Relevant bibliographies by topics / Semi-monocoque

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

Academic literature on the topic 'Semi-monocoque'

Author: Grafiati
Published: 28 June 2021
Last updated: 29 July 2025

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Journal articles on the topic "Semi-monocoque"

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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. Fr
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kedarnath, G. "Modelling and Analysis of Aircraft Fuselage Semi monocoque Structure." INTERNATIONAL JOURNAL OF SCIENTIFIC RESEARCH IN ENGINEERING AND MANAGEMENT 09, no. 06 (2025): 1–9. https://doi.org/10.55041/ijsrem49875.

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Abstract - The structural integrity and performance of an aircraft fuselage are critical factors in aerospace engineering. This project focuses on the modelling and analysis of a semi-monocoque aircraft fuselage structure, a widely used design due to its high strength-to-weight ratio and efficient load distribution. The study involves creating a finite element model (FEM) of the fuselage to simulate real-world loading conditions, including aerodynamic forces, internal pressurization, and structural stresses. Various materials and geometries are considered to optimize weight, strength, and dura
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Yusuf Kafi, Kafi, Sri Hastuti, and Nani Mulyaningsih. "OPTIMASI KETEBALAN STRUKTUR CHASSIS SEMI-MONOCOQUE BUS LISTRIK MENGGUNAKAN STATIC STRUCTURAL ANALYSIS." JURNAL FOUNDRY 6, no. 2 (2023): 9–19. http://dx.doi.org/10.62944/jf.v6i2.71.

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ABSTRAKPada pengembangan bus listrik medium menggunakan chassis tipe semi-monocoque masih memiliki permasalahan yaitu kelebihan massa pada strukturnya. Chassis merupakan suatu kerangka yang menopang seluruh komponen diatasnya, sehingga chassis harus kuat dan massanya kecil (ringan) untuk meningkatkan efisiensi dari kendaraan. Oleh karena itu untuk mengurangi massa struktur dapat dilakukan optimasi ukuran salah satunya pada ukuran tebal profil chassis kendaraan. Tujuan dari penelitian ini untuk menganalisis pengaruh variasi tebal profil chassis semi-monocoque bus listrik medium terhadap kekuata
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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 th
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Farrow, Ian. "Design, Build and Test of a Semi-Monocoque Wing Structure." International Journal of Mechanical Engineering Education 30, no. 1 (2002): 73–89. http://dx.doi.org/10.7227/ijmee.30.1.7.

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K., Ravindranath Tagore Rachumalla Pallavi. "RANDOM VIBRATION ANALYSIS OF SANDWICH COMPOSITE BEAMS." INTERNATIONAL JOURNAL OF ENGINEERING SCIENCES & RESEARCH TECHNOLOGY 5, no. 9 (2016): 769–79. https://doi.org/10.5281/zenodo.155243.

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In this thesis, a sandwich composite for Semi-monocoque construction in aircraft fuselage is analyzed for its strength under different loading conditions using different materials for Stringers balsa wood, syntactic foams, and honeycombs and Carbon Fiber reinforced thermoplastics is used as skin material. 3D modeling is done in Pro/Engineer. Static, Modal and Random Vibration analysis is done on the beam using finite element analysis software Ansys.
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Katrňák, Tomáš, Jaroslav Juračka, and Ivo Jebáček. "RESEARCH OF EFFECTS OF DEFECTS ON STABILITY FAILURES OF SEMI-MONOCOQUE STIFFENERS." Aviation 23, no. 3 (2020): 83–90. http://dx.doi.org/10.3846/aviation.2019.11903.

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This article presents further results of the research of effects of model defects on the local buckling of compressed stiffeners in nonlinear finite element (FE) analyses. The main outcomes are confirmation of trends for 10 sets of profile dimensions, final validations of various sets of FE simulations, and designs of practical types of defects with appropriate ratio values. A single node defect and then complex types of defects with alternating distributions of node shifts along one edge, two free flange edges, one flange surface and both flange surfaces are analyzed in this research project.
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Dababneh, Odeh, and Altan Kayran. "Design, analysis and optimization of thin walled semi-monocoque wing structures using different structural idealization in the preliminary design phase." International Journal of Structural Integrity 5, no. 3 (2014): 214–26. http://dx.doi.org/10.1108/ijsi-12-2013-0050.

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Purpose – In modeling an aircraft wing, structural idealizations are often employed in hand calculations to simplify the structural analysis. In real applications of structural design, analysis and optimization, finite element methods are used because of the complexity of the geometry, combined and complex loading conditions. The purpose of this paper is to give 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. Design/methodology/approach – In th
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Barca, Iga, Marek Rośkowicz, and Jan Godzimirski. "Selection of materials for repairing punctures of metal skin of semi-monocoque structures using composite patches." Technologia i Automatyzacja Montażu 120, no. 2 (2023): 19–32. http://dx.doi.org/10.7862/tiam.2023.2.3.

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For repairing punctures of skin of semi-monocoque structures under field conditions, simple methods are sought to guarantee the reliability of the repaired structure. Therefore, adhesive joints and composite materials are being increasingly used in repairs. During repairs using adhesion, an important aspect that affects the quality of the joint is the selection of the adhesive and the quality of surface preparation of the parts to be joined. This is necessary to get the right bond strength and durability of the joint in working environments characterized by extreme temperatures and exposure to
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Webster, J. M., T. Schmidt, and J. Mew. "A Holographic Interferometric Technique for the Detection and Computerized Recognition of Structural Faults in Semi-Monocoque Structures." Imaging Science Journal 46, no. 1 (1998): 16–20. http://dx.doi.org/10.1080/13682199.1998.11736438.

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Dissertations / Theses on the topic "Semi-monocoque"

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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
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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 efeti
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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 d
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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
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Čížková, Markéta. "Analýza poškození dopravního letounu při teroristickém útoku." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2021. http://www.nusl.cz/ntk/nusl-443754.

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In its theoretical part, the diploma thesis deals with the reasons leading to terrorist attacks and a brief list of some attacks on aircraft. It also focuses on the aircraft as the target of a terrorist attack, especially the aircraft kite as the major researched part. The conclusion of the theoretical part summarizes a list of types of aircraft fuselage structures in respect of design solutions for load transfer. The practical part determines the extent of damage caused by a missile with a fragmentation warhead. This scope is then applied to the illustrative case. In the following chapters, t
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Zamazal, Jakub. "Návrh rekonstrukce střední části trupu letounu Z 143 náhradou za poloskořepinu." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2017. http://www.nusl.cz/ntk/nusl-318137.

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The thesis is focused on reconstruction of middle part of fuselage Z 143 aircraft from truss frame to semi-monocoque frame. In the thesis there is a conceptual design of semi-monocoque middle part of fuselage. The spars of centre wing section are strength controlled. In thesis there is weight analysis according to use the semi-monocoque middle part of fuselage. In second half of the thesis there is a study of retractable landing gear. The thesis shows weight savings according to use a semi-monocoque frame. The thesis also shows that semi-monocoque frame allows other option to upgrade Z 143 air
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Book chapters on the topic "Semi-monocoque"

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"semi-monocoque, n." In Oxford English Dictionary, 3rd ed. Oxford University Press, 2023. http://dx.doi.org/10.1093/oed/2705863225.

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Conference papers on the topic "Semi-monocoque"

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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. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-4742.

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Ouellette, Jeffrey A., and Alexander W. Chin. "Finite Element Based Model of Fiber-optic Strain Sensor Mounted on a Semi-monocoque Structure." In AIAA SCITECH 2024 Forum. American Institute of Aeronautics and Astronautics, 2024. http://dx.doi.org/10.2514/6.2024-0612.

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Ravindren, Prabu Ganesh, Kirti Ghia, and Urmila Ghia. "Dynamic Analysis of the Joined-Wing Configuration in High-Altitude Long-Endurance Aircraft Using Fluid-Structure Interaction Model." In ASME/JSME 2007 5th Joint Fluids Engineering Conference. ASMEDC, 2007. http://dx.doi.org/10.1115/fedsm2007-37683.

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Recent studies of the joined-wing configuration of the High Altitude Long Endurance (HALE) aircraft have been performed by analyzing the aerodynamic and structural behaviors separately. In the present work, a fluid-structure interaction (FSI) analysis is performed, where the fluid pressure on the wing, and the corresponding non-linear structural deformation, are analyzed simultaneously using a finite-element matrix which couples both fluid and structural solution vectors. An unsteady, viscous flow past the high-aspect ratio wing causes it to undergo large deflections, thus changing the domain
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You might also be interested in the extended bibliographies on the topic 'Semi-monocoque' for particular source types:
Journal articles
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