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Relevant bibliographies by topics / Aerospace material / Dissertations / Theses

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Dissertations / Theses on the topic 'Aerospace material'

Author: Grafiati

Published: 4 June 2021

Last updated: 10 February 2022

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1

Jenett, Benjamin (Benjamin Eric). "Digital material aerospace structures." Thesis, Massachusetts Institute of Technology, 2015. http://hdl.handle.net/1721.1/101837.

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Thesis: S.M., Massachusetts Institute of Technology, Department of Civil and Environmental Engineering, 2015.<br>Cataloged from PDF version of thesis.<br>Includes bibliographical references (pages 71-76).<br>This thesis explores the design, fabrication, and performance of digital materials in aerospace structures in three areas: (1) a morphing wing design that adjusts its form to respond to different behavioral requirements; (2) an automated assembly method for truss column structures; and (3) an analysis of the payload and structural performance requirements of space structure elements made f

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2

Jönsson, Gustav. "Material selection for an aerospace component." Thesis, KTH, Lättkonstruktioner, 2015. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-198494.

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In the world of today there is a drive for lighter and more effective products for various reasons e.g. reduced environmental impact, higher payload, fuel efficiency etc. There is also an expanding development of new materials for a large number of different applications. This makes it more and more difficult for engineers to make good material selections. This has led to the development of a large amount of material selection methods that require more or less effort to select material. An effective way to do this is offered by utilisation of material selection software’s like Granta Design CE

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3

Anderson, Mélissa. "Tube hydroforming of aerospace alloys : material characterization methods." Mémoire, École de technologie supérieure, 2010. http://espace.etsmtl.ca/625/1/ANDERSON_M%C3%A9lissa.pdf.

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L'objectif du projet est de développer des outils de modélisation de procédé pour la fabrication virtuelle de composants aéronautiques par hydroformage de tubes. L'industrie aérospatiale s'intéresse aux possibilités qu'offre la technologie d'hydroformage pour la fabrication de pièces aéronautiques. Dans ce contexte, les travaux menés portent sur la mise en place de méthodes appropriées pour caractériser certains alliages aéronautiques: les aciers inoxydables 321, 17-4 PH ainsi que le superalliage base-nickel Inconel 718. Le présent travail cherche à comprendre le comportement mécanique d

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4

Pan, Qing. "Multi-scale modelling and material characterisation of textile composites for aerospace applications." Thesis, University of Nottingham, 2016. http://eprints.nottingham.ac.uk/33396/.

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Textile composites offer an excellent alternative to metallic alloys in the aerospace engineering due to their high specific stiffness and strength, superb fatigue strength, excellent corrosion resistance and dimensional stability. In order to successfully apply these materials to engineering problems, a methodology to characterise and predict the constitutive response of these materials is essential. The lack of the modelling tools for modern textile composites that would facilitate systematic analysis and characterisation of these materials hinders the wide adoption of such material systems

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5

Munoz, Raul E. "Finite element modelling (including material grain refinement prediction) when turning advanced aerospace alloys." Thesis, University of Birmingham, 2015. http://etheses.bham.ac.uk//id/eprint/5844/.

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The overall aim of the project/research was to develop finite element modelling/process simulation capability to predict workpiece surface integrity following machining of advanced aerospace alloys. The modelling work employed the general-purpose commercial finite element (FE) software ABAQUS, due to its robust solver for handling complex, dynamic non-linear problems as well as the facility to define custom algorithms/subroutines. Both 2D and 3D fully coupled thermo-mechanical FE models were formulated to simulate the orthogonal turning of Ti-6Al-4V titanium alloy and Inconel 718 nickel based

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6

Purzer, Nicholas R. (Nicholas Richard) 1972. "Managing the supply, release, and machining of material within an aerospace component shop." Thesis, Massachusetts Institute of Technology, 1998. http://hdl.handle.net/1721.1/50444.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering; and, (S.M.)--Massachusetts Institute of Technology, Sloan School of Management, 1998.<br>Includes bibliographical references (p. 69).<br>by Nicholas R. Purzer.<br>S.M.

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7

Zhang, Tao. "The Effects of Ball Burnishing for Aerospace Blade Material 17-4 PH Steel." University of Toledo / OhioLINK, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=toledo1384971374.

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8

Perry, Mark Joseph. "Analysis of resin transfer molding: Material characterization, molding and simulation /." The Ohio State University, 1993. http://rave.ohiolink.edu/etdc/view?acc_num=osu1382637062.

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9

Anokye-Siribor, Kwame. "An analytical model for pressbrake forming using in-process identification of aerospace material characteristics." Thesis, University of Ulster, 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.298630.

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10

Wilson, Andrew David. "Wear and fatigue studies of surface engineered ferrous and non-ferrous aerospace alloys." Thesis, University of Hull, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.264952.

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11

YI, WEITAO. "MICROMECHANICS BASED COMPOSITE MATERIAL MODELS FOR CRASHWORTHINESS FINITE ELEMENT SIUMLATION." University of Cincinnati / OhioLINK, 2001. http://rave.ohiolink.edu/etdc/view?acc_num=ucin990541929.

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12

Forconi, Mattia. "Experimental analysis of a hybrid composite material." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2017.

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The main aim of this thesis is to investigate the mechanical properties of a hybrid composite material under static loadings. The material is a composite laminate made by layers of carbon bars and a rubber layer. The thesis can be split into three main parts. In the first part a background about carbon bar composite is given and, subsequently, the research and main results on hybrid composites is introduced. The objective of this section is to provide a base on which built the main results of this work. In the second part it is explained how the test activities have been performed and the main

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13

Beji, Faycel Ben Hedi. "Buckling Analysis of Composite Stiffened Panels and Shells in Aerospace Structure." Thesis, Virginia Tech, 2018. http://hdl.handle.net/10919/81620.

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Stiffeners attached to composite panels and shells may significantly increase the overall buckling load of the resultant stiffened structure. Initially, an extensive literature review was conducted over the past ten years of published work wherein research was conducted on grid stiffened composite structures and stiffened panels, due to their applications in weight sensitive structures. Failure modes identified in the literature had been addressed and divided into a few categories including: buckling of the skin between stiffeners, stiffener crippling and overall buckling. Different methods ha

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14

Hoover, Luke Daniel. "Large Strain Plastic Deformation of Traditionally Processed and Additively Manufactured Aerospace Metals." University of Dayton / OhioLINK, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1627570139729633.

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15

Gunel, Murat. "Linear And Nonlinear Progressive Failure Analysis Of Laminated Composite Aerospace Structures." Master's thesis, METU, 2011. http://etd.lib.metu.edu.tr/upload/12614033/index.pdf.

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This thesis presents a finite element method based comparative study of linear and geometrically non-linear progressive failure analysis of thin walled composite aerospace structures, which are typically subjected to combined in-plane and out-of-plane loadings. Different ply and constituent based failure criteria and material property degradation schemes have been included in a PCL code to be executed in MSC Nastran. As case studies, progressive failure analyses of sample composite laminates with cut-outs under combined loading are executed to study the effect of geometric non-linearity on the

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16

Li, Jianing. "Characterization of a Novel Porous Injector for Multi-Lean Direct Injection (M-LDI) Combustor." University of Cincinnati / OhioLINK, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1530269081550143.

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17

Gordon, Neal A. "Material Health Monitoring of SIC/SIC Laminated Ceramic Matrix Composites With Acoustic Emission And Electrical Resistance." University of Akron / OhioLINK, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=akron1414835900.

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18

Dhakal, Binod. "Characterization of a 3D Multi-Mechanism SMA Material Model for the Prediction of the Cyclic "Evolutionary" Response of NiTi for Use in Actuations." University of Akron / OhioLINK, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=akron1384506213.

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19

Carter, Justin B. "Vibration and Aeroelastic Prediction of Multi-Material Structures based on 3D-Printed Viscoelastic Polymers." Miami University / OhioLINK, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=miami1627048967306654.

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20

DRENSKY, GEORGE K. "EXPERIMENTAL INVESTIGATION OF COMPOSITE MATERIAL EROSION CHARACTERISTICS UNDER CONDITIONS ENCOUNTERED IN TURBOFAN ENGINES." University of Cincinnati / OhioLINK, 2007. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1178118863.

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21

Ananth, Sirija. "Stability Analysis of Additively Manufactured Isogrid." University of Dayton / OhioLINK, 2015. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1449850405.

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22

Amarchinta, Hemanth. "Uncertainty Quantification of Residual Stresses Induced By Laser Peening Simulation." Wright State University / OhioLINK, 2010. http://rave.ohiolink.edu/etdc/view?acc_num=wright1278028187.

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23

Nastic, Aleksandra. "Repair of Aluminum Alloy Aerospace Components and Cold Gas Dynamic Spray Flow Distribution Study." Thesis, Université d'Ottawa / University of Ottawa, 2015. http://hdl.handle.net/10393/32998.

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Aluminum alloys have been used for decades in aircraft as they offer a wide range of properties explicitly developed to provide a set of characteristics adapted to structural and non-structural components. However, aircraft components inevitably undergo degradation during service due to their extensive use and exposure to harsh environments. Typical repair methods are either not efficient for large scale repairs due to their low material growth rate, not suitable for field repair or involve the use of high process temperatures. The present research aims at evaluating the cold gas dynamic spray

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24

Owusu-Danquah, Josiah Sam Owusu-Danquah. "MODELING AND CHARACTERIZATION OF A GENERAL MULTIMECHANISM MATERIAL MODEL FOR ADVANCED ENGINEERING APPLICATIONS OF SHAPE MEMORY ALLOYS." University of Akron / OhioLINK, 2017. http://rave.ohiolink.edu/etdc/view?acc_num=akron149936399244747.

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25

Pangsrivinij, Suksant. "High Throughput Functional Material Deposition Using A Laser Hot Wire Process." Case Western Reserve University School of Graduate Studies / OhioLINK, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=case1464740037.

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26

Shang, Wei. "LABORATORY-SCALE EVALUATION OF ARAMID BLEND MATERIAL AS A FIRE BARRIER FOR FLEXIBLE POLYURETHANE FOAM." Case Western Reserve University School of Graduate Studies / OhioLINK, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=case1462873811.

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27

Tseng, Ya-Ting. "Three-Dimensional Model of Solid Ignition and Ignition Limit by a Non-Uniformly Distributed Radiant Heat Source." Case Western Reserve University School of Graduate Studies / OhioLINK, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=case1307551796.

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28

Goyal, Deepak. "Analysis of linear elasticity and non-linearity due to plasticity and material damage in woven and biaxial braided composites." [College Station, Tex. : Texas A&M University, 2007. http://hdl.handle.net/1969.1/ETD-TAMU-2405.

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29

Fulcher, Jared T. "A DESIGN PATHFINDER WITH MATERIAL CORRELATION POINTS FOR INFLATABLE SYSTEMS." UKnowledge, 2014. http://uknowledge.uky.edu/me_etds/39.

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The incorporation of inflatable structures into aerospace systems can produce significant advantages in stowed volume to mechanical effectiveness and overall weight. Many applications of these ultra-lightweight systems are designed to precisely control internal or external surfaces, or both, to achieve desired performance. The modeling of these structures becomes complex due to the material nonlinearities inherent to the majority of construction materials used in inflatable structures. Furthermore, accurately modeling the response and behavior of the interfacing boundaries that are common to m

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30

Kulkarni, Mandar Madhukar. "Prediction of Elastic Properties of a Carbon Nanotube Reinforced Fiber Polymeric Composite Material Using Cohesive Zone Modeling." University of Cincinnati / OhioLINK, 2009. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1235433423.

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31

Mummareddy, Bhargavi. "Additive Manufacturing Processes for High-Performance Ceramics: Manufacturing - Mechanical and Thermal property Relationship." Youngstown State University / OhioLINK, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=ysu1629131959379597.

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32

Ben, Aissia Hazem. "Model reduction for thermal management of high power electronic components for aerospace application." Thesis, Lyon, 2019. http://www.theses.fr/2019LYSEI071.

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Dans la transition vers l’avion plus électrique, un des verrous technologiques est l'échauffement des composants électroniques ce qui affecte fortement leurs fiabilités et leurs durées de vie. Par conséquence, il est nécessaire de contrôler la température des cartes électroniques. Cette thèse a pour objectif de construire deux modèles thermiques réduits permettant de suivre en temps réel la température des composants électroniques. La différence entre le modèle réduit directe (MRD) et le modèle réduit inverse (MRI) réside dans les paramètres d'entrée et le formalisme mathématique de leurs cons

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33

Brandl, Erhard [Verfasser]. "Microstructural and mechanical properties of additive manufactured titanium (Ti-6Al-4V) using wire : Evaluation with respect to additive processes using powder and aerospace material specifications / Erhard Brandl." Aachen : Shaker, 2010. http://d-nb.info/1081887001/34.

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34

Líkař, Martin. "Experimentální elektroerozivní obrábění speciálních materiálů pro letecký průmysl." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2020. http://www.nusl.cz/ntk/nusl-417096.

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This master´s thesis deals with the issues of electroerosive machining material used in aerospace industry. The master´s thesis is divided into the theoretical and practical part. In the theoretical part is described electroerosive machining with a focus on electrical discharge sinking. One section of the theoretical part is an analysis of materials used in the aerospace industry. The practical part of the master´s thesis is focused on electrical discharge sinking of aerospace material INCO 713LC, here is investigated the influence of machining parameters on the surface of the workpiece and to

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35

Montag, Benjamin W. "Lithiated ternary compounds for neutron detectors: material production and device characterization of lithium zinc phosphide and lithium zinc arsenide." Diss., Kansas State University, 2015. http://hdl.handle.net/2097/20415.

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Doctor of Philosophy<br>Mechanical and Nuclear Engineering<br>Douglas S. McGregor<br>There is a need for compact, rugged neutron detectors for a variety of applications including national security and oil well logging. A solid form neutron detector would have a higher efficiency than present day gas filled ³He and ¹⁰BF ₃ detectors, which are standards currently used in the industry today. A sub-branch of the III-V semiconductors is the filled tetrahedral compounds, known as Nowotny-Juza compounds (A[superscript I]B[superscript II]C[superscript V]). These materials are desirable for their cubic

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36

Holdren, Matthew C. "Capability Study of Lattice Frame Materials for Use as Recuperative Heat Exchangers in Aircraft Systems." Case Western Reserve University School of Graduate Studies / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=case1554463168699054.

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37

Delfa, G. L. a. "Aerospace composite materials in fire." Thesis, University of Newcastle Upon Tyne, 2010. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.519566.

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38

Sweeney, Benjamin Andrew. "The Effect of Biocomposite Material In A Composite Structure Under Compression Loading." DigitalCommons@CalPoly, 2017. https://digitalcommons.calpoly.edu/theses/1932.

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While composite structures exhibit exceptional strength and weight saving possibilities for engineering applications, sometimes their overall cost and/or material performance can limit their usage when compared to conventional structural materials. Meanwhile ‘biocomposites’, composite structures consisting of natural fibers (i.e. bamboo fibers), display higher cost efficiency and unique structural benefits such as ‘sustainability’. This analysis will determine if the integration of these two different types of composites are beneficial to the overall structure. Specifically, the structure will

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39

Subramanian, Rohit. "COMPUTATIONAL FRAMEWORK TO ASSESS ROLE OF MANUFACTURING IN MATERIAL-DEFECT RELATED FAILURE RISK." The Ohio State University, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=osu1398998282.

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40

Melendez, Alma. "A Study on the Vibrational Performance Characteristics of an E22 Isolator After Outgassing and Bake-out." DigitalCommons@CalPoly, 2014. https://digitalcommons.calpoly.edu/theses/1190.

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The launch environment experiences many vibration, shock, and acoustic loads. A great concern is the high random vibration levels that can damage components and spacecraft structures, which can cause a mission failure. An effective method of reducing high frequency energy is using isolators. Overall, the need for vibration isolation has been increasing because there has been an increase in the use of mechanisms in which vibrations are prevalent. In addition, there has not been extensive research on the effects of isolators that are outgassed and cured. Therefore, it is important to investigate

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41

Piccioni, Flavio. "Numerical Evaluation of Mode II Disbonding on Fiberglass CCPs-Specimens and Material Characterization Utilizing a Distributed Sensing Rayleigh Backscattering System." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2020. http://amslaurea.unibo.it/19848/.

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Nowadays, composite materials have become the main construction materials for aeronautical structures, replacing traditional materials commonly used in this industry. However, composite structures are still characterized by conservative designs due to the lack of understanding from a physics-based approach their damage propagation and failure mechanisms. Since repairs of composite structures are a crucial part of the long-term use of composites in aerospace, the stakeholders require an in depth understanding of the physics of disbonding in composites. The aim of this research is a numerical ev

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42

Singh, Harpal. "An Investigation of Material Properties and Tribological Performance of Magnetron Sputtered Thin Film Coatings." University of Akron / OhioLINK, 2015. http://rave.ohiolink.edu/etdc/view?acc_num=akron1449850005.

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43

Kudesia, Sean Swarup. "Precision Nd:YAG laser drilling of aerospace materials." Thesis, Heriot-Watt University, 2003. http://hdl.handle.net/10399/387.

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44

Shirley, Kevin Alexander. "Toward a Production Ready FBJ Process for Joining Dissimilar Combinations of GADP 1180 Steel and AA 7085-T76." BYU ScholarsArchive, 2018. https://scholarsarchive.byu.edu/etd/6694.

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Friction Bit Joining (FBJ) is a new technology that can be used to join dissimilar materials together. This ability makes it a good candidate for creating light weight structures for the automotive industry by combining lightweight materials such as aluminum to stronger materials like advanced high-strength steels. The automotive industry and many other industries have great interest in reducing structure weight to increase fuel efficiency. The purpose of this research is to make FBJ of GADP 1180 to AA 7085-T76 a production ready process by (1) better understanding the effects of process param

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45

Curran, John P. J. "A robotic cell for handling aerospace composite materials." Thesis, Queen's University Belfast, 1986. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.328705.

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46

Hu, Zhuopei. "Finite Element Modeling of Aerospace Materials and Structure." University of Akron / OhioLINK, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=akron1344224158.

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47

Zahn, Alexander R. "Characterization and Examination of Performance Parameters of a Back-pressurized RDC." University of Cincinnati / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1554119639742205.

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48

Wilson, James Alexander. "The microstructure of mechanically alloyed Ti-based aerospace materials." Thesis, University of Bristol, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.297971.

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49

Polimeno, Umberto. "Non linear spectroscopy for damage detection on aerospace materials." Thesis, University of Bath, 2010. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.535639.

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50

Xxx, Priyadarshini Jayashree. "Tribological Studies of Advanced Materials for Aerospace Braking Applications." Doctoral thesis, Università degli studi di Trento, 2021. http://hdl.handle.net/11572/296431.

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The most important and basic objective of aircraft operation is safe flying, which is achieved through the proper functioning of various components. Amongst these components, a lot of importance has been given to the tribological properties of brakes in an aircraft, as its failure could lead to catastrophic possibilities. The materials employed for these braking applications must satisfy a range of requirements like high stiffness, thermal and chemical stability, and most importantly deliver stable friction coefficient and high wear resistance. Amidst ever-developing technologies, the ne

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