Relevant bibliographies by topics / Aerospace Structure

Contents

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

Academic literature on the topic 'Aerospace Structure'

Author: Grafiati
Published: 14 March 2023
Last updated: 31 July 2025

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Journal articles on the topic "Aerospace Structure"

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RAHIM, Erween, Takayuki OGAWA, Akihiko MIURA, Hiroyuki SASAHARA, Rei Koyasu, and Yasuhiro Yao. "3252 Ultrasonic Torsional Vibration Drilling of Aerospace Structure Material." Proceedings of International Conference on Leading Edge Manufacturing in 21st century : LEM21 2011.6 (2011): _3252–1_—_3252–4_. http://dx.doi.org/10.1299/jsmelem.2011.6._3252-1_.

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Bajurko, Piotr. "Modelling of the Aerospace Structure Demonstrator Subcomponent." Transactions on Aerospace Research 2019, no. 1 (2019): 37–52. http://dx.doi.org/10.2478/tar-2019-0004.

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Abstract Carbon-epoxy composite materials, due to their high strength in relation to mass, are increasingly used in the construction of aircraft structures, however, they are susceptible to a number of damages. One of the most common is delamination, which is a serious problem in the context of safe operation of such structures. As part of the TEBUK project, the Institute of Aviation has developed a methodology for forecasting the propagation of delamination. In order to validate the proposed method, an aerial structure demonstrator, modelled on the horizontal stabilizer of the I-23 Manager ai
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DOS SANTOS E LUCATO, S. L., R. M. MCMEEKING, and A. G. EVANS. "SMS-12: Shape Morphing Truss Structure for Aerospace and Marine Applications(SMS-II: SMART MATERIALS AND STRUCTURES, NDE)." Proceedings of the JSME Materials and Processing Conference (M&P) 2005 (2005): 30. http://dx.doi.org/10.1299/jsmeintmp.2005.30_4.

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Al-Madani, Ramadan A., M. Jarnaz, K. Alkharmaji, and M. Essuri. "Finite Element Modeling of Composites System in Aerospace Application." Applied Mechanics and Materials 245 (December 2012): 316–22. http://dx.doi.org/10.4028/www.scientific.net/amm.245.316.

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The characteristics of composite materials are of high importance to engineering applications; therefore the increasing use as a substitute for conventional materials, especially in the field of aircraft and space industries. It is a known fact that researchers use finite element programs for the design and analysis of composite structures, use of symmetrical conditions especially in complicated structures, in the modeling and analysis phase of the design, to reduce processing time, memory size required, and simplifying complicated calculations, as well as considering the response of composite
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Horton, B., Y. Song, D. Jegley, F. Collier, and J. Bayandor. "Predictive analysis of stitched aerospace structures for advanced aircraft." Aeronautical Journal 124, no. 1271 (2019): 44–54. http://dx.doi.org/10.1017/aer.2019.137.

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ABSTRACTIn recent years, the aviation industry has taken a leading role in the integration of composite structures to develop lighter and more fuel efficient aircraft. Among the leading concepts to achieve this goal is the Pultruded Rod Stitched Efficient Unitized Structure (PRSEUS) concept. The focus of most PRSEUS studies has been on developing an hybrid wing body structure, with only a few discussing the application of PRSEUS to a tube-wing fuselage structure. Additionally, the majority of investigations for PRSEUS have focused on experimental validation of anticipated benefits rather than
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YAMAMOTO, Tetsuya. "Application of adhesive bonded structure on aerospace." Journal of the Surface Finishing Society of Japan 40, no. 11 (1989): 1203–6. http://dx.doi.org/10.4139/sfj.40.1203.

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Sainfort, P., Christophe Sigli, G. M. Raynaud, and P. Gomiero. "Structure and Property Control of Aerospace Alloys." Materials Science Forum 242 (January 1997): 25–32. http://dx.doi.org/10.4028/www.scientific.net/msf.242.25.

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Jiayu, Yao. "A method of coding for aerospace product quality DNA." MATEC Web of Conferences 151 (2018): 05006. http://dx.doi.org/10.1051/matecconf/201815105006.

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Aiming at the problem that the manufacturing process of our aerospace products is relatively discrete and the lack of appropriate quality monitoring and feedback mechanism, a method of coding for aerospace product quality DNA was proposed. Based on the structure of biological DNA and the theory of quality assessment, equipment diagnosis and quality traceability, the biological DNA structure was transformed into the structure of aerospace product quality DNA, and the concept of aerospace product quality DNA was defined, including the genetic and variation characteristics of aerospace product qu
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Bai, Yan, Chuncheng Xiao, Zijian Wei, and Lan Yin. "Study on Structure health monitoring method of space vehicle based on PVDF piezoelectric film." Journal of Physics: Conference Series 2479, no. 1 (2023): 012022. http://dx.doi.org/10.1088/1742-6596/2479/1/012022.

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Abstract At present, health monitoring technology of large structures has been paid more and more attention, among which structure measurement system based on PVDF piezoelectric film sensor has been widely used in various fields. To solve the problem that large structural parts of aerospace are easy to be damaged, a load measurement system based on PVDF piezoelectric film sensor is built in this paper given the complex design structure of aerospace. A large cylinder of aerospace is taken as the test part, the stress state of structural parts is measured online, and the corresponding load value
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Si, Liang, and Zongfeng Li. "Online structural state assessment for aerospace composite structures using an acousto-ultrasonics-based multi-damage index identification approach." Structural Health Monitoring 19, no. 6 (2020): 1790–807. http://dx.doi.org/10.1177/1475921719899334.

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The development of aerospace manufacturing has promoted the application of lightweight composite materials into aerospace structures. Although the aerospace composite structures possess numerous advantages, invisible internal structural damage such as delaminations induced by various external factors can significantly reduce the mechanical affordability, safety, and life-cycle of the structure. Therefore, it is of great significance to monitor and assess the health state and predict accurately the lifetime of aerospace composite structures. An acousto-ultrasonics-based multi-damage index ident
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Dissertations / Theses on the topic "Aerospace Structure"

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Ahn, Junghyun. "Integrated analysis procedure of aerospace composite structure." Thesis, Massachusetts Institute of Technology, 2008. http://hdl.handle.net/1721.1/43106.

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Thesis (S.M.)--Massachusetts Institute of Technology, System Design and Management Program, 2008.<br>Includes bibliographical references (p. 50).<br>The emergence of composite material application in major commercial aircraft design, represented by the Boeing 787 and Airbus A350-XWB, signals a new era in the aerospace industry. The high stiffness to weight ratio of continuous fiber composites (CFC) makes CFCs one of the most important materials to be introduced in modern aircraft industry. In addition to inherent strength (per given weight) of CFCs, they also offer the unusual opportunity to d
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Key, Ross A. "Automated manufacturing processes for secondary structure aerospace composites." Thesis, University of Nottingham, 2016. http://eprints.nottingham.ac.uk/33572/.

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As projected manufacturing rates for commercial aircraft increase to levels of multiple ship sets per day from individual manufacturing facilities, GE Aviation have expressed the need for a shift in composites secondary structure manufacturing philosophy. Traditional manufacturing processes tend to be touch labour intensive and hence costly. The manual placement of large numbers of individual ply profiles, lengthy debulking operations and complex cure cycles, result in excessive component lead times and manufacturing costs. As a result, direct labour cost is a major factor in the total economi
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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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Zheng, LiangKan 1972. "Fluid-structure coupling for aeroelastic computations in the time domain using low fidelity structural models." Thesis, McGill University, 2005. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=99127.

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Flutter analysis plays an important role in the design and development of aircraft wings because of the information it provides regarding the flight envelope of the aircraft. With the coupling of the flow and structural solver, the flutter boundary of wings can be evaluated in the time domain. This study: First, computes the aeroelastic response for a typical sweptback wing section model by coupling a flow solver and a two degree of freedom structural equation of motion solver to predict the flutter boundary of an airfoil at different Mach numbers. The results agree well with previous numerica
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Seddon, Caroline Michelle. "Modelling transient dynamic fluid-structure interaction in aerospace applications." Thesis, University of Salford, 2006. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.492434.

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Although significant progress has been made in the study of dynamic loading of aircraft structures, several areas have been identified that require further research. In particular, attention is drawn to problems involving transient, dynamic fluid-structure interaction, where fluids play an important role, heavily influencing the response of the structure to the applied dynamic load. In this work the use of existing numerical modelling techniques for the evaluation of such problems is investigated.
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Bhatti, Wasim. "Mechanical integration of a PEM fuel cell for a multifunctional aerospace structure." Thesis, Loughborough University, 2016. https://dspace.lboro.ac.uk/2134/21513.

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A multifunctional structural polymer electrolyte membrane (PEM) fuel cell was designed, developed and manufactured. The structural fuel cell was designed to represent the rear rib section of an aircraft wing. Custom membrane electrode assemblies (MEA s) were manufactured in house. Each MEA had an active area of 25cm2.The platinum loading on each electrode (anode and cathode) was 0.5mg/cm2. Sandwiched between the electrodes was a Nafion 212 electrolyte membrane. Additional components of the structural fuel included metallic bipolar plates and end plates. Initially all the components were manufa
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Palsule, Sanjay. "Structure and properties of aerospace molecular composites : third generation polymers." Thesis, Heriot-Watt University, 1994. http://hdl.handle.net/10399/1388.

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Khataee, Amin. "Structure and properties of some Ti-Al-Ru alloys." Thesis, Imperial College London, 1987. http://hdl.handle.net/10044/1/46915.

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Liang, Lijun. "Experimental investigation of an aeroelastic structure with continuous nonlinear stiffness." Thesis, McGill University, 2003. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=80123.

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An experimental investigation is presented for the aeroelastic response of a two-degree-of-freedom airfoil positioned in an incompressible flow. In particular, the effects of cubic structural nonlinearities in the pitch degree-of-freedom are considered. These nonlinearities are introduced via a specially designed pitch cam, which permits different degrees of nonlinearity, as well as a linear system, to be obtained.<br>Several linear and nonlinear system tests are presented, and the results compared and analyzed. The effects of linear plunge stiffness on the stability of the aeroelastic
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Ozsoy, Serhan. "Vibration Induced Stress And Accelerated Life Analyses Of An Aerospace Structure." Master's thesis, METU, 2006. http://etd.lib.metu.edu.tr/upload/2/12606966/index.pdf.

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Fatigue failure of metallic structures operating under dynamic loading is a common occurrence in engineering applications. It is difficult to estimate the response of complicated systems analytically, due to structure&amp<br>#8217<br>s dynamic characteristics and varying loadings. Therefore, experimental, numerical or a combination of both methods are used for fatigue evaluations. Fatigue failure can occur on systems and platforms as well as components to be mounted on the platform. In this thesis, a helicopter&amp<br>#8217<br>s Missile Warning Sensor - Cowling assembly is analyzed. Analytical
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Books on the topic "Aerospace Structure"

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Ryzhikova, tamara. Marketing in the aerospace field. INFRA-M Academic Publishing LLC., 2020. http://dx.doi.org/10.12737/1003199.

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The tutorial provides an overview of the main methodological approaches to the analysis of the market of rocket and space technology and services on the basis of its specific features, methods of evaluating competition and its justification, the reinterpretation of basic marketing tools and approaches in combination with innovative ideas and methods of achieving high economic results in the space market.&#x0D; The main aim is to provide future marketers with the necessary material, methods, technologies and tools with which to solve various problems related to the understanding of the structur
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H, Laakso John, and Langley Research Center, eds. System integration and demonstration of adhesive bonded high temperature aluminum alloys for aerospace structure: Phase II. National Aeronautics and Space Administration, Langley Research Center, 1993.

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United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. NASA-UVa light aerospace alloy and structure technology program supplement: Aluminum-based materials for high speed aircraft. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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Center, Langley Research, ed. NASA-UVa light aerospace alloy and structure technology program supplement: Aluminum-based materials for high speed aircraft. National Aeronautics and Space Administration, Langley Research Center, 1997.

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United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. NASA-UVa light aerospace alloy and structure technology program suppleyment: Aluminum-based materials for high speed aircraft. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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Starke, E. A. NASA-UVa Light Aerospace Alloy and Structure Technology Program supplement: aluminum-based materials for high speed aircraft. Langley Research Center, 1993.

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United States. National Aeronautics and Space Administration., ed. Modelling directional soldification: Second semi-annual progress report, 1 November 1990 to 30 April 1991. Clarkson University, 1991.

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L, Regelʹ L., and United States. National Aeronautics and Space Administration., eds. Modelling directional soldification: Progress report on grant NAG8-831, 1 May 1991 to 31 October 1992. Clarkson University, 1991.

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United States. National Aeronautics and Space Administration., ed. Modelling directional soldification: Fourth semi-annual progress report, 1 March 1987 to 31 August 1987. Clarkson University, 1987.

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L, Regel £. L., and United States. National Aeronautics and Space Administration., eds. Modelling directional soldification: Progress report on grant NAG8-831, 1 May 1991 to 31 October 1992. Clarkson University, 1991.

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Book chapters on the topic "Aerospace Structure"

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van ‘t Hoff, Stefan, Philipp Hofmeister, Linghai Lu, Gareth D. Padfield, Giuseppe Quaranta, and Mark White. "Structure of the RCbS Process." In Springer Aerospace Technology. Springer Nature Switzerland, 2025. https://doi.org/10.1007/978-3-031-86398-1_2.

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Abstract In this Chapter, the RCbS Process is outlined, highlighting the Phases necessary to progress from developing the Requirements Specification through to presenting the Credibility assessment as a critical aspect of the Certification.
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Krumweide, Gary C., and Eddy A. Derby. "Aerospace Equipment and Instrument Structure." In Handbook of Composites. Springer US, 1998. http://dx.doi.org/10.1007/978-1-4615-6389-1_48.

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Li, Quanxin, Liang Wang, Weiping Yang, and Sufen Zhang. "Numerical Investigation of Fluid-Structure Interaction Dynamics in Micro-Rotors." In Springer Aerospace Technology. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-96-3240-4_20.

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Zhang, Yipeng, Hai Huang, and Shenyan Chen. "Structure analysis and optimisation of SSS-1 microsatellite." In Aerospace and Associated Technology. Routledge, 2022. http://dx.doi.org/10.1201/9781003324539-64.

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Gunasegeran, Muthukumaran, P. Edwin Sudhagar, and A. Ananda Babu. "Failure of Composite Structure." In Repair of Advanced Composites for Aerospace Applications. CRC Press, 2022. http://dx.doi.org/10.1201/9781003200994-9.

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Zhao, Guoyang, Jian Shi, and Zhaowei Zeng. "Improved Design and Compression Buckling Performance of a Quasi-Zero-Stiffness Vibration Isolation Metamaterial Structure." In Springer Aerospace Technology. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-96-3240-4_22.

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Arviso, Michael, D. Gregory Tipton, and Patrick S. Hunter. "Preliminary Validation of a Complex Aerospace Structure." In Structural Dynamics, Volume 3. Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-9834-7_64.

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Pironneau, Olivier. "Numerical Study of a Monolithic Fluid–Structure Formulation." In Variational Analysis and Aerospace Engineering. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-45680-5_15.

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Bracco, F. V. "Structure of High-Speed Full-Cone Sprays." In Recent Advances in the Aerospace Sciences. Springer US, 1985. http://dx.doi.org/10.1007/978-1-4684-4298-4_10.

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Sanjay, A. V., and B. Sudarshan. "Effect of oblique shocks interaction on the inlet structure in a hypersonic flow." In Aerospace and Associated Technology. Routledge, 2022. http://dx.doi.org/10.1201/9781003324539-96.

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Conference papers on the topic "Aerospace Structure"

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Naydenkin, E. V., I. P. Mishin, I. V. Ratochka, and V. A. Vinokurov. "High-strength nanostructured titanium alloy for aerospace industry." In ADVANCED MATERIALS WITH HIERARCHICAL STRUCTURE FOR NEW TECHNOLOGIES AND RELIABLE STRUCTURES. AIP Publishing LLC, 2015. http://dx.doi.org/10.1063/1.4932850.

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Joshi, Ashok. "Structure - Control Interactions in Flexible Aerospace Vehicles." In 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
18th AIAA/ASME/AHS Adaptive Structures Conference
12th. American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-2948.

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Mariano, Silvio Luiz, Marcelo Gomes da Silva, André Moreno da Costa Moreira, Everaldo de Barros, and Leandro Ribeiro de Camargo. "Modal Correlation of an Aerospace Structure." In 2006 SAE Brasil Congress and Exhibit. SAE International, 2006. http://dx.doi.org/10.4271/2006-01-2786.

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Kawabe, Hiroki, Yuichiro Aoki, and Toshiya Nakamura. "Biological Optimization of Aerospace Shell Structure." In AIAA SCITECH 2022 Forum. American Institute of Aeronautics and Astronautics, 2022. http://dx.doi.org/10.2514/6.2022-2602.

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Kim, Seung Jo, Ki-Ook Kim, Jungsun Park, Maenghyo Cho, Eui Sup Shin, and Jin Yeon Cho. "Advancements of Aerospace Computational Structure Technology in Korea." In 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-2439.

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Blair, Max, and Greg Reich. "A demonstration of CAD/CAM/CAE in a fully associative aerospace design environment." In 37th Structure, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-1630.

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ELLIS, DAVID. "Overview - Design of an efficient lightweight airframe structure forthe National Aerospace Plane." In 30th Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-1406.

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Yoshida, Tsutomu, and Takuya Ishida. "Practical Ductile Fracture Criterion Model for Metallic Aerospace Structure Static Strength Evaluations." In ASME 2023 Aerospace Structures, Structural Dynamics, and Materials Conference. American Society of Mechanical Engineers, 2023. http://dx.doi.org/10.1115/ssdm2023-105345.

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Abstract A practical ductile fracture criterion model is developed, which is well suited for the aerospace structure static strength evaluations using detailed finite element analysis. The model is based on the classical Coulomb-Mohr fracture criterion and extended to handle strength anisotropy commonly present in aerospace structural metal materials through the application of stress linear transformation. The resulting model (TCM: Transformed Coulomb-Mohr model) employs the model parameter identification procedure which utilizes the well-established statistically based material allowable data
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Alexander, Eric, Ben Carey, Michael DiNardo, et al. "Validated Aerospace Soft Impact Modeling Platform." In ASME 2012 Fluids Engineering Division Summer Meeting collocated with the ASME 2012 Heat Transfer Summer Conference and the ASME 2012 10th International Conference on Nanochannels, Microchannels, and Minichannels. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/fedsm2012-72459.

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The research has been dedicated to developing a virtual crashworthiness platform for large advanced aircraft structures when subjected to water ditching incidents. A numerical design tool, incorporating fluid-structure interaction analysis module, was created to assess damage tolerance in future aerospace design concepts to help with the prognosis of structural failure. To accomplish this, an experimental water impact set up was used to calibrate and validate the developed detailed virtual model. Specific data acquisition techniques implemented allowed for the capture of strain distribution an
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Eremenko, A. "Aquarius main structure configuration." In 2013 IEEE Aerospace Conference. IEEE, 2013. http://dx.doi.org/10.1109/aero.2013.6496819.

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Reports on the topic "Aerospace Structure"

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Swanson, F., E. Kamykowski, M. Horn, and N. Holden. Neutron radiography of aerospace structure hidden corrosion. Office of Scientific and Technical Information (OSTI), 1995. http://dx.doi.org/10.2172/10130409.

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Freeman, Arthur J., Oleg Y. Kontsevoi, Yuri N. Gornostyrev, and Nadezhda I. Medvedeva. Fundamental Electronic Structure Characteristics and Mechanical Behavior of Aerospace Materials. Defense Technical Information Center, 2008. http://dx.doi.org/10.21236/ada480633.

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Perdigão, Rui A. P. Triadic Flight Technologies. Synergistic Manifolds, 2024. http://dx.doi.org/10.46337/240307.

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A novel triadic suite of flight technologies is introduced by developing, articulating and integrating ground-effect, free amphibian flight and orbital flight capabilities into a triadic system-of-systems able to seamlessly operate across all three mobility paradigms. The triad is then implemented onto our new purpose-designed hydro-aerospace vehicle, propelled by latest-generation micro-reactors for industry-leading aerospace thrust, whilst providing long-range carbon-free flight mobility and autonomy. The vehicle structure and materials are further optimized for a seamless switch between sta
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Atluri, S. N. AASERT-Structural Integrity of Aging of Aerospace Structures and Repairs. Defense Technical Information Center, 1996. http://dx.doi.org/10.21236/ada326704.

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Venkayya, Vipperla B. Aerospace Structures Design on Computers. Defense Technical Information Center, 1989. http://dx.doi.org/10.21236/ada208811.

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Grandhi, Ramana V., and Geetha Bharatram. Multiobjective Optimization of Aerospace Structures. Defense Technical Information Center, 1992. http://dx.doi.org/10.21236/ada260433.

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Farhat, Charbel. Multidisciplinary Thermal Analysis of Hot Aerospace Structures. Defense Technical Information Center, 2010. http://dx.doi.org/10.21236/ada564851.

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Muelaner, Jody Emlyn. Generative Design in Aerospace and Automotive Structures. SAE International, 2024. http://dx.doi.org/10.4271/epr2024016.

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&lt;div class="section abstract"&gt;&lt;div class="htmlview paragraph"&gt;Semi-automated computational design methods involving physics-based simulation, optimization, machine learning, and generative artificial intelligence (AI) already allow greatly enhanced performance alongside reduced cost in both design and manufacturing. As we progress, developments in user interfaces, AI integration, and automation of workflows will increasingly reduce the human inputs required to achieve this. With this, engineering teams must change their mindset from designing products to specifying requirements, fo
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Grandt, A. F., Farris Jr., Hillberry T. N., and B. H. Analysis of Widespread Fatigue Damage in Aerospace Structures. Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada360820.

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Selvam, R. P., and Zu-Qing Qu. Adaptive Navier Stokes Flow Solver for Aerospace Structures. Defense Technical Information Center, 2004. http://dx.doi.org/10.21236/ada424479.

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