images both qualitatively and quantitatively.
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50

Sundberg, Lars Andreas. "Analysis of welded reinforcements on a boom mower : A structural and modal analysis of reinforcement properties on a industrial boom mower." Thesis, Umeå universitet, Institutionen för tillämpad fysik och elektronik, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-148593.

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Abstract:
Road safety is a complicated issue that affects most world economies due to its negative socioeconomic impact. Road safety programs include different programs that cover different areas for minimizing the effects of these impacts. One of these programs focuses road safety against invasion of wildlife into traffic roads. Most economies that heavily include these particular programs, such as Sweden, rely on specific machinery and techniques for clearing road shoulders that allows driver to foresee any possible danger or road invasion in good time. The most common piece of machinery used for covering this type of activity is known as a boom mower. Boom mowers can be pictured as giant lawnmowers that are attached into a long boom crane from wheel loaders or excavators, so they can clear invading vegetation from the road shoulders. Boom mowers suffer from heavy wear due to their dimensions, weight and operating speed which it requires companies to pay extra attention to their construction and choice of materials. Cranab Slagkraft is a Swedish company that has been specialized for providing high quality boom mowers for the last 30 yearsfor clearing vegetation on the Swedish roads. But, despite their higher quality products, these boo mowers are often expensive and complicated to manufacture. For this reason, Cranab has requested a study to minimize the manufacturing burden in order to simplify its production and diminish cost. This research study focuses on the latest components addition into the boom mower construction to assess their performance. For this research, the researcher will put to test the reinforcements of the boom mower’s model SH150 and see what their performance against harmonic vibrations and structural strength against local stresses are. The research follows two complementary analysis. First, a modal analysis on the boom mower’s main structure for evaluating resonance levels at an operating frequency. Second, a structural analysis with idealized conditions at operating speed to determine construction stress resilience. The results in this research reveals that the modal analysis rejects the viability of one group of reinforcements and confirms the implications of the other one. Also, the results reveal that the complicated geometry requires advanced software for providing more conclusive results. In addition, the boom mower’s own geometry and choice of material might play a role in adjusting the harmonic resonance and adjusting the boom mower’s mechanical properties. The latter conclusion should be considered as a theme of study for future research in this same field.
Trafiksäkerhet är ett komplicerat ärende som påverkar de flesta världsekonomier på grund av dess negativa socioekonomiska inverkan. I trafiksäkerhetsprogrammen ingår olika program som täcker olika områden för att minimera de socioekonomiska effekterna. Ett av dessa program koncentrerar sig på trafiksäkerhet mot invasion av vilda djur på motorbanor. De flesta världsekonomiers system som omfattar dessa trafiksäkerhetsprogram, till exempel Sverige, är beroende av specifika maskiner och tekniker för röjning av vägarna som gör det möjligt för föraren att i god tid ska kunna förutse eventuell fara eller vilt som kommer in på vägen. Den vanligaste maskinen som används för röjning av vägar kallas kättingröjare. Kättingröjaren kan liknas vid gigantiska gräsklippare som är fastsatta på en grävmaskin, hjullastare och/eller väghyvel så att de kan rensa bort gräs från vägkanten. Kättingröjare lider av kraftigt slitage på grund av deras dimensioner, vikt och driftshastighet. Det kräver att tillverkaren uppmärksammar konstruktionen och materialvalet till kättingröjaren. Cranab Slagkraft är ett svenskt företag som under de senaste 30 åren har specialiserat sig på att leverera högkvalitativa kättingröjare. Kättingröjarna är ofta dyra och komplicerade att tillverka. Av den anledningen har Cranab begärt en studie för att förenkla produktionen och minska tillverkningskostnaderna. Den här studien koncentrerar sig på det senaste komponenttillägget i kättingröjarens konstruktion för att bedöma deras prestanda. I den här studien testas flera förstärkningar i kättingröjarens modell SH150 för att undersöka deras prestanda mot harmonisk vibration och strukturell hållfasthet mot lokala spänningar. I studien ingår två kompletterande analyser. Först görs en modalanalys på kättingröjarens huvudstruktur för utvärdering av resonansnivåer vid driftsfrekvensen. Sedan görs en strukturell analys med idealiserat tillstånd vid driftshastigheten för att bestämma spänningsmotståndet. I resultatet beskrivs en grupp av förstärkningar som inte har någon påverkan för kättingröjarens harmoniska vibration och spänningsmotstånd och en andra grupp som visar påverkan. Även resultaten visar att den komplicerade geometrin kräver avancerad mjukvara för att ge mer avgörande resultat. Dessutom kan kättingröjarens egen geometri och materialval ha påverkan vid justering av dess harmoniska resonans och mekaniska egenskaper. Den senare slutsatsen bör betraktas som ett begrepp för framtida studier inom samma område.
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