Relevant bibliographies by topics / Monocoque

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers

Academic literature on the topic 'Monocoque'

Author: Grafiati
Published: 4 June 2021
Last updated: 2 February 2022

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Journal articles on the topic "Monocoque"

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SKOVAJSA, MICHAL, ROMAN KROFT, and FRANTISEK SEDLACEK. "NUMERICAL AND EXPERIMENTAL MODAL ANALYSIS OF A CARBON FIBRE MONOCOQUE." MM Science Journal 2021, no. 2 (June 2, 2021): 4371–75. http://dx.doi.org/10.17973/mmsj.2021_6_2021048.

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This paper deals with the comparison of experimental measurements and numerical simulation of the natural frequency and natural shape of a carbon fibre monocoque. This comparison is used to validate the numerical analysis with a real monocoque. Usually, monocoques consist of orthotropic materials like carbon fibre sandwich with a honeycomb core. The monocoque is manufactured by hand from several layers of different materials, which are connected by glued joints. This does not guarantee the material properties or the same mass the idealized numerical simulation.
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Singhanart, Thanyarat, Kulanun Chutisemachai, Kiatnathee Dilokthonsakun, Jintasarn Sanchai, and Kasemphan Siriployngam. "On the Use of Composite-Steel Joint for Semi-Monocoque Frame Design." Applied Mechanics and Materials 619 (August 2014): 23–27. http://dx.doi.org/10.4028/www.scientific.net/amm.619.23.

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The design of semi-monocoque frame by using the composite-steel joint is considered in this paper. The frame is designed with weight less than 30kg and torsional stiffness more than 1200 Nm/deg. In order to design the semi-monocoque frame, the analysis of the composite-steel joint has to be clearly investigated. Therefore, the stress analysis of composite-steel joint is performed and then the frame is designed. The double lab joint with two holes is tested and verified by the experiments. The carbon-fiber fabric laminated with the KEVLAR fabric composite laminate is used for composite part. From experiments, the joint’s strength can be increased by using the eccentric holes. Therefore, in order to meet the requirement of the SAE rules; load capacity more than 30 kN, the eccentric hole double lap joint is numerically designed and applied to semi-monocoque frame. The joint has strength of 32 kN and can be used in frame design. The semi-monocoque frame is designed and analyzed by finite element analysis. The maximum stress at maximum load is 208 MPa which is less than the yield strength of the materials so it can withstand the loads, the mass is 29.6kg, and the torsional stiffness of the frame is 1408 Nm/degree. Therefore, the semi-monocoque frame can be successfully designed.
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Zoppke, Hartmut, Matthias Scherer, Matthias Braband, and Alexander Dietz. "Leichtbau-Pkw mit naturfaserverstärktem Monocoque." ATZ - Automobiltechnische Zeitschrift 122, no. 7-8 (July 2020): 74–78. http://dx.doi.org/10.1007/s35148-020-0277-7.

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Bulgu, Chala Jembere. "Design a Space Frame Chassis for Light Weight Automobiles for Improved Safety and Reliability." Mechanical Engineering Research 9, no. 2 (January 31, 2020): 36. http://dx.doi.org/10.5539/mer.v9n2p36.

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The objective of this research is to design a spaceframe chassis for light weight automobiles possessing unladen weight of ≤ 550Kg to replace the conventional monocoque type chassis frame. The maximum stress and maximum deflection that the chassis can resist without fracturing are important criteria. In this thesis, the existing monocoque chassis was considered and analyzed under static loading, frontal impact, side impact, rear impact, front rollover and side rollover loading conditions by using Finite Element Analysis method. Then, taking the test results as a reference, a spaceframe chassis was designed for the same size vehicle. The critical evaluation standard points stated in the Federal Motor Vehicle Safety Standard (FMVSS), U.S.A standard, were used as guideline to see the performance of the existing and the new chassis frames. The test results show that a space frame chassis has better stress resisting capacity and reliability than the conventional monocoque chassis frame under all impacts.
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Fragassa, Cristiano, Giangiacomo Minak, and Mauro Sassatelli. "Reducing defects in composite monocoque frames." FME Transactions 47, no. 1 (2019): 48–53. http://dx.doi.org/10.5937/fmet1901048f.

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Chang, C. K., and J. H. Cheng. "Optimization of Sandwich Monocoque Car Body with Equivalent Shell Element." Journal of Mechanics 23, no. 4 (December 2007): 381–88. http://dx.doi.org/10.1017/s172771910000143x.

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AbstractThis research proposes a straightforward and efficient method to optimize a sandwich monocoque car body with the developed equivalent shell element based on stiffness equivalence. The fact that stiffness rather than strength is dominant constraint for ordinary car body optimization is demonstrated. A simple but heavy flat chassis plate is utilized as upper bound, while an ideal monocoque is used as lower bound for an actual car body optimization. Convergence hours can be significantly reduced with the equivalent element and the initial-bounded method. A novel electric car body optimization is presented, fulfilling UltraLight Steel Auto Body (ULSAB) stiffness requirements and showing similar optimal weight results as a conventional approach with a much lower analysis time cost.
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Лозбинев, Владимир, and Vladimir Lozbinev. "Analysis of factors providing efficiency of load-bearing elements of the car body." Bulletin of Bryansk state technical university 2015, no. 3 (September 30, 2015): 52–56. http://dx.doi.org/10.12737/22992.

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The factors that determine the performance monocoque cars. New approaches to the evaluation of the stress state of car bodies, the stability of load-bearing elements. The importance of assessing the survivability of bearing elements.
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Barygin, Valery V. "Digital Technologies for Aerospace Industry Products." AEROSPACE SPHERE JOURNAL, no. 2 (June 26, 2021): 76–83. http://dx.doi.org/10.30981/2587-7992-2020-107-2-76-83.

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The creation of new generations of products in the aerospace industry is possible by applying a fundamentally new method of designing and manufacturing solid metal multilayer monocoque. A new additive manufacturing technology based on Russian patents is proposed.
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Alonso, L., C. Bedoya, B. Lauret, and F. Alonso. "F²TE³: a Transparent Semi-Monocoque VIP Envelope." Applied Mechanics and Materials 71-78 (July 2011): 594–97. http://dx.doi.org/10.4028/www.scientific.net/amm.71-78.594.

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This article examines a new lightweight, slim, high energy efficient, light-transmitting, self-supporting envelope system, providing for seamless, free-form designs for use in architectural projects. The system exploits vacuum insulation panel technology. The research was based on envelope components already existing on the market and patents and prototypes built by independent laboratories, especially components implemented with silica gel insulation, as this is the most effective transparent thermal insulation there is today. The tests run on these materials revealed that there is not one that has all the features required of the new envelope model, although some do have properties that could be exploited to generate this envelope, namely, the vacuum chamber of vacuum insulation panels, the use of monolithic aerogel as insulation in some prototypes, and reinforced polyester barriers. These three design components have been combined and tested to design a new, variable geometry, energy-saving envelope system that also solves many of the problems that other studies ascribe to the use of vacuum insulation panels.
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Keolian, Robert M., Kevin J. Bastyr, Ray S. Wakeland, and John F. Brady. "Monocoque shell and tube heat exchanger for thermoacoustics." Journal of the Acoustical Society of America 144, no. 3 (September 2018): 1712. http://dx.doi.org/10.1121/1.5067595.

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Dissertations / Theses on the topic "Monocoque"

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Lizotte, Patrick L. "Stress analysis and fabrication of composite monocoque bicycle frames." Thesis, McGill University, 1996. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=24064.

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An analytical and experimental investigation was conducted to study the design and fabrication of carbon fiber track bicycle frames. A finite element software was used for the geometry development, laminate configuration, and for predicting failure using the maximum stress criteria. A load case and boundary conditions simulating actual riding conditions were developed. The stresses in each of the composite layers were found to be lower than the allowable stresses because of a properly designed geometry and laminate. Two composite frames were fabricated using the hand lay-up technique, using unidirectional and woven carbon fiber pre-preg material over an internal foam core. Using static testing techniques and comparisons with traditional tubular frames, the carbon fiber prototypes were shown to be better in all rigidity aspects. Combining the experimental and theoretical results, a good understanding of the critical problems related to composite monocoque bicycle frame design was obtained.
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Humphreys, Matthew. "Development and Structural Investigation of Monocoque Fibre Composite Trusses." Queensland University of Technology, 2003. http://eprints.qut.edu.au/15898/.

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Fibre composite materials are gaining recognition in civil engineering applications as a viable alternative to traditional materials. Their migration from customary automotive, marine, aerospace and military industries into civil engineering has continued to gain momentum over the last three decades as new civil engineering applications develop. The use of fibre composite materials in civil engineering has now evolved from non-structural applications, such as handrails and cladding, into primary structural applications such as building frames, bridge decks and concrete reinforcement. However, there are issues which are slowing the use of fibre composite materials into civil engineering. Issues include high costs, difficulties in realising potential benefits, general lack of civil engineers' familiarity with the material and relatively little standardisation in the composites industry. For composites to truly offer a viable alternative to traditional construction materials in the civil engineering marketplace, it is essential that these issues be addressed. It is proposed that this situation could be improved by demonstrating that potential benefits offered by composites can be achieved with familiar civil engineering forms. These forms must be well suited to fibre composite materials and be able to produce safe and predictable civil engineering structures with existing structural engineering methods. Of the numerous structural forms currently being investigated for civil engineering applications, the truss form appears particularly well suited to fibre composites. The truss is a familiar structural engineering form which possesses certain characteristics that make it well suited to fibre composite materials. In this research a novel monocoque fibre composite truss concept was developed into a working structure and investigated using analytical and experimental methods. To the best of the author's knowledge the research presented in this thesis represents the first doctoral research into a structure of this type. This thesis therefore presents the details of the development of the monocoque fibre composite (MFC) truss concept into a working structure. The developed MFC truss was used as the basis for a detailed investigation of the structural behaviour of the MFC truss elements and the truss as a whole. The static structural behaviour of the principal MFC truss elements (tension members, compression members and joints) was investigated experimentally and analytically. Physical testing required the design and fabrication of a number of novel test rigs. Well established engineering principles were used along with complex finite element models to predict the behaviour of the tested truss elements and trusses. Results of the theoretical analysis were compared with experimental results to determine how accurately their static structural behaviour could be predicted. It was found that the static structural behaviour of all three principal truss elements could be accurately predicted with existing engineering methods and finite element analysis. The knowledge gained from the investigation of the principal truss elements was then used in an investigation of the structural behaviour of the MFC truss. Three full-scale MFC trusses were fabricated in the form of conventional Pratt, Howe and Warren trusses and tested to destruction. The investigation included detailed finite element modelling of the full-scale trusses and the results were compared to the full-scale test results. Results of the investigation demonstrated that the familiar Pratt, Howe and Warren truss forms could be successfully manufactured with locally available fibre composite materials and existing manufacturing technology. The static structural behaviour of these fibre composite truss forms was accurately predicted with well established engineering principles and finite element analysis. A successful marriage between fibre composite materials and a civil engineering structure has been achieved. Monocoque fibre composite trusses have been developed in the familiar Pratt, Howe and Warren truss forms. These structures possess characteristics that make them well suited to applications as primary load bearing structures.
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Santos, Fábio Henrique Massuia de Souza. "Modelagem computacional para análise de tensões e deslocamentos em fuselagem semi-monocoque." Instituto Tecnológico de Aeronáutica, 2004. http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=2905.

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Este trabalho apresenta a análise de tensões e deslocamentos de uma fuselagem semi-monocoque através do método dos elementos finitos. Os diversos modelos utilizados nas análises possuem variações a partir de dois modelos básicos. O primeiro modelo considera o modelamento de cavernas e reforçadores como elementos de barra. O segundo modelo considera que somente os reforçadores devem ser modelados com elementos de barra; as cavernas, neste modelo, são modeladas com elementos de placa. As variações consideradas são: modelamento e não modelamento dos shear clips, presença e ausência de offsets nos reforçares e discretização da malha (malhas mais grosseira e malhas mais refinidas). Os resultados obtidos mostram que a quantidade e qualidade da malha influenciam muito mais os resultados do que presença ou não de offsets. Modelos com mesma malha, porém com diferença entre os offsets, possuem resultados muito próximos. A modelagem ou não dos shear clips influência na rigidez da estrutura e conseqüentemente deve ser modelado para melhor representar a estrutura real.
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Rich, Jonathan E. "Design Optimization Procedure for Monocoque Composite Cylinder Structures Using Response Surface Techniques." Thesis, Virginia Tech, 1997. http://hdl.handle.net/10919/35512.

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An optimization strategy for the design of composite shells is investigated. This study differs from previous work in that an advanced analysis package is utilized to provide buckling information on potential designs. The Structural Analysis of General Shells (STAGS) finite element code is used to provide linear buckling calculations for a minimum buckling load constraint. A response surface, spanning the design space, is generated from a set of design points and corresponding buckling load data. This response surface is incorporated into a genetic algorithm for optimization of composite cylinders. Laminate designs are limited to those that are balanced and symmetric. Three load cases and four different variable formulations are examined. In the first approach, designs are limited to those whose normalized in-plane and out-of-plane stiffness parameters would be feasible with laminates consisting of two independent fiber orientation angles. The second approach increases the design space to include those that are bordered by those in the first approach. The third and fourth approaches utilize stacking sequence designs for optimization, with continuous and discrete fiber orientation angle variation, respectively. For each load case and different variable formulation, additional runs are made to account for inaccuracies inherent in the response surface model. This study concluded that this strategy was effective at reducing the computational cost of optimizing the composite cylinders.
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Paulin, Julio Cezar. "Dimensionamento preliminar de uma seção de fuselagem semi-monocoque de uma aeronave de passageiros." Instituto Tecnológico de Aeronáutica, 2008. http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1173.

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Um método de pré-dimensionamento da estrutura da fuselagem de uma aeronave foi desenvolvido nesse trabalho com o objetivo de possibilitar ao engenheiro de estruturas o cálculo rápido dos esforços primários e secundários, bem como das margens de segurança dessa estrutura. Para tanto, as teorias de cálculo desse tipo de estrutura foram implementadas em uma planilha de forma a permitir que o engenheiro mude com facilidade os parâmetros de projeto, podendo assim buscar uma solução mais eficiente. Neste trabalho são discutidas também as conseqüências de não se considerar as reduções das áreas efetivas do revestimento, devido à flambagem dos mesmos, no cálculo da área total resistente à compressão axial.
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Castillo, Henry A. "Optimum design of isotropic monocoque and ring-stiffened circular cylindrical shells subject to external hydrostatic pressure." Thesis, Monterey, California : Naval Postgraduate School, 1992. http://handle.dtic.mil/100.2/ADA257864.

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Thesis (M.S. in Mechanical Engineering)--Naval Postgraduate School, June 1992.
Thesis Advisor: Salinas, David. Description based on title screen as viewed on April 16, 2009. Includes bibliographical references (p. 124). Also available in print.
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Mello, Pedro Paulo Serrajordia Rocha de. "Análise da influência dos esforços primários em fuselagem semi-monocoque nas tensões de da tração diagonal." Instituto Tecnológico de Aeronáutica, 2004. http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=611.

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A determinação dos esforços primários via NASTRAN, ao contrário do que ocorre ao se utilizar a teoria do engenheiro que faz uso extensivo de larguras efetivas de chapa, baseia-se na hipótese de que os painéis não flambam. A redistribuição das tensões ocorre apenas levando-se em conta os efeitos da tração diagonal, enquanto a flambagem dos painéis não é levada em conta neste estudo. Sabendo-se que ao não considerar a flambagem, erros podem ser cometidos, este trabalho realiza uma comparação entre duas análises da estrutura primária: análise usando NASTRAN, levando-se em conta a redistribuição de tensão devido à tração diagonal - sem considerar a flambagem dos painéis; e análise da teoria do engenheiro considerando a flambagem dos painéis, através do uso de larguras e áreas efetivas dos painéis flambados, também se levando em conta a redistribuição de tensões devido à tração diagonal. Aqui se apresenta a questão de como devem ser utilizados os resultados obtidos através de uma análise de uma fuselagem semi-monocoque pelo NASTRAN, face ao fato de que existe a possibilidade real de flambagem de chapas dessa estrutura.
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Dababneh, Odeh. "Design, Analysis And Optimization Of Thin Walled Semi-monocoque Wing Structures Using Different Structural Idealizations In The Preliminary Design Phase." Master's thesis, METU, 2011. http://etd.lib.metu.edu.tr/upload/12613759/index.pdf.

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This thesis gives a comprehensive study on the effect of using different structural idealizations on the design, analysis and optimization of thin walled semi-monocoque wing structures in the preliminary design phase. In the design part, wing structures are designed by employing two different structural idealizations that are typically used in the preliminary design phase. In the structural analysis part, finite element analysis of one of the designed wing configurations is performed using six different one and two dimensional element pairs which are typically used to model the sub-elements of semi-monocoque wing structures. The effect of using different finite element types on the analysis results of the wing structure is investigated. During the analysis study, depending on the mesh size used, conclusions are also inferred with regard to the deficiency of certain element types in handling the true external load acting on the wing structure. Finally in the optimization part, wing structure is optimized for minimum weight by using finite element models which have the same six different element pairs used in the analysis phase. The effect of using different one and two dimensional element pairs on the final optimized configurations of the wing structure is investigated, and conclusions are inferred with regard to the sensitivity of the optimized wing configurations with respect to the choice of different element types in the finite element model. Final optimized wing structure configurations are also compared with the simplified method based designs which are also optimized iteratively. Based on the results presented in the thesis, it is concluded that with the simplified methods, preliminary sizing of the wing structures can be performed with enough confidence, as long as the simplified method based designs are also optimized. Results of the simplified method of analysis showed that simplified method is applicable to be used as an analysis tool in performing the preliminary sizing of the wing structure before moving on to more refined finite element based analysis.
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Mende, Milan. "Konstrukční návrh kompozitního chassis Formule Student." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2021. http://www.nusl.cz/ntk/nusl-449785.

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The Master’s thesis deals with the design and production of a composite chassis of the new formula Dragon X. The carbon prepreg used for manufacturing of the monocoque was to be operated at high temperatures. Therefore, this thesis deals with the application of composites structures in the high temperature environment. The thesis addresses the torsional stiffness problematics and it was not only physically tested, but also simulated by FEM analysis and the results were compared.
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Ricardo, Vagner Proença. "Projeto comparativo da fuselagem central de uma aeronave em material compósito e alumínio." Instituto Tecnológico de Aeronáutica, 2004. http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=675.

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Esse trabalho apresenta uma metodologia para seleção da melhor concepção na fabricação da fuselagem central de uma aeronave executiva de seis ocupantes. Para isso, são estudadas três possibilidades: construção semi-monocoque em alumínio; materiais compósitos produzidos por Laminação por Controle Numérico e materiais compósitos produzidos por Hand Lay-up. A metodologia permite uma análise quantitativa das concepções, mesmo em fases iniciais do projeto, o que contribui para a seleção das melhores opções de concepções logo no início da análise. A partir deste estudo, ée possível observar que o projeto em Laminação por Controle Numérico ée mais adequado economicamente na fabricação da fuselagem em material compósito, devido a menores custos com matéria-prima e com mão-de-obra. Dessa maneira, o estudo prossegue com as duas concepções (material compósito fabricado por Laminação por Controle Numérico e estrutura semi-monocoque em alumínio). ÉE realizado o pré-dimensionamento das duas soluções, e em seguida estima-se o peso e o custo de fabricação das mesmas. A análise comparativa entre as soluções mostra que a concepção em material compósito apresenta uma diminuição de peso considerável acompanhada de ligeira diminuição de custo, o que permite concluir que ela se apresenta como uma alternativa técnica e economicamente viável e interessante do ponto de vista de ganho em desempenho da aeronave.
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Books on the topic "Monocoque"

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Sandham, Tommy. How to restore chassis and monocoque bodywork. London: Osprey, 1985.

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Shippen, J. M. An investigation into a monocoque vehicle bodyshell acoustic behaviour using conceptual level information. Birmingham: University of Birmingham, 1988.

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Castillo, Henry A. Optimum design of isotropic monocoque and ring-stiffened circular cylindrical shells subject to external hydrostatic pressure. Monterey, California: Naval Postgraduate School, 1992.

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Bielawa, Richard L. Static strain and vibration characteristics of a metal semimonocoque helicopter tail cone of moderate size. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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Wimpffen, Janos. Monocoques & ground effects: World championship sports car racing in photographs, 1982-1992. Phoenix, AZ: David Bull Pub., 2008.

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Christian, Meyer. Mensura monochordi: La division du monocorde, IXe-XVe siècles. Paris: Société française de musicologie, 1996.

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La prensa chilena en la encrucijada: Entre la voz monocorde y la revolución digital. Santiago de Chile: LOM Ediciones, 2012.

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How to Restore Chassis and Monocoque Bodywork. Osprey Pub Co, 1986.

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N, Bansek Robert, George W. Woodruff School of Mechanical Engineering., and NASA/USRA University Advanced Design Program., eds. Monocoque structure for the skitter three-legged walker. Atlanta, Ga: The George W. Woodruff School of Mechanical Engineering, Georgia Institute of Technology, 1988.

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Hoff, Nicholas J. Monocoque, Sandwich, and Composite Aerospace Structures: Selected Papers of Nicholas J. Hoff. Technomic Publishing Company, 1986.

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Book chapters on the topic "Monocoque"

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Rogacki, Igor, Eugeniusz Rusiński, and Marek Sawicki. "Structural Analysis of Composite Scooter Monocoque." In Lecture Notes in Mechanical Engineering, 599–610. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-04975-1_69.

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Liu, Zhuli, Xiangyu Huo, Hao Zhou, and Xiaoguang Wu. "Topology Optimization Design of the Monocoque Bus Body Structure." In Advances in Mechanical Design, 456–65. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-32-9941-2_37.

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Casale, Nicholas, Daniel Bristow, and Christopher M. Pastore. "Design and Fabrication of a Braided Composite Monocoque Bicycle Frame." In ACS Symposium Series, 90–101. Washington, DC: American Chemical Society, 1991. http://dx.doi.org/10.1021/bk-1991-0457.ch006.

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Azriyuddin, Izzat Afandi Mohd, Ya’akob Yusof, Ahmad Kamil Hussain, and Jamaluddin Mahmud. "Solar Car (Tigris) Monocoque Design: Structure, Cost and Power Consumption." In Lecture Notes in Mechanical Engineering, 241–55. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-9505-9_24.

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Duffuaa, Salih O., and Boaz Golany. "Homomonotone Games and Monocore Solutions." In Systems and Management Science by Extremal Methods, 311–26. Boston, MA: Springer US, 1992. http://dx.doi.org/10.1007/978-1-4615-3600-0_20.

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Yu, D., K. DeMoranville, M. Takayasu, and T. Wong. "A New Technique to Fabricate Multifilament Nb3Sn Superconductor Using Cabled Monocore Subelements." In Advances in Cryogenic Engineering Materials, 911–18. Boston, MA: Springer US, 1998. http://dx.doi.org/10.1007/978-1-4757-9056-6_120.

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"Body Monocoque Loads." In Structural Loads Analysis for Commercial Transport Aircraft, 191–206. Washington DC: American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/5.9781600862465.0191.0206.

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Hagedorn, H., and Z. Q. Wei. "Monocoque lining design for the Gotthard Base Tunnel." In Shotcrete: Engineering Developments, 135–44. CRC Press, 2020. http://dx.doi.org/10.1201/9781003078678-20.

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"THE MONOCOLUS." In Mysterium Coniunctionis, 533–46. Routledge, 2014. http://dx.doi.org/10.4324/9781315725338-43.

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Conference papers on the topic "Monocoque"

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Kamal, K., K. P. Rajgopalan, and M. R. Joshi. "Monocoque, Automotive Bodies in Advanced Composites." In Symposium on International Automotive Technology. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1996. http://dx.doi.org/10.4271/962560.

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Farinasso Perucci, Laura, Rafael Marchi, and Gustavo Gonçalves. "The development of a race car monocoque." In 24th ABCM International Congress of Mechanical Engineering. ABCM, 2017. http://dx.doi.org/10.26678/abcm.cobem2017.cob17-2778.

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Ning, Xin, and Sergio Pellegrino. "Design and testing of imperfection-insensitive monocoque cylindrical shells." In 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-1768.

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Christensen, John. "Carbon Fibre Monocoque Chassis Feasibility and Manufacturability for FSAE." In 18th Asia Pacific Automotive Engineering Conference. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2015. http://dx.doi.org/10.4271/2015-01-0078.

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KAMBLE, MEGHANA, TALAL SHAKFEH, and HAMID DALIR. "Analysis and Optimization of a Composite Monocoque for Structural Performance." In American Society for Composites 2019. Lancaster, PA: DEStech Publications, Inc., 2019. http://dx.doi.org/10.12783/asc34/31258.

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Weidner, L. R., D. W. Radford, and P. A. Fitzhorn. "A Multi-Shell Assembly Approach Applied to Monocoque Chassis Design." In Motorsports Engineering Conference & Exhibition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2002. http://dx.doi.org/10.4271/2002-01-3360.

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Davidson, Stephanie. "Pulp: Research in Temporary, Biodegradable Structures." In AIA/ACSA Intersections Conference. ACSA Press, 2020. http://dx.doi.org/10.35483/acsa.aia.inter.20.4.

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Abstract:
This paper documents in-progress design research in temporary, biodegradable structures. The experimental, thin-shell monocoque structures have been cast using a variety of cellulose-based materials, and represent a sampling of the outcome of a studio taught at three different architecture schools to date.
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Nicholson, Colin R., Stephen R. Turnour, and Helen E. Chapman. "The Design and Testing of Buckling Monocoque Seating Structures for Aircraft." In General, Corporate & Regional Aviation Meeting & Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1999. http://dx.doi.org/10.4271/1999-01-1599.

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Hamilton, Leonard, Peter Joyce, Chris Forero, and Martin McDonald. "Production of a Composite Monocoque Frame for a Formula SAE Racecar." In SAE 2013 World Congress & Exhibition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2013. http://dx.doi.org/10.4271/2013-01-1173.

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Kalyanasundaram, Haribaskar, and Masoud Rais-Rohani. "Design optimization and residual strength assessment of a semi-monocoque cylindrical structure." In 8th Symposium on Multidisciplinary Analysis and Optimization. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-4742.

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