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1
Kocer, Hasan Basri Broughton Roy. "Laminated and hybrid soft body armor for ballistic applications". Auburn, Ala., 2007. http://repo.lib.auburn.edu/2007%20Fall%20Theses/Kocer_Hasan_7.pdf.
Testo completo
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Sikkil, Kaarthik K. "Finite element damage modeling of plain weave fabrics". Morgantown, W. Va. : [West Virginia University Libraries], 2003. http://etd.wvu.edu/templates/showETD.cfm?recnum=3234.
Testo completoAbstract (sommario):
Thesis (M.S.)--West Virginia University, 2003.Title from document title page. Document formatted into pages; contains ix, 101 p. : ill. (some col.). Includes abstract. Includes bibliographical references (p. 83-85).
3
Ujjin, Rapee Mechanical & Manufacturing Engineering Faculty of Engineering UNSW. "Prediction of bearing failure in pin-loaded laminates". Awarded by:University of New South Wales. School of Mechanical and Manufacturing Engineering, 2007. http://handle.unsw.edu.au/1959.4/28197.
Testo completoAbstract (sommario):
This thesis presents the results of an investigation of bearing failure at a loaded hole in carbon fibre composite laminates. The investigation included finite element analysis and a program of experimental testing for quasi-isotropic laminates, uni-directional laminates and laminates with fibres steered along predefined trajectories. The investigation formed part of a research program in the Cooperative Research Centre for Advanced Composite Structures Ltd (CRC-ACS) support by the Office of Naval Research from the United States. Work in progress in the CRC includes research defined in this thesis including the addition of nano-particles to the resin to improve the bearing strength. The literature survey undertaken in this thesis identified that the micro-buckling theory proposed by Professor C.T. Sun from Purdue University, Indiana USA, is the best analysis procedure for initial bearing failure in pin-loaded laminates. This failure theory has therefore been implemented in a Fortran program using the results from a finite element analysis for the nonlinear contact problem of a pin bearing on a hole in a composite laminate. The finite element analysis is executed using the commercial finite element system MSC.MARC. The numerical predictions have been validated by a test of progressive failure with the aid of an acoustic emission monitoring system. The acoustic emission parametric and frequency analysis is performed using the acoustic emission software Vallen Systeme. Fast fourier transformation of the waveform have been achieved to distinguish and identify microfailure mode. Failure mechanisms have been verified by post-mortem microstructural examination. There are 3 failure mechanisms associated with bearing failure in carbon fibre reinforced epoxy composite, the first is fibre matrix interfacial failure, followed by fibre fracture, and subsequently matrix splitting. The application of AE technique has been applied successfully to characterise the development of failure.
4
Sarin, Siddartha. "Liquid transport mechanisms in cotton-polypropylene laminated nonwoven fabrics influencing pesticide penetration". Thesis, This resource online, 1994. http://scholar.lib.vt.edu/theses/available/etd-01102009-063449/.
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5
Pecku, Suven. "The use of thermoplastic starch for the modification of hydrophilic breathable membranes". Diss., Pretoria : [s.n.], 2009. http://upetd.up.ac.za/thesis/available/etd-06302009-175421/.
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Sutton, Corey R. "Characterization of Resistance Change in Stretchable Silver Ink Screen Printed on TPU-Laminated Fabrics Under Cyclic Tensile Loading". DigitalCommons@CalPoly, 2019. https://digitalcommons.calpoly.edu/theses/2089.
Testo completoAbstract (sommario):
A stretchable silver ink was screen printed to TPU sheets, then tensile coupons of the TPU, both bare and laminated to cotton, Denim and spandex fabric, were subjected to 1000 cycles of 20% uniaxial strain. In-situ resistance measurements of printed traces were processed to generate datasets of maximum and minimum resistance per cycle. A mechanistic fit model was used to predict the resistance behavior of the ink across TPU/fabric levels. The results show that traces strained on TPU laminated to spandex (polyester) fibers had an average rate of increase in resistance significantly lower than that of traces strained on bare TPU. The variation in predicted resistance was significantly lower in the spandex group than in the TPU group. Trace width was not found to have a significant effect on the resistance behavior across TPU/fabric groups. More testing is required to understand the effect of lamination to high elasticity fabrics on resistance behavior as it relates to the viscoelastic properties of the fibers and weave structure.
7
Dib, Wassim. "Comportement mécanique de tissus à voiles, en fibres synthétiques, sous sollicitations biaxiales et déformation finie". Thesis, Grenoble, 2014. http://www.theses.fr/2014GRENI006/document.
Testo completoAbstract (sommario):
Ce travail concerne l'étude théorique, expérimentale et numérique du comportement mécanique de matériaux tissés et de toiles laminées à base de fibres synthétiques, destinés à la fabrication des voiles, comme le polyester ou le Kevlar. Une approche théorique originale a été proposée ; elle permet une prise en compte du comportement spécifique des fils, de l'enduction et de leurs interactions. La modélisation, qui en résulte, permet de décrire le comportement biaxial des matériaux tissés et des toiles, en chargements cycliques complexes, avec une prise en compte des déformations finies, des effets visqueux non linéaires, de l'irréversibilité indépendante du temps et de l'anisotropie. Une mise en œuvre de cette modélisation a été effectuée dans un code d'Eléments Finis, afin de produire un outil opérationnel pour le calcul des voiles. L'approche théorique proposée a été validée grâce à une étude expérimentale détaillée, qui a été réalisée sur le Dacron SF HTP Plus. Ainsi, nous avons réalisé sur ce matériau différents essais de tractions monotones et de tractions ondulées, contrôlés en déformation et en force. Certains de ces essais comportent des séquences de relaxation. Ces essais ont été réalisés dans les axes du matériau, dans le sens chaîne ou dans le sens trame, ainsi qu'en hors axes avec des orientations par rapport à la direction chaîne allant de 5° à 45°. Des résultats expérimentaux complémentaires ont également été obtenus sur une toile laminée en Kevlar X15 et sur un Dacron SF HTM simple. Enfin, une simulation de l'essai de traction biaxiale a été réalisée et a permis d'étudier l'homogénéité des champs de contrainte et de déformation de trois formes d'éprouvette différentesThis work deals with theoretical, experimental and numerical studies of the mechanical behavior of woven materials and laminated fabrics, made with synthetic fibers, for the manufacture of sails, such as polyester or Kevlar. An original theoretical approach was proposed, it allows taking into account the specific behavior of yarns, of coating and their interactions. The resulting modeling allows describing the behavior of woven materials and laminated fabrics, in the case of complex cyclic biaxial loadings, taking into account finite deformations, nonlinear viscous effects, time-independent irreversibility and anisotropy. The implementation of this modeling was performed in a finite element code, in order to produce an operational tool for the design and calculation of sails. The proposed theoretical approach has been validated through a detailed experimental study, which was conducted on material “Dacron SF HTP Plus”. Thus, we performed various monotonous and cyclic tensile tests, which were strain or load-controlled. Some of these tests include relaxation sequences. These tests were conducted in the axes of the material, in the warp and weft directions, as well as off-axis or bias orientations, from 5 ° to 45 ° with respect to the warp direction. Further experimental results were also obtained on a laminated “Kevlar X15” and a woven “Dacron SF HTM simple” fabrics. Finally, numerical simulations of the biaxial tensile test were performed and were used for studying homogeneity of the stress and the strain fields in the cases of three different contours of biaxial-tensile samples
8
Belmonte, H. M. S. "Notched strength of woven fabric composites". Thesis, University of Surrey, 2002. http://epubs.surrey.ac.uk/774243/.
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Munden, Daniel Christopher. "Development of a Progressive Failure Model for Notched Woven Composite Laminates". Thesis, Virginia Tech, 2018. http://hdl.handle.net/10919/85058.
Testo completoAbstract (sommario):
As part of the Composite Technology for Exploration (CTE) project at NASA, woven fabric composites are being investigated for their use in Space Launch System (SLS) hardware. Composites are more difficult to analyze than isotropic materials and require more complex methods for predicting failure. NASA is seeking a method for predicting the damage initiation and propagation of woven fabric composites in order to utilize these materials effectively in SLS hardware. This work focuses on notched woven fabric composites under tensile loading. An analytical model consisting of a macro-level failure criterion and damage propagation was developed and implemented in explicit finite element analysis to simulate woven composite materials. Several failure criteria and propagation models were investigated and compared. A response surface was used to better understand the effects of damage parameters on the failure load of a specimen. The model chosen to have best represented the physical specimen used the Tsai-Wu failure criterion. Additional physical tests are needed to further validate the model.Master of Science
A composite material consists of two or more different materials that are joined together to form a new material with improved properties. Woven fabric composites weave strips of fibers and a bonding material into a pattern to increase the material’s ability to withstand loads in various directions. NASA is seeking a method to predict the conditions under which woven fabric composites will break. A greater understanding of the capabilities of woven fabric composites will help NASA improve the structures involved in space exploration. This work attempts to build an analytical model that can predict the loads under which a woven fabric composite will break in tension. Several different analytical theories were used to model a woven fabric composite and the results were compared with lab tests. One of the theories, the Tsai-Wu failure criterion, was selected as the best representation of the physical specimen. Further additional physical tests are necessary to further validate the analytical model.
10
Manger, Christopher I. C. "Failure of notched woven GFRP composites : damage analysis and strength modelling". Thesis, University of Surrey, 1999. http://epubs.surrey.ac.uk/738/.
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Döbrich, Oliver, Thomas Gereke, Olaf Diestel, Sybille Krzywinski e Chokri Cherif. "Decoupling the bending behavior and the membrane properties of finite shell elements for a correct description of the mechanical behavior of textiles with a laminate formulation". Sage, 2014. https://tud.qucosa.de/id/qucosa%3A35608.
Testo completoAbstract (sommario):
Drape simulation of textiles is a field of research, which is known in the clothing sector for a long time. The ongoing development of high-performance composites made of textile reinforcements and matrix materials focus the interests on a serial production in many industrial sectors, such as aviation and automotive industries. Challenges occur mainly in the serial production technologies and in supplying concepts for the preform architecture and shape. Research aims on the acceleration of preform manufacturing and the reduction of expensive pretests. Numerical simulation models can help to improve the composite development chain with structure and process simulation. A special challenge in drape modeling is the bending behavior of textiles. This study introduces a novel approach for modeling single textile layers as laminates to gain a correct mechanical behavior, where all deformation mechanisms are uncoupled. The implementation in the finite element software LS-DYNA® is described. An algorithm is introduced which provides the membrane stiffness for each layer of a laminate to fit the measured cantilever bending stiffness of textiles in every bending direction and bending side. The calculated parameters for the laminate formulation result in the requested bending stiffness for the textile layer. The cantilever bending stiffness can be used directly for dimensioning the model.
12
Bendzovski, Daniel. "Trend-sandwich : Exploring new ways of joining inspiration, such as different kinds of trends, through processes of morphing and melding different trendy garments and materials, for new methods, garment types, materials and expressions". Thesis, Högskolan i Borås, Akademin för textil, teknik och ekonomi, 2015. http://urn.kb.se/resolve?urn=urn:nbn:se:hb:diva-248.
Testo completoAbstract (sommario):
The aim of this work is to explore the joining of inspiration, such as different garments and materials, in relation to commonly used methods in the fashion industry when it comes to joining of different trends and references such as clashing and collaging. The work proposes a new method and framework for join- ing inspiration which generates different results depending on what kind of inspiration that is put in to it. A garment can roughly be broken down to a silhouette and shape, materials and details. The material put in to the method and framework is based on information from trend seminars for SS16, because that is how many of today’s trend-oriented fashion brands get there inspiration. Trendy garment silhouettes are mixed through processes of computational morphing in Adobe Flash by a generation of spin in the mixing process were shape hints are used in a new manner. The new generated silhouettes are further developed and materialized through procedures of interpretation and figuration. Different trendy materials are melded in a direct and concrete way through mixed media techniques such as laminating, fusing and vacuum-techniques. The final steps of the method is a garment shape and material synthesis with starting point in the generated shape with the final material. The projects intention is to let the physical experimentation, interpretation and figuration play a central role in the research process for new types of methods, garments, materials and expressive pos- sibilities.
13
Coignac, Bruno. "Lois d'écoulement et endommagement en chargement statique ou cyclique d'un multimatériau "composite (verre/epoxy)-cuivre" : Etude expérimentale et modelisation". Besançon, 1988. http://www.theses.fr/1988BESA2024.
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14
Rosario, Kirit Keith. "Quasi-three-dimensional woven composites". Diss., 2008.
Cerca il testo completoAbstract (sommario):
Thesis (M.S.)--Michigan State University. Dept. of Mechanical Engineering, 2008.Title from PDF t.p. (viewed on July 29, 2009) Includes bibliographical references (p. 108-110). Also issued in print.
15
Ma, Wen-Hsuan, e 馬文軒. "Evaluation of Manufacturing Process and Stab Resistance of TPU Laminated Composite Fabrics". Thesis, 2008. http://ndltd.ncl.edu.tw/handle/61529775865503535503.
Testo completoAbstract (sommario):
碩士逢甲大學
紡織工程所
96
With the progress of the science and technology and the society, people pay much more attention to their own safety which lead all kinds of personal protection apparatus to rapidly develop. Because the principles of penetrating resistance between a bullet and a hard sharp apparatus are different, the improvement of the ballistic resistant cloth in preventing stabbing of the hard sharp apparatus is very important. This study designed and manufactured the stabbing resistant fabrics to prevent the pricking damage of human body. In this study, the Kevlar unidirectional fabric (Kevlar UD fabric) and the woven fabric were laid into two layers polyamide (Nylon 6) webs respectively to form composite fabric by needle punching and thermal bonding. The optimal process condition was gained by evaluating the results of tensile strength test, constant-rate stab resistant test, and puncture resistant test of dropping weight. The performance of stab resistance was raised by laminated a film of thermal-plastic polyurethane. The experimental results show that the interfacial combination of laminated fabric is useful for composite fabric to increase the property of stab resistance. The stab resistant strength of composite fabric structure is better than the general high-performance laminated fabric. The stab resistant strength for composite fabric is increased about 25 %, while the cost is down around 30 %. The composite fabric has optimal stab resistant while the content of low melted-temperature staple fiber is 30%, the thermal bonding temperature is 150℃, the linear velocity of thermal calender is 0.5 m/min, and the needle-punched density is 200 needles/cm2.
16
Chen, Kuan-Hung, e 陳冠宏. "A Study on the Functional Properties of Laminated Fabrics through Polyurethane/ Zinc Oxide Pad Process". Thesis, 2011. http://ndltd.ncl.edu.tw/handle/apv4t5.
Testo completoAbstract (sommario):
碩士國立臺北科技大學
有機高分子研究所
99
This study is synthesized Polyurethane by prepolymer synthesis. Hard segment is made by 1,4-butane diols and 4, 4’-diphenylmethane diisocyanate, and soft segment is made by polytetramethylene glycol. Furthermore, added the ZnO powders to N,N-dimethyl acetamide, then mixed with PU during synthesis process. Finally, through the drying treatment in 60℃, and fabricate PU/ZnO composite materials.PET and PA 6 fabrics were treated by plasma in different seconds, and pick up with ZnO/PU and drying treatment to fabricate the composite materials. From the experimental results, The contact angle would be improved to 0° that proved the hydrophilic properties could be modified. The useful function group would be checked by FT-IR spectrum that proved the functional group has not existed significantly. Otherwise, the UV-vis properties of the composites were also tested to investigate UV penetration coefficient and also found improvement close to 0%. It could used at umbrellas、hat and kind of Shade cloth.
17
Pan, Yu-Hao, e 潘毓豪. "Low Velocity Impact Damage of Various Glass Fabric Laminates". Thesis, 2003. http://ndltd.ncl.edu.tw/handle/84497777369271945938.
Testo completoAbstract (sommario):
博士逢甲大學
紡織工程所
91
Four E-glass fabrics, non-crimp fabric, woven fabric, nonwoven mat, and integrated hollow pile fabric were selected as reinforcements for composite laminates. Three laminates, monolithic, sandwich, and hybrid structures with various numbers of layers, were formed. Low-velocity impact tests were conducted using a guided drop-weight test rig in ascending energy up to 24 J/layer nominal impact energy. A computer digitally recorded the impact load-time and energy-time histories of the laminate. Metallographic microscopy was used to observe the damage characteristics of the perpendicular cross section of the impacted laminates after a micropowder polishing treatment. The results showed that the impact energy absorption and the damage characteristics were strongly dependent on the construction of the laminate. From the observation of the metallographic fractographics, it was found that fiber breakage had occurred prior to the major damage. When the impact energy increased past the threshold energy of the major damage, matrix cracking, delamination, and fiber breakage were observed at the back surface, below a nearly undamaged zone, which attributed to bending stresses. Significant delamination was found in both of the sandwich laminate and the hybrid laminate, which could explain the increase in impact energy absorption. The damage thresholds can be identified from impact load-time and energy-time curves, and they were affected by the construction and thickness of the laminates. For the monolithic laminates, the damage force of Hertzian failure, major damage, and penetrating energy were identified. The load-time curve of the MP laminate showed a double hump response. The damage force of core buckling, major damage force of the top skin, major damage force to the bottom skin, and densification point energy, penetrating energy of the top skin, and penetrating energy of the MP laminate all were identified. The inlaid nonwoven mat induced a serious delamination response on the load-time curve of nonwoven mat inlaid multiaxial warp knit fabric laminate. The load-time curve of multilayer nonwoven mats inlaid multiaxial warp knit fabric laminate showed a corresponding multiple damage force peak response. The inlaid nonwoven mat played an important role in impact behavior and damage characteristics. The location of the inlaid nonwoven mat is another important parameter for the impact energy absorption of a laminate.
18
劉家宏. "The Property Evaluations of Woven Fabric Reinforced Thermoplastic Composite Laminated Sheet". Thesis, 2015. http://ndltd.ncl.edu.tw/handle/gg29wb.
Testo completoAbstract (sommario):
碩士逢甲大學
纖維與複合材料學系
103
In this study, woven fabrics are made with different warp/weft combinations in order to form carbon fibers/carbon fibers (CC),glass fibers/carbon fibers (GC),carbon fibers/basalt fibers (CB),and glass fibers/basalt fibers (GB) woven fabrics. The woven fabrics are then enclosed with two layers of PET laminates. Next,they undergo the hot press molding to form CC, GC, CB, and GB composites with a thickness of 1mm, 1.25mm, 1.5mm, 1.75mm, and 2mm. The control group is CC laminated with two epoxy laminates. Five laminated composite types are compared with their compositions and thicknesses in terms of the tensile strength, flexural strength, impact strength, and electromagnetic interference shielding effectiveness (EMI SE). An optical microscope is used to observe themorphology of the fractured composites that are collected from mechanical tests in order to compare with their corresponding tensile strength, flexural strength, and impact strength. The control group has the optimal mechanical properties, followed by CC, GC, CB, and eventually GB composites. In addition, the mechanical properties are also proportional their thickness, and the morphology observations indicate that the laminated composites are primarily reinforced by the woven fabrics that bear the external force. The EMI SE test results indicate that the CC composites and control group both attain an EMI SE of 55dB, that reaches the EMI SE level required by livelihood necessities.
19
Alves, Ricardo Filipe Salgueiro. "Laminador mecânico para fabrico de materiais macroporosos para regeneração óssea". Master's thesis, 2008. http://hdl.handle.net/10216/59145.
Testo completo
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Alves, Ricardo Filipe Salgueiro. "Laminador mecânico para fabrico de materiais macroporosos para regeneração óssea". Dissertação, 2008. http://hdl.handle.net/10216/59145.
Testo completo
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Wang, Jieming, e 王桀民. "Nondestructive Detection of Damage in Woven Fabric Composite Laminates Using Energy Index Method". Thesis, 2008. http://ndltd.ncl.edu.tw/handle/32711257774187643055.
Testo completoAbstract (sommario):
碩士國立屏東科技大學
車輛工程系所
96
The work presents the detection of surface cracks in a woven fabric composite laminate using a modal strain energy method. A carbon fabric F3T-282/epoxy (DICY) is used to fabricate a plain woven laminate. In the first place, the unknown material properties are computed by utilizing an inverse method through the finite element analysis and experimental modal analysis. Three equivalent models, i.e. cross-ply [0/90]ns, orthotropic and representative cell, are established to simulate the woven laminate. A surface crack is created to represent a nominal damage which is comparatively small and not to significantly affect the global stiffness of the woven laminate. Experimental modal analysis is conducted on the woven laminate to obtain the modal displacements before and after damage. The modal displacements are used to compute the modal strain energies through the three equivalent models. A damage index is defined by employing the fractional modal strain energy of the woven laminate before and after damage, and then used to identify the location of surface crack. Limited by grid points in measurement, a differential quadrature method is utilized to compute the partial differential terms in strain energy formula. Global, locate and scanning damage index three detection way are developed. Results show, the damage indices obtained from global and local measurements successfully locate the surface crack in woven laminate. The scanning damage index well identify the surface crack location and crack direction. Only few measured mode shapes are required in this method, which holds a relatively low cost and flexibility in measurement, nondestructive evaluation, and feasibility of real-time monitoring in woven laminates.
22
林立凱. "Fracture Toughness of Glass Fabric Reinforced 2-Ethyl Hexyl Acrylate Toughening Epoxy Laminates". Thesis, 2014. http://ndltd.ncl.edu.tw/handle/49785141368407866956.
Testo completo
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Chang, Kuo-An, e 張國安. "MVP and W/R Property of Laminated and Coated on Fabric Surface of Polytetrafluoroethylene Micro Porous Membrane". Thesis, 2005. http://ndltd.ncl.edu.tw/handle/22530936155630021126.
Testo completoAbstract (sommario):
碩士逢甲大學
紡織工程所
93
The thesey are by means of varties coating ways to research best way for laminated to the micro porous membrane. that including technology and recipe such as glues viscosity, coating depressure, coating layer thiness, processing speed, oven temperature and fan recycle to make bonding between interface on each side.then to have a observe to these coating sample on Polytetrafluoroethylene micro porous membrane have any parameter to cuase the micro porous structure alter and influence to these fabrics function in breathable characterstics after washing by AATCC-135 testing criteria. Varties coating processing factor make the testing result is different from each sample,that are include as thickness of membrane and the coating layer,coating and laminated resin,fabrics relative factor.testing value are from Hydrostatic,Water Moisture Permeability and Taping Strength,that result are trend to a phenomenon as the node are expand by washing in generally.that are have serious influce to breathable functionon fabrics.for sample as the one is Water Moisture Permeability and Taping strength testing value are strengthen by washing number of times.the other one as Hydrostastic testing value was cause by membrane thickness became to thiness to make the cave vanish or reduce. no matter coating resin on the surfece or not, this should be occuring after machine washing. According to experiment result shown as the physical properties of the membrane has get higher elongation rate period washing to make the unit density of micro porous from lower change to higer.and then coating layer is difficult to protection and maintain functional ability on fabrics.meanwhile,when coating on the part area of the surface,that will squeeze the branch fabril from node and make it became to vanish.
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Na, Lai Wen, e 賴文娜. "Analysis of the Flexural Behavior of Laminated Plain Woven Fabric Composite C-Beams with Various Cross-Sections". Thesis, 2000. http://ndltd.ncl.edu.tw/handle/31698240861704473006.
Testo completoAbstract (sommario):
碩士逢甲大學
紡織工程學系
88
In this study, carbon fiber plain woven fabrics were laminated to produce C-beam perform with various cross-sections. The Resin Transfer Molding technique was used to transfer resin into the mold by pressure difference. After the appropriate curing processes, the laminated plain woven composite C-beam was produced. Three point bending test was then employed. The load-deflection curve and fracture surface were investigated. The results of the experiments showed that the flexural rigidity and the peak load increased with the web height or flange width of the specimen. For the same thickness of 2 mm, the specific flexural rigidity of the beam reaches its maximum, when the web height is approximately 5 cm , and the flange width is approximately 1 cm. The specific flexural load of the beam reaches its maximum, when the web height is approximately 3 cm and the flange width is approximately 1 cm. Therefore, we get an optimal cross-section of C-beam from experiments. From the experiments, the higher web specimen, the higher stress can be found on upper flange. Under the loading head, the sudden loss of stiffness was the result of the rupture of the material at the corners of the beam cross-section. This local loss of stiffness consequently changed the deflected shape and introduced torsion in the material underneath the loading head. For the specimen with lower web height, high stress can be found on the upper and lower flanges. The phenomenon was caused by the resin breakage. The A. Rothwell’s efficiency formulae was used to analyze for the C-beams of various cross-sections. Comparison of A.Rothwell formulae and experimental data showed that the web height of 1 cm has better accuracy. But the higher web was, the less accuracy of the analysis was. This may arise due to unwanted deformations of the beam as a result of bending-torsion and lateral buckling.
25
Liu, Chun-Ting, e 劉郡婷. "The Study on the Export Competitiveness of Taiwan''s Impregnated, Coated, Covered or Laminated Textile Fabric". Thesis, 2019. http://ndltd.ncl.edu.tw/handle/rzy3ps.
Testo completoAbstract (sommario):
碩士國立臺中科技大學
企業管理系碩士班
107
Due to the continuous expansion of the international application market and the continuous development of new materials, the global industrial textiles have driven the market to grow, and the Asia-Pacific region has the most growth. This study uses customs import and export statistics to explore the textile industry in China, which is impregnated, coated, coated or bonded, and compares its export market share (EMS), display comparative benefit index (RCA), market share/displayability. The post-performance indicators such as the interest index (MSRCA) and the relative competitive position (RP) measure the export competitiveness of textiles impregnated, coated, coated or bonded in the Vietnamese market. The empirical results show that China and Vietnam are the main textile export markets for impregnation, coating, coating or bonding in China, while China and South Korea are the main competitors of China; the main products exported from Taiwan to Vietnam are “Textile fabrics impregnated, coated, covered or laminated with plastics, other than those of heading 59.02" and " Tyre cord fabric of high tenacity yarn of nylon or other polyamides, polyesters or viscose rayon" are large; in 2016, the former EMS of Taiwan was 15.37% South Korea, the latter''s EMS was 27.73%, followed by South Korea was 25.37%. In 2017, the RCA value was 3.45 in Vietnam, 7.95 in Indonesia, and 2.51 in mainland China, indicating that China has strong export competitiveness in Vietnam, Indonesia and China. Through the analysis of indicators such as MSRCA index and RP, textiles impregnated, coated, coated or bonded in Taiwan are still industries with “excellent export competitiveness”.
26
Küster, Yvonne. "Bromide characteristics and deformation mechanisms of naturally deformed rock salt of the German Zechstein Basin". Doctoral thesis, 2011. http://hdl.handle.net/11858/00-1735-0000-0006-B304-8.
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